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lOMoARcPSD|6566483

INSTRUCTOR'S SOLUTIONS MANUAL for

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL Robert A. Adams University of British Columbia

Calculus Ninth Edition Robert A. Adams University of British Columbia

Christopher Essex University of Western Ontario

dumperina

ISBN: 978-0-13-452876-2 Copyright © 2018 Pearson Canada Inc., Toronto, Ontario. All rights reserved. This work is protected by Canadian copyright laws and is provided solely for the use of instructors in teaching their courses and assessing student learning. Dissemination or sale of any part of this work (including on the Internet) will destroy the integrity of the work and is not permitted. The copyright holder grants permission to instructors who have adopted Calculus: A Complete Course, Single-Variable Calculus, or Calculus of Several Variables by Adams and Essex, to post this material online only if the use of the website is restricted by access codes to students in the instructor’s class that is using the textbook and provided the reproduced material bears this copyright notice.

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FOREWORD These solutions are provided for the benefit of instructors using the textbooks:

Calculus: A Complete Course (9th Edition), Single-Variable Calculus (9th Edition), and Calculus of Several Variables (9th Edition) by R. A. Adams and Chris Essex, published by Pearson Canada. For the most part, the solutions are detailed, especially in exercises on core material and techniques. Occasionally some details are omitted—for example, in exercises on applications of integration, the evaluation of the integrals encountered is not always given with the same degree of detail as the evaluation of integrals found in those exercises dealing specifically with techniques of integration. Instructors may wish to make these solutions available to their students. However, students should use such solutions with caution. It is always more beneficial for them to attempt exercises and problems on their own, before they look at solutions done by others. If they examine solutions as “study material” prior to attempting the exercises, they can lose much of the benefit that follows from diligent attempts to develop their own analytical powers. When they have tried unsuccessfully to solve a problem, then looking at a solution can give them a “hint” for a second attempt. Separate Student Solutions Manuals for the books are available for students. They contain the solutions to the even-numbered exercises only. November, 2016. R. A. Adams [email protected]

Chris Essex [email protected]

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lOMoARcPSD|6566483

CONTENTS

Solutions for Chapter P

1

Solutions for Chapter 1

23

Solutions for Chapter 2

39

Solutions for Chapter 3

81

Solutions for Chapter 4

108

Solutions for Chapter 5

177

Solutions for Chapter 6

213

Solutions for Chapter 7

267

Solutions for Chapter 8

316

Solutions for Chapter 9

351

Solutions for Chapter 10

392

Solutions for Chapter 11

420

Solutions for Chapter 12

448

Solutions for Chapter 13

491

Solutions for Chapter 14

538

Solutions for Chapter 15

579

Solutions for Chapter 16

610

Solutions for Chapter 17

637

Solutions for Chapter 18

644

Solutions for Chapter 18-cosv9

671

Solutions for Appendices

683

NOTE: “Solutions for Chapter 18-cosv9” is only needed by users of Calculus of Several Variables (9th Edition), which includes extra material in Sections 18.2 and 18.5 that is found in Calculus: a Complete Course and in Single-Variable Calculus in Sections 7.9 and 3.7 respectively. Solutions for Chapter 18-cosv9 contains only the solutions for the two Sections 18.2 and 18.9 in the Several Variables book. All other Sections are in “Solutions for Chapter 18.” It should also be noted that some of the material in Chapter 18 is beyond the scope of most students in single-variable calculus courses as it requires the use of multivariable functions and partial derivatives.

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INSTRUCTOR’S SOLUTIONS MANUAL

CHAPTER P.

SECTION P.1 (PAGE 10)

PRELIMINARIES

19.

Given: 1=.2 x/ < 3. CASE I. If x < 2, then 1 < 3.2 x/ D 6 3x, so 3x < 5 and x < 5=3. This case has solutions x < 5=3. CASE II. If x > 2, then 1 > 3.2 x/ D 6 3x, so 3x > 5 and x > 5=3. This case has solutions x > 2. Solution: . 1; 5=3/ [ .2; 1/.

20.

Given: .x C 1/=x  2. CASE I. If x > 0, then x C 1  2x, so x  1. CASE II. If x < 0, then x C 1  2x, so x  1. (not possible) Solution: .0; 1.

21.

Given: x 2 2x  0. Then x.x 2/  0. This is only possible if x  0 and x  2. Solution: Œ0; 2.

Section P.1 Real Numbers and the Real Line (page 10) 1.

2 D 0:22222222    D 0:2 9

2.

1 D 0:09090909    D 0:09 11

3. If x D 0:121212   , then 100x D 12:121212    D 12 C x. Thus 99x D 12 and x D 12=99 D 4=33. 4. If x D 3:277777   , then 10x 32 D 0:77777    and 100x 320 D 7 C .10x 32/, or 90x D 295. Thus x D 295=90 D 59=18. 5.

1=7 D 0:142857142857    D 0:142857

22.

Given 6x 2 5x  1, then .2x 1/.3x 1/  0, so either x  1=2 and x  1=3, or x  1=3 and x  1=2. The latter combination is not possible. The solution set is Œ1=3; 1=2.

23.

Given x 3 > 4x, we have x.x 2 4/ > 0. This is possible if x < 0 and x 2 < 4, or if x > 0 and x 2 > 4. The possibilities are, therefore, 2 < x < 0 or 2 < x < 1. Solution: . 2; 0/ [ .2; 1/.

2=7 D 0:285714285714    D 0:285714 3=7 D 0:428571428571    D 0:428571

4=7 D 0:571428571428    D 0:571428 note the same cyclic order of the repeating digits 5=7 D 0:714285714285    D 0:714285

24.

6=7 D 0:857142857142    D 0:857142

6. Two different decimal expansions can represent the same number. For instance, both 0:999999    D 0:9 and 1:000000    D 1:0 represent the number 1. 7.

25.

x  0 and x  5 define the interval Œ0; 5.

8. x < 2 and x  3 define the interval Œ 3; 2/. 5 or x
10. x  11.

6 defines the union . 1; 6/ [ . 5; 1/.

1 defines the interval . 1; 1.

2x > 4, then x
0. Solution: .0; 1/ 2

18. If x < 9, then jxj < 3 and . 3; 3/

3 < x < 3. Solution:

2 3 < . x 1 xC1 CASE I. If x > 1 then .x 1/.x C 1/ > 0, so that 3.x C 1/ < 2.x 1/. Thus x < 5. There are no solutions in this case. CASE II. If 1 < x < 1, then .x 1/.x C 1/ < 0, so 3.x C 1/ > 2.x 1/. Thus x > 5. In this case all numbers in . 1; 1/ are solutions. CASE III. If x < 1, then .x 1/.x C 1/ > 0, so that 3.x C 1/ < 2.x 1/. Thus x < 5. All numbers x < 5 are solutions. Solutions: . 1; 5/ [ . 1; 1/.

Given:

12. x < 4 or x  2 defines the interval . 1; 1/, that is, the whole real line. 13. If

4 x 1C . 2 x CASE I. If x > 0, then x 2  2x C 8, so that x 2 2x 8  0, or .x 4/.x C 2/  0. This is possible for x > 0 only if x  4. CASE II. If x < 0, then we must have .x 4/.x C 2/  0, which is possible for x < 0 only if x  2. Solution: Œ 2; 0/ [ Œ4; 1/. Given:

26.

2 defines the interval . 2; 1/.

x>

Given x 2 x  2, then x 2 x 2  0 so .x 2/.x C1/  0. This is possible if x  2 and x  1 or if x  2 and x  1. The latter situation is not possible. The solution set is Œ 1; 2.

3j D 7, then x

t j D 1, then 1

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3 D ˙7, so x D

4 or x D 10. 9=2 or

t D ˙1, so t D 0 or t D 2. 1 or 17, and

1

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SECTION P.1 (PAGE 10)

ADAMS and ESSEX: CALCULUS 9

ˇs ˇ s ˇ ˇ 32. If ˇ 1ˇ D 1, then 1 D ˙1, so s D 0 or s D 4. 2 2 33. If jxj < 2, then x is in . 2; 2/.

4.

From A.0:5; 3/ to B.2; 3/, x D 2 y D 3 3 D 0. jABj D 1:5.

5.

Starting point: . 2; 3/. Increments x D 4, y D New position is . 2 C 4; 3 C . 7//, that is, .2; 4/.

6.

Arrival point: . 2; 2/. Increments x D 5, y D 1. Starting point was . 2 . 5/; 2 1/, that is, .3; 3/.

7.

x 2 C y 2 D 1 represents a circle of radius 1 centred at the origin. p x 2 C y 2 D 2 represents a circle of radius 2 centred at the origin.

34. If jxj  2, then x is in Œ 2; 2. 35. If js

1j  2, then 1

36. If jt C 2j < 1, then . 3; 1/.

2  s  1 C 2, so s is in Œ 1; 3. 2

2 C 1, so t is in

1 < t
jx 3j says that the distance from x to 1 is greater than the distance from x to 3, so x must be to the right of the point half-way between 1 and 3. Thus x > 1.

jxj  jx C yj Apply this inequality with x D a ja

bj  jaj

jyj: b and y D b to get jbj:

ˇ ˇ ˇ ˇ Similarly, ja bj D jb aj  jbj jaj. Since ˇjaj jbjˇ is equal to either jaj jbj or jbj jaj, depending on the sizes of a and b, we have ja

ˇ ˇ bj  ˇjaj

ˇ ˇ jbjˇ:

Section P.2 Cartesian Coordinates in the Plane (page 16) 1.

From A.0; 3/ to B.4; 0/, xp D 4 0 D 4 and y D 0 3 D 3. jABj D 42 C . 3/2 D 5.

2. From A. 1; 2/ to B.4; 10/, xpD 4 . 1/ D 5 and y D 10 2 D 12. jABj D 52 C . 12/2 D 13. 3. From A.3; 2/ to B. 1; 2/, x and pD 1 3 D 4p y D 2 2 D 4. jABj D . 4/2 C . 4/2 D 4 2. 2

11.

x 2 C y 2  1 represents points inside and on the circle of radius 1 centred at the origin.

y  x 2 represents all points lying on or above the parabola y D x 2 .

12. y < x 2 represents all points lying below the parabola y D x2. The vertical line through . 2; 5=3/ is x D 2; the horizontal line through that point is y D 5=3. p p The vertical line through . 2; 1:3/ is x D 2; the horizontal line through that point is y D 1:3.

15.

Line through . 1; 1/ with slope m D 1 is y D 1C1.xC1/, or y D x C 2.

16.

Line through . 2; 2/ with slope m D 1=2 is y D 2 C .1=2/.x C 2/, or x 2y D 6.

17.

Line through .0; b/ with slope m D 2 is y D b C 2x.

1/,

45. The triangle inequality jx C yj  jxj C jyj implies that

7.

10. x 2 C y 2 D 0 represents the origin.

14.

43. jaj D a if and only if a  0. It is false if a < 0. .x

9.

13.

42. jx 3j < 2jxj , x 2 6x C 9 D .x 3/2 < 4x 2 , 3x 2 C 6x 9 > 0 , 3.x C 3/.x 1/ > 0. This inequality holds if x < 3 or x > 1.

44. The equation jx 1j D 1 x holds if jx 1j D that is, if x 1  0, or, equivalently, if x  1.

8.

0:5 D 1:5 and

18. Line through .a; 0/ with slope m D or y D 2a 2x.

2 is y D 0 2.x a/,

19.

At x D 2, the height of the line 2x C 3y D 6 is y D .6 4/=3 D 2=3. Thus .2; 1/ lies above the line.

20.

At x D 3, the height of the line x 4y D 7 is y D .3 7/=4 D 1. Thus .3; 1/ lies on the line.

21.

The line through .0; 0/ and .2; 3/ has slope m D .3 0/=.2 0/ D 3=2 and equation y D .3=2/x or 3x 2y D 0.

22.

The line through . 2; 1/ and .2; 2/ has slope m D . 2 1/=.2 C 2/ D 3=4 and equation y D 1 .3=4/.x C 2/ or 3x C 4y D 2.

23.

The line through .4; 1/ and . 2; 3/ has slope m D .3 1/=. 2 4/ D or x C 3y D 7.

24. 25.

1=3 and equation y D 1

The line through . 2; 0/ and .0; 2/ has slope m D .2 0/=.0 C 2/ D 1 and equation y D 2 C x. p If m D 2 and p b D 2, then the line has equation y D 2x C 2.

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1 .x 4/ 3

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION P.2 (PAGE 16)

y

26. If m D 1=2 and b D 3, then the line has equation y D .1=2/x 3, or x C 2y D 6. 1:5x 27.

3x C 4y D 12 has x-intercept a D 12=3 D 4 and yintercept b D 12=4 D 3. Its slope is b=a D 3=4. y

2y D

3

x

Fig. P.2-30 3x C 4y D 12

31.

line through .2; 1/ parallel to y D x C 2 is y D x perpendicular to y D x C 2 is y D x C 3.

32.

line through . 2; 2/ parallel to 2xCy D 4 is 2xCy D line perpendicular to 2x C y D 4 is x 2y D 6.

33.

We have

x Fig. P.2-27

3x C 4y D 6 2x 3y D 13

28. x C 2y D 4 has x-intercept a D 4 and y-intercept b D 4=2 D 2. Its slope is b=a D 2=. 4/ D 1=2. y

2;

6x C 8y D 12 6x 9y D 39:

Subtracting these equations gives 17y D 51, so y D 3 and x D .13 9/=2 D 2. The intersection point is .2; 3/. 34.

x x C 2y D

÷

1; line

We have 2x C y D 8 5x 7y D 1

4

÷

14x C 7y D 56 5x 7y D 1:

Adding these equations gives 19x D 57, so x D 3 and y D 8 2x D 2. The intersection point is .3; 2/. 35.

If a ¤ 0 and b ¤ 0, then .x=a/ C .y=b/ D 1 represents a straight line that is neither horizontal nor vertical, and does not pass through the origin. Putting y D 0 we get x=a D 1, so the x-intercept of this line is x D a; putting x D 0 gives y=b D 1, so the y-intercept is y D b.

36.

The line .x=2/ .y=3/ D 1 has x-intercept a D 2, and y-intercept b D 3. y

Fig. P.2-28

29.

p

p p p 2x 3y D 2 has x-intercept a D 2= 2 D 2 p and y-intercept 2= 3. Its slope is p b pD b=a D 2= 6 D 2=3. y

2

p

2x

p

x

x 2

3y D 2

x

y D1 3

3

Fig. P.2-29 Fig. P.2-36 30. 1:5x 2y D 3 has x-intercept a D 3=1:5 D 2 and y-intercept b D 3=. 2/ D 3=2. Its slope is b=a D 3=4.

37. The line through .2; 1/ and .3; 1/ has slope m D . 1 1/=.3 2/ D 2 and equation y D 1 2.x 2/ D 5 2x. Its y-intercept is 5.

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SECTION P.2 (PAGE 16)

ADAMS and ESSEX: CALCULUS 9

38. The line through . 2; 5/ and .k; 1/ has x-intercept 3, so also passes through .3; 0/. Its slope m satisfies 1 k Thus k

3D

0 5 0 DmD D 3 3C2

43.

B D .1; 3/; C D . 3; 2/ p p jABj D .1 2/2 C .3 C 1/2 D 17 p p p p jAC j D . 3 2/2 C .2 C 1/2 D 34 D 2 17 p p jBC j D . 3 1/2 C .2 3/2 D 17: p Since jABj D jBC j and jAC j D 2jABj, triangle ABC is an isosceles right-angled triangle with right angle at B. Thus ABCD is a square if D is displaced from C by the same amount A is from B, that is, by increments x D 2 1 D 1 and y D 1 3 D 4. Thus D D . 3 C 1; 2 C . 4// D . 2; 2/.

44.

If M D .xm ; ym / is the midpoint of P1 P2 , then the displacement of M from P1 equals the displacement of P2 from M :

1:

1, and so k D 2.

39. C D Ax C B. If C D 5; 000 when x D 10; 000 and C D 6; 000 when x D 15; 000, then 10; 000A C B D 5; 000 15; 000A C B D 6; 000 Subtracting these equations gives 5; 000A D 1; 000, so A D 1=5. From the first equation, 2; 000 C B D 5; 000, so B D 3; 000. The cost of printing 100,000 pamphlets is $100; 000=5 C 3; 000 D $23; 000.

xm

40ı and 40ı is the same temperature on both the Fahrenheit and Celsius scales. C 40

xq

C DF

-20 -30

46. 10 20 30 40 50 60 70 80 F C D

5 .F 9

47.

A D .2; 1/; B D .6; 4/; C D .5; 3/ p p jABj D .6 2/2 C .4 1/2 D 25 D 5 p p jAC j D .5 2/2 C . 3 1/2 D 25 D 5 p p p jBC j D .6 5/2 C .4 C 3/2 D 50 D 5 2: Since jABj D jAC j, triangle ABC is isosceles. p A D .0; 0/; B D .1; 3/; C D .2; 0/ q p p jABj D .1 0/2 C . 3 0/2 D 4 D 2 p p jAC j D .2 0/2 C .0 0/2 D 4 D 2 q p p 3/2 D 4 D 2: jBC j D .2 1/2 C .0 Since jABj D jAC j D jBC j, triangle ABC is equilateral.

4

x1 D 2.x2

xq /;

.x C X/=2 D 2;

Fig. P.2-40

42.

y1 D y2

ym :

yq

y1 D 2.y2

yq /:

Let the coordinates of P be .x; 0/ and those of Q be .X; 2X/. If the midpoint of PQ is .2; 1/, then

32/

-40 . 40; 40/ -50

41.

ym

Thus xq D .x1 C 2x2 /=3 and yq D .y1 C 2y2 /=3.

10 -50 -40 -30 -20 -10 -10

xm ;

If Q D .xq ; yq / is the point on P1 P2 that is two thirds of the way from P1 to P2 , then the displacement of Q from P1 equals twice the displacement of P2 from Q:

30 20

x1 D x2

Thus xm D .x1 C x2 /=2 and ym D .y1 C y2 /=2. 45.

40.

A D .2; 1/;

48.

.0

2X/=2 D 1:

The second equation implies that X D 1, and the second then implies that x D 5. Thus P is .5; 0/. p .x 2/2 C y 2 D 4 says that the distance of .x; y/ from .2; 0/ is 4, so the equation represents a circle of radius 4 centred at .2; 0/. p p .x 2/2 C y 2 D x 2 C .y 2/2 says that .x; y/ is equidistant from .2; 0/ and .0; 2/. Thus .x; y/ must lie on the line that is the right bisector of the line from .2; 0/ to .0; 2/. A simpler equation for this line is x D y.

49.

The line 2x C ky D 3 has slope m D 2=k. This line is perpendicular to 4x C y D 1, which has slope 4, provided m D 1=4, that is, provided k D 8. The line is parallel to 4x C y D 1 if m D 4, that is, if k D 1=2.

50.

For any value of k, the coordinates of the point of intersection of x C 2y D 3 and 2x 3y D 1 will also satisfy the equation .x C 2y

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3/ C k.2x

3y C 1/ D 0

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION P.3 (PAGE 22)

because they cause both expressions in parentheses to be 0. The equation above is linear in x and y, and so represents a straight line for any choice of k. This line will pass through .1; 2/ provided 1 C 4 3 C k.2 6 C 1/ D 0, that is, if k D 2=3. Therefore, the line through the point of intersection of the two given lines and through the point .1; 2/ has equation x C 2y

2 3 C .2x 3

3y C 1/ D 0;

13.

Together, x 2 C y 2 > 1 and x 2 C y 2 < 4 represent annulus (washer-shaped region) consisting of all points that are outside the circle of radius 1 centred at the origin and inside the circle of radius 2 centred at the origin.

14.

Together, x 2 C y 2  4 and .x C 2/2 C y 2  4 represent the region consisting of all points that are inside or on both the circle of radius 2 centred at the origin and the circle of radius 2 centred at . 2; 0/.

15.

Together, x 2 Cy 2 < 2x and x 2 Cy 2 < 2y (or, equivalently, .x 1/2 C y 2 < 1 and x 2 C .y 1/2 < 1) represent the region consisting of all points that are inside both the circle of radius 1 centred at .1; 0/ and the circle of radius 1 centred at .0; 1/.

16.

x2 C y2 4x C 2y > 4 can be rewritten .x 2/2 C .y C 1/2 > 9. This equation, taken together with x C y > 1, represents all points that lie both outside the circle of radius 3 centred at .2; 1/ and above the line x C y D 1.

17.

The interior of the circle with centre . 1; 2/ and radius p 6 is given by .x C 1/2 C .y 2/2 < 6, or 2 x C y 2 C 2x 4y < 1.

or, on simplification, x D 1.

Section P.3 Graphs of Quadratic Equations (page 22) 1.

x 2 C y 2 D 16

2. x 2 C .y

2/2 D 4, or x 2 C y 2

4y D 0

3. .x C 2/2 C y 2 D 9, or x 2 C y 2 C 4y D 5 4. .x 5.

x2 C y2 x

6.

3/2 C .y C 4/2 D 25, or x 2 C y 2

2

6x C 8y D 0.

2x D 3

2x C 1 C y 2 D 4

.x 1/2 C y 2 D 4 centre: .1; 0/; radius 2.

18. The exterior of the circle with centre .2; 3/ and radius 4 is given by .x 2/2 C .y C 3/2 > 16, or x 2 C y 2 4x C 6y > 3.

x 2 C y 2 C 4y D 0

19.

2

2

x C y C 4y C 4 D 4 2

7.

x2 C y2

x

2

2x C 4y D 4

2x C 1 C y 2 C 4y C 4 D 9

.x 1/2 C .y C 2/2 D 9 centre: .1; 2/; radius 3. 8.

x2 C y2

x2

2x

yC1D0

2x C 1 C y 2

yC

1 4

D

2 .x 1/2 C y 12 D 41 centre: .1; 1=2/; radius 1=2.

1 4

2

2

x1 1/2 C .y

3/2 < 10

20.

x C y > 4;

21.

The parabola with focus .0; 4/ and directrix y D equation x 2 D 16y.

22.

The parabola with focus .0; 1=2/ and directrix y D 1=2 has equation x 2 D 2y.

23.

The parabola with focus .2; 0/ and directrix x D equation y 2 D 8x.

24.

The parabola with focus . 1; 0/ and directrix x D 1 has equation y 2 D 4x.

25.

y D x 2 =2 has focus .0; 1=2/ and directrix y D

2

x C .y C 2/ D 4 centre: .0; 2/; radius 2.

x 2 C y 2 < 2;

.x

2 has

1=2.

y

9. x 2 C y 2 > 1 represents all points lying outside the circle of radius 1 centred at the origin.

yDx 2 =2

.0;1=2/

10. x 2 C y 2 < 4 represents the open disk consisting of all points lying inside the circle of radius 2 centred at the origin. 11.

4 has

x yD 1=2

.x C 1/2 C y 2  4 represents the closed disk consisting of all points lying inside or on the circle of radius 2 centred at the point . 1; 0/.

12. x 2 C .y 2/2  4 represents the closed disk consisting of all points lying inside or on the circle of radius 2 centred at the point .0; 2/.

Fig. P.3-25 26.

yD

x 2 has focus .0; 1=4/ and directrix y D 1=4.

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5

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SECTION P.3 (PAGE 22)

ADAMS and ESSEX: CALCULUS 9

y

y

Version (c) yD1=4

y D x2

x

.3; 3/ Version (b)

.0; 1=4/ yD x 2

Fig. P.3-26

x 4 Version (d) .4; 2/

27.

xD

Version (a) 3

y 2 =4 has focus . 1; 0/ and directrix x D 1. y

Fig. P.3-29 a) has equation y D x 2

xD1 . 1;0/

b) has equation y D .x

x

c) has equation y D .x d) has equation y D .x

xD y 2 =4

30. Fig. P.3-27

28. x D y 2 =16 has focus .4; 0/ and directrix x D

4.

y

31. .4;0/

32. x

33.

xD 4 xDy 2 =16

34. Fig. P.3-28

6

8x C 16.

3/2 C 3 or y D x 2 4/2

2, or y D x 2

6x C 12. 8x C 14.

b) If y D mx is shifted vertically by amount y1 , the equation y D mx C y1 results. If .a; b/ satisfies this equation, then b D ma C y1 , and so y1 D b ma. Thus the shifted equation is y D mx C b ma D m.x a/ C b, the same equation obtained in part (a). p y D .x=3/ C 1 p 4y D x C 1 p y D .3x=2/ C 1 p .y=2/ D 4x C 1 x 2 shifted down 1, left 1 gives y D

35.

yD1

36.

x2 C y2 D .x C 4/2 C .y

38.

4/2 or y D x 2

a) If y D mx is shifted to the right by amount x1 , the equation y D m.x x1 / results. If .a; b/ satisfies this equation, then b D m.a x1 /, and so x1 D a .b=m/. Thus the shifted equation is y D m.x a C .b=m// D m.x a/ C b.

37. y D .x y D .x 29.

3.

.x C 1/2 .

5 shifted up 2, left 4 gives 2/2 D 5.

1/2 2/2

1 shifted down 1, right 1 gives 2. p p y D x shifted down 2, left 4 gives y D x C 4

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2.

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION P.3 (PAGE 22)

y

39. y D x 2 C 3, y D 3x C 1. Subtracting these equations gives x 2 3x C 2 D 0, or .x 1/.x 2/ D 0. Thus x D 1 or x D 2. The corresponding values of y are 4 and 7. The intersection points are .1; 4/ and .2; 7/.

9x 2 C16y 2 D144

x

40. y D x 2 6, y D 4x x 2 . Subtracting these equations gives 2x 2 4x 6 D 0, or 2.x 3/.x C 1/ D 0. Thus x D 3 or x D 1. The corresponding values of y are 3 and 5. The intersection points are .3; 3/ and . 1; 5/. 41. x 2 C y 2 D 25, 3x C 4y D 0. The second equation says that y D 3x=4. Substituting this into the first equation gives 25x 2 =16 D 25, so x D ˙4. If x D 4, then the second equation gives y D 3; if x D 4, then y D 3. The intersection points are .4; 3/ and . 4; 3/. Note that having found values for x, we substituted them into the linear equation rather than the quadratic equation to find the corresponding values of y. Had we substituted into the quadratic equation we would have got more solutions (four points in all), but two of them would have failed to satisfy 3x C 4y D 12. When solving systems of nonlinear equations you should always verify that the solutions you find do satisfy the given equations. 42. 2x 2 C 2y 2 D 5, xy D 1. The second equation says that y D 1=x. Substituting this into the first equation gives 2x 2 C .2=x 2 / D 5, or 2x 4 5x 2 C 2 D 0. This equation factors to p .2x 2 1/.x 2 p2/ D 0, so its solutions are x D ˙1= 2 and x D ˙ 2. The corresponding values of y are givenpby p y D 1=x. p Therefore, p the p intersection p points are .1= 2; 2/, . 1= 2; 2/, . 2; 1= 2/, and p p 2; 1= 2/. .

Fig. P.3-44

45.

3/2

.y C 2/2 D 1 is an ellipse with centre at 9 4 .3; 2/, major axis between .0; 2/ and .6; 2/ and minor axis between .3; 4/ and .3; 0/. .x

C

y

x

.3; 2/

.x 3/2 .yC2/2 C D1 9 4

Fig. P.3-45

46.

43. .x 2 =4/ C y 2 D 1 is an ellipse with major axis between . 2; 0/ and .2; 0/ and minor axis between .0; 1/ and .0; 1/.

.y C 1/2 D 4 is an ellipse with centre at 4 .1; 1/, major axis between .1; 5/ and .1; 3/ and minor axis between . 1; 1/ and .3; 1/. .x

1/2 C

y

.x 1/2 C

.yC1/2 D4 4

y x2 2 4 Cy D1

x .1; 1/ x

Fig. P.3-46 Fig. P.3-43 44. 9x 2 C 16y 2 D 144 is an ellipse with major axis between . 4; 0/ and .4; 0/ and minor axis between .0; 3/ and .0; 3/.

47.

.x 2 =4/ y 2 D 1 is a hyperbola with centre at the origin and passing through .˙2; 0/. Its asymptotes are y D ˙x=2.

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7

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SECTION P.3 (PAGE 22)

ADAMS and ESSEX: CALCULUS 9

y

y x2 4

y 2 D1

yD x=2

.x

x 1/.y C 2/ D 1 yD

x yDx=2

2

xD1

Fig. P.3-47

Fig. P.3-50 51.

48. x 2 y 2 D 1 is a rectangular hyperbola with centre at the origin and passing through .0; ˙1/. Its asymptotes are y D ˙x. y x2 y2 D 1

yDx

a) Replacing x with x replaces a graph with its reflection across the y-axis. b) Replacing y with y replaces a graph with its reflection across the x-axis.

52.

Replacing x with x and y with y reflects the graph in both axes. This is equivalent to rotating the graph 180ı about the origin.

53.

jxj C jyj D 1. In the first quadrant the equation is x C y D 1. In the second quadrant the equation is x C y D 1. In the third quadrant the equation is x y D 1. In the fourth quadrant the equation is x y D 1.

x yD x

y Fig. P.3-48 1 jxj C jyj D 1 1

49. xy D 4 is a rectangular hyperbola with centre at the origin and passing through .2; 2/ and . 2; 2/. Its asymptotes are the coordinate axes.

x

1

y

1

Fig. P.3-53 x

Section P.4 Functions and Their Graphs (page 32)

xyD 4

Fig. P.3-49

50. .x 1/.y C 2/ D 1 is a rectangular hyperbola with centre at .1; 2/ and passing through .2; 1/ and .0; 3/. Its asymptotes are x D 1 and y D 2.

8

1.

f .x/ D 1 C x 2 ; domain R, range Œ1; 1/

2.

f .x/ D 1

3.

G.x/ D

4.

F .x/ D 1=.x 1/; domain . 1; 1/ [ .1; 1/, range . 1; 0/ [ .0; 1/

p

p

8

x; domain Œ0; 1/, range . 1; 1 2x; domain . 1; 4, range Œ0; 1/

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION P.4 (PAGE 32)

t ; domain . 1; 2/, range R. (The equation 2 t y D h.t / can be squared and rewritten as t 2 C y 2 t 2y 2 D 0, a quadratic equation in t having real solutions for every real value of y. Thus the range of h contains all real numbers.)

1 p ; domain Œ2; 3/ [ .3; 1/, range 1 x 2 . 1; 0/ [ .0; 1/. The equation y D g.x/ can be solved for x D 2 .1 .1=y//2 so has a real solution provided y ¤ 0.

b) is the graph of x 2 if x < 1.

y

x/, which is positive

d) is the graph of x 3 x 4 , which is positive if 0 < x < 1 and behaves like x 3 near 0. 9. x 0 ˙0:5 ˙1 ˙1:5 ˙2

y graph (i)

x 3 D x 2 .1

c) is the graph of x x 4 , which is positive if 0 < x < 1 and behaves like x near 0.

6. g.x/ D

7.

x/2 , which is positive for x > 0.

a) is the graph of x.1

5. h.t / D p

graph (ii)

f .x/ D x 4 0 0:0625 1 5:0625 16

y x y

y D x4

x y

graph (iii)

graph (iv)

x

x x

Fig. P.4-7 Graph (ii) is the graph of a function because vertical lines can meet the graph only once. Graphs (i), (iii), and (iv) do not have this property, so are not graphs of functions.

Fig. P.4-9 10.

8. y

y

graph (a)

graph (b)

x

f .x/ D x 2=3

0 ˙0:5 ˙1 ˙1:5 ˙2

0 0:62996 1 1:3104 1:5874 y

x

y

y

graph (c)

yDx

x

2=3

graph (d) x Fig. P.4-10 11.

x Fig. P.4-8

x

f .x/ D x 2 C 1 is even: f . x/ D f .x/

12. f .x/ D x 3 C x is odd: f . x/ D f .x/ x is odd: f . x/ D f .x/ 13. f .x/ D 2 x 1

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9

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SECTION P.4 (PAGE 32)

1

14.

f .x/ D

x2

15.

f .x/ D

x

16. f .x/ D f. 4

17.

1

1 2

ADAMS and ESSEX: CALCULUS 9

26.

is even: f . x/ D f .x/ is odd about .2; 0/: f .2

y

x/ D

f .2 C x/

1 is odd about . 4; 0/: xC4 x/ D f . 4 C x/

f .x/ D x 2

x

18. f .x/ D x 3 2 is odd about .0; 2/: f . x/ C 2 D .f .x/ C 2/ 3

yD.x 1/2 C1

6x is even about x D 3: f .3 x/ D f .3 C x/ 27.

y

3

19. f .x/ D jx j D jxj is even: f . x/ D f .x/ 20. f .x/ D jx C 1j is even about x D 1: f . 1 x/ D f . 1 C x/ p 21. f .x/ D 2x has no symmetry. p 22. f .x/ D .x 1/2 is even about x D 1: f .1 x/ D f .1 C x/ 23.

yD1 x 3

x

28.

y

y yD x 2

x

x yD.xC2/3

24.

29.

y

y yD1 x 2 p yD xC1 x

x

25.

30. y

y

yD.x 1/2 p yD xC1

x x

10

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION P.4 (PAGE 32)

31.

36. y

y x

xD2

x yD jxj yD

32.

1 2 x

37.

y

y x yD xC1

yDjxj 1

yD1 x x xD 1

33.

38.

y

y xD1 yDjx 2j x yD 1 x yD 1 x

x

34. y

39.

yD1Cjx 2j

y

y .1;3/ yDf .x/C2 2

.2;2/

.1;1/ yDf .x/ x

2

x

x

Fig. P.4.39(a)

35.

Fig. P.4.39(b)

y

40. y

y .1;3/ yDf .x/C2

xD 2 2

.2;2/

x 1 x 1 yD

yDf .x/ 1 x .2; 1/

2 xC2

Fig. P.4.40(a)

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Fig. P.4.40(b)

11

lOMoARcPSD|6566483

SECTION P.4 (PAGE 32)

ADAMS and ESSEX: CALCULUS 9

y 0.8 0.6

41. y

y D 0:68 x C 2 yD 2 x C 2x C 3

0.4 0.2

. 1;1/ yDf .xC2/ x

2

-5

-4

-3

-2

-1 -0.2

1y D2 0:18 3

4

x

-0.4 -0.6

42. y

.2;1/

1

-0.8 -1.0 Fig. P.4-47

yDf .x 1/ 3

x

48.

Range is approximately . 1; 0:1 [ Œ2:9; 1/. y

43. 4

y

3 2 2 yD f .x/ .1; 1/

1

x

-4

-3 -2 -1

1 -1

44. y

-2

2

3 4 5 x 2 yD x.x C 2/

6 x

-3

. 1;1/ yDf . x/

-4 x

2

-5 Fig. P.4-48

45. y

49. y yDf .4 x/

5

.3;1/

4 4 x

2

3 2 46. y

1 -5

. 1;1/

-4

-3

.1;1/

1

Range is approximately Œ 0:18; 0:68.

2

y D x4 Fig. P.4-49

x

12

-1 -1

yD1 f .1 x/

47.

-2

3

4

x

6x 3 C 9x 2

1

Apparent symmetry about x D 1:5. This can be confirmed by calculating f .3 x/, which turns out to be equal to f .x/.

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION P.5 (PAGE 38)

Apparent symmetry about . 2; 2/. This can be confirmed by calculating shifting the graph right by 2 (replace x with x 2) and then down 2 (subtract 2). The result is 5x=.1 C x 2 /, which is odd.

50. y yD

3 2

2

2

2x C x 2x C x 2

53.

1

-5

-4

-3

-2

-1

1

2

3

4

Section P.5 Combining Functions to Make New Functions (page 38)

Apparent symmetry about x D 1. This can be confirmed by calculating f .2 x/, which turns out to be equal to f .x/.

1.

51. y 4 yDx 1 x 1 x 2

3

yD

2 1 -2

-1

1

2

3

4

-1

5

xC3

2.

Fig. P.4-51 Apparent symmetry about .2; 1/, and about the lines y D x 1 and y D 3 x. These can be confirmed by noting that f .x/ D 1 C

1

x 2 so the graph is that of 1=x shifted right 2 units and up one. yD

2x 2 C 3x C 4x C 5

y

x2

p f .x/ D x, g.x/ D x 1. D.f / D R, D.g/ D Œ1; 1/. D.f C g/ D D.f g/ D D.fg/ D D.g=f / D Œ1; 1/, D.f =g/ D .1; 1/. p .f C g/.x/ D x C x 1 p .f g/.x/ D x x 1 p .fg/.x/ D x x 1 p .f =g/.x/ D x= x 1 p .g=f /.x/ D . 1 x/=x

x

6

yD

-2

52.

f .x/,

x

-1 Fig. P.4-50

-3

If f is both even and odd the f .x/ D f . x/ D so f .x/ D 0 identically.

,

p p f .x/ D 1 x, g.x/ D 1 C x. D.f / D . 1; 1, D.g/ D Œ 1; 1/. D.f C g/ D D.f g/ D D.fg/ D Œ 1; 1, D.f =g/ D . 1;p1, D.g=fp/ D Œ 1; 1/. .f C g/.x/ D 1 x C 1 C x p p .f g/.x/ D 1 x 1Cx p 2 .fg/.x/ D 1 x p .f =g/.x/ D .1 x/=.1 C x/ p .g=f /.x/ D .1 C x/=.1 x/

3. y

5 4

yDx

3

x2

x

2 yDx

1 -7

-6

-5

-4

-3

-2

-1

1

2

x

-1 -2

yD

x2

Fig. P.4-52

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13

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SECTION P.5 (PAGE 38)

ADAMS and ESSEX: CALCULUS 9

4.

8.

y yD

x 1

-2

-1

x

1 y D x3

x

f .x/ D 2=x, g.x/ D x=.1 x/. f ı f .x/ D 2=.2=x/ D xI D.f ı f / D fx W x ¤ 0g f ı g.x/ D 2=.x=.1 x// D 2.1 x/=xI D.f ı g/ D fx W x ¤ 0; 1g g ı f .x/ D .2=x/=.1 .2=x// D 2=.x 2/I D.g ı f / D fx W x ¤ 0; 2g g ı g.x/ D .x=.1 x//=.1 .x=.1 x/// D x=.1 2x/I D.g ı g/ D fx W x ¤ 1=2; 1g

-1 y D x3

-2

9.

5. y

y D x C jxj

y D jxj

p f .x/ D 1=.1 x/, g.x/ D x 1. f ı f .x/ D 1=.1 .1=.1 x/// D .x 1/=xI D.f ı f / D fx W x ¤ 0; 1g p x 1/I f ı g.x/ D 1=.1 D.f ı g/ D fx W x  1; x ¤ 2g p p g ı f .x/ D .1=.1 x// 1 D x=.1 x/I D.g ı f / D Œ0; 1/ q p g ı g.x/ D x 1 1I D.g ı g/ D Œ2; 1/

y D x D jxj x

yDx

6. y 4

y D jxj C jx

3

2j

y D jxj

2

f .x/ y D jx

1 -2

-1

10. f .x/ D .x C 1/=.x 1/ D 1 C 2=.x 1/, g.x/ D sgn .x/. f ı f .x/ D 1 C 2=.1 C .2=.x 1/ 1// D xI D.f ı f / D fx W x ¤ 1g sgn x C 1 f ı g.x/ D D 0I D.f ı g/ D . 1; 0/ sgn x 1   n xC1 1 if x < 1 or x > 1 g ı f .x/ D sgn D I 1 if 1 < x < 1 x 1 D.g ı f / D fx W x ¤ 1; 1g g ı g.x/ D sgn .sgn .x// D sgn .x/I D.g ı g/ D fx W x ¤ 0g

1

2

3

4

2j

5

11. 12. 13. 14. 15. 16.

x

-1

7.

x

2

xp 4 x 2x 3 C 3 .x C 1/=x 1=.x C 1/2

g.x/

f ı g.x/

xC1 xC4 x2 x 1=3 1=.x 1/ x 1

.x C 1/2 x jxj 2x C 3 x 1=x 2

f .x/ D x C 5, g.x/ D x 2 3. f ı g.0/ D f . 3/ D 2; g.f .0// D g.5/ D 22 f .g.x// D f .x 2

3/ D x 2 C 2

g ı f .x/ D g.f .x// D g.x C 5/ D .x C 5/2 f ı f . 5/ D f .0/ D 5; g.g.2// D g.1/ D f .f .x// D f .x C 5/ D x C 10 g ı g.x/ D g.g.x// D .x 2

14

3/2

3

3 2

17.

p y D x. p y D 2 C px: previous graph is raised 2 units. y D 2 C 3p C x: previous graph is shiftend left 3 units. y D 1=.2 C 3 C x/: previous graph turned upside down and shrunk vertically.

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION P.5 (PAGE 38)

y

21. y

y D2C y D2C

p

xC3

y D 1=.2 C

p

p

.1=2;1/ yDf .2x/

x

yD

x C 3/

x

1

p

x 22. y

x yDf .x=3/

Fig. P.5-17

18. yD

p

1

23.

y

2x

y

y D 2x yD p

y D 2x

1 1

6 x

3

. 2;2/

1 yD1Cf . x=2/

2x

x

x yD p

24.

1 1

2x

y

1

yD2f ..x 1/=2/

yD1

2x

Fig. P.5-18

1

5

x

19. y

25. y .1;2/

y D f .x/ .1; 1/

yD2f .x/

82

x

2

x

26.

20.

-2y

y

y D g.x/ .1; 1/ 2 x yD .1=2/f .x/

x

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15

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SECTION P.5 (PAGE 38)

27.

ADAMS and ESSEX: CALCULUS 9

F .x/ D Ax C B (a) F ı F .x/ D F .x/ ) A.Ax C B/ C B D Ax C B ) AŒ.A 1/x C B D 0 Thus, either A D 0 or A D 1 and B D 0. (b) F ı F .x/ D x ) A.Ax C B/ C B D x ) .A2 1/x C .A C 1/B D 0 Thus, either A D 1 or A D 1 and B D 0

28. bxc D 0 for 0  x < 1; dxe D 0 for

35.

a)

Let E.x/ D 12 Œf .x/ C f . x/. Then E. x/ D 21 Œf . x/ C f .x/ D E.x/. Hence, E.x/ is even. Let O.x/ D 12 Œf .x/ f . x/. Then O. x/ D 12 Œf . x/ f .x/ D O.x/ and O.x/ is odd. E.x/ C O.x/

D 12 Œf .x/ C f . x/ C 12 Œf .x/

1  x < 0.

f . x/

D f .x/:

29. bxc D dxe for all integers x.

Hence, f .x/ is the sum of an even function and an odd function.

30. d xe D bxc is true for all real x; if x D n C y where n is an integer and 0  y < 1, then x D n y, so that d xe D n and bxc D n. 31. y y D x bxc

b) If f .x/ D E1 .x/ C O1 .x/ where E1 is even and O1 is odd, then E1 .x/ C O1 .x/ D f .x/ D E.x/ C O.x/: Thus E1 .x/ E.x/ D O.x/ O1 .x/. The left side of this equation is an even function and the right side is an odd function. Hence both sides are both even and odd, and are therefore identically 0 by Exercise 36. Hence E1 D E and O1 D O. This shows that f can be written in only one way as the sum of an even function and an odd function.

x 32. f .x/ is called the integer part of x because jf .x/j is the largest integer that does not exceed x; i.e. jxj D jf .x/j C y, where 0  y < 1. y

Section P.6 Polynomials and Rational Functions (page 45) x y D f .x/

1.

x 2 7x C 10 D .x C 5/.x C 2/ The roots are 5 and 2.

2.

x 2 3x 10 D .x 5/.x C 2/ The roots are 5 and 2.

34. f even , f . x/ D f .x/ f odd , f . x/ D f .x/ f even and odd ) f .x/ D ) f .x/ D 0

16

f .x/ ) 2f .x/ D 0

4

8

D

1 ˙ i.

If x C 2x C 2 D 0, then x D 2 The roots are 1 C i and 1 i . x 2 C 2x C 2 D .x C 1 i /.x C 1 C i /.

4.

Rather than use the quadratic formula this time, let us complete the square. x2

6x C 13 D x 2 D .x D .x

f ı g. x/ D f .g. x// D f . g.x// D f .g.x// D f ı g.x/ .fg/. x/ D f . x/g. x/ D f .x/Œ g.x/ D f .x/g.x/ D .fg/.x/: The others are similar.

p

3. Fig. P.5-32 33. If f is even and g is odd, then: f 2 , g 2 , f ı g, g ı f , and f ı f are all even. fg, f =g, g=f , and g ı g are odd, and f C g is neither even nor odd. Here are two typical verifications:



2

The roots are 3 C 2i and 3

6x C 9 C 4

3/2 C 22 3 2i /.x

3 C 2i /:

2i .

5.

16x 4 8x 2 C 1 D .4x 2 1/2 D .2x 1/2 .2x C 1/2 . There are two double roots: 1=2 and 1=2.

6.

x 4 C 6x 3 C 9x 2 D x 2 .x 2 C 6x C 9/ D x 2 .x C 3/2 . There are two double roots, 0 and 3.

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INSTRUCTOR’S SOLUTIONS MANUAL

7.

SECTION P.6 (PAGE 45)

x 3 C 1 D .x C 1/.x 2 x C 1/. One root is 1. The other two are the solutions of x 2 x C 1 D 0, namely xD



p

1

4

p 3 1 ˙ i: 2 2

D

2

15.

The denominator is x 3 C x 2 D x 2 .x C 1/ which is zero only if x D 0 or x D 1. Thus the rational function is defined for all real numbers except 0 and 1.

16.

The denominator is x 2 Cx 1, which is a quadratic polynomial whose roots can p be found with the quadratic formula. They are x D . 1 ˙ 1 C 4/=2. Hence the given rational p 5/=2 function is p defined for all real numbers except . 1 and . 1 C 5/=2.

We have p

3 i 2

1 2

x 3 C 1 D .x C 1/ x

8. x 4 1 D .x 2 1/.x 2 C 1/ D .x The roots are 1, 1, i , and i .

!

p ! 1 3 C i : 2 2

x

1/.x C 1/.x

10.

x

x

4

16x C 16 D .x

The roots are 1, 2, 11.

1/.x

4

2, 2i , and

2i .

x 5 C x 3 C 8x 2 C 8 D .x 2 C 1/.x 3 C 8/

i /.x C i /.x 2

D .x C 2/.x

18.

16/

1/.x 2 4/.x 4 C 4/ 1/.x 2/.x C 2/.x

D .x D .x

2i /.x C 2i /:

19.

p p 20. x Cx C8x C8 D .xC2/.x i /.xCi /.x aC 3 i /.x a 3 i /: 12.

x9

3

4x 7

2

x 6 C 4x 4 D x 4 .x 5 4

D x .x

x2

3

1/.x

4

D x .x

4x 3 C 4/

2

4/

2/.x C 2/.x 2 C x C 1/:

1/.x

Seven of the nine roots are: 0 (with multiplicity 4), 1, 2, and 2. The other two roots are solutions of x 2 C x C 1 D 0, namely xD



p 2

1

4

D

The required factorization of x 9 x 4 .x 1/.x 2/.xC2/ x

Following the method of Example 6, we calculate .x 2 bxCa2 /.x 2 CbxCa2 / D x 4 Ca4 C.2a2 b 2 /x 2 D x 4 Cx 2 C1

! 3 i : 2

p

13. The denominator is x 2 C 2x C 2 D .x C 1/2 C 1 which is never 0. Thus the rational function is defined for all real numbers. 14.

x4 C x2 x.x 3 C x 2 C 1/ x 3 x C x 2 D 2 Cx C1 x3 C x2 C 1 3 .x C x 2 C 1/ C x 2 C 1 x C x 2 DxC x3 C x2 C 1 2 2x xC1 : D x 1C 3 x C x2 C 1

x3

22.

provided a D 1 and b 2 D 1 C 2a2 D 1, so b D ˙1. Thus P .x/ D .x 2 x C 1/.x 2 C x C 1/.

x 6 C 4x 4 is 1 2

x3 x 3 C 2x 2 C 3x 2x 2 3x D C 2x C 3 x 2 C 2x C 3 x.x 2 C 2x C 3/ 2x 2 3x D x 2 C 2x C 3 2.x 2 C 2x C 3/ 4x 6 C 3x Dx x 2 C 2x C 3 xC6 Dx 2C 2 : x C 2x C 3

4 2 As in Example p 6, we wantpa D 4, so a D 2 and a D 2, b D ˙ 2a D ˙2. Thus P .x/ D .x 2 2x C 2/.x 2 C 2x C 2/.

3 1 ˙ i: 2 2

p ! 1 3 C i x 2 2

x2

3

21.

p

4x 7

1 x 3 2x C 2x 1 D 2 x2 2 x.x 2 2/ C 2x 1 D x2 2 2x 1 DxC 2 : x 2

x 2 C 5x C 3 5x x2 D x 2 C 5x C 3 x 2 C 5x C 3 5x 3 : D1C 2 x C 5x C 3

2x C 4/

Three of the five roots are 2, i and i . The remain2 ing two are 2x C 4 D 0, namely p solutions of x p 2 ˙ 4 16 xD D 1 ˙ 3 i . We have 2 5

x3 x2

i /.x C i /.

9. x 6 3x 4 C 3x 2 1 D .x 2 1/3 D .x 1/3 .x C 1/3 . The roots are 1 and 1, each with multiplicity 3. 5

17.

The denominator is x 3 x D x.x 1/.x C 1/ which is zero if x D 0, 1, or 1. Thus the rational function is defined for all real numbers except 0, 1, and 1.

23.

24.

Let P .x/ D an x n C an 1 x n 1 C    C a1 x C a0 , where n  1. By the Factor Theorem, x 1 is a factor of P .x/ if and only if P .1/ D 0, that is, if and only if an C an 1 C    C a1 C a0 D 0.

Let P .x/ D an x n C an 1 x n 1 C    C a1 x C a0 , where n  1. By the Factor Theorem, x C 1 is a factor of P .x/ if and only if P . 1/ D 0, that is, if and only if a0 a1 C a2 a3 C    C . 1/n an D 0. This condition says that the sum of the coefficients of even powers is equal to the sum of coefficients of odd powers.

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ADAMS and ESSEX: CALCULUS 9

25. Let P .x/ D an x n C an 1 x n 1 C    C a1 x C a0 , where the coefficients ak , 0  k  n are all real numbers, so that ak D ak . Using the facts about conjugates of sums and products mentioned in the statement of the problem, we see that if z D x C iy, where x and y are real, then P .z/ D an z n C an n

D an z C an D P .z/:

1z

n 1

1z

n 1

4.

sin

5.

cos

6.

sin

C    C a1 z C a0

C    C a1 z C a0

If z is a root of P , then P .z/ D P .z/ D 0 D 0, and z is also a root of P . 26. By the previous exercise, z D u iv is also a root of P . Therefore P .x/ has two linear factors x u iv and x u C iv. The product of these factors is the real quadratic factor .x u/2 i 2 v 2 D x 2 2ux C u2 C v 2 , which must also be a factor of P .x/. 27.

By the previous exercise P .x/ D 2ux C u2 C v 2 .x

x2

u

P .x/ iv/.x

u C iv/

D Q1 .x/;

where Q1 , being a quotient of two polynomials with real coefficients, must also have real coefficients. If z D u C iv is a root of P having multiplicity m > 1, then it must also be a root of Q1 (of multiplicity m 1), and so, therefore, z must be a root of Q1 , as must be the real quadratic x 2 2ux C u2 C v 2 . Thus .x 2

P .x/ D 2 2ux C u2 C v 2 /2 x

Q1 .x/ D Q2 .x/; 2ux C u2 C v 2

where Q2 is a polynomial with real coefficients. We can continue in this way until we get

.x 2

7.

P .x/ D Qm .x/; 2ux C u2 C v 2 /m



7 12



1.

cos

2. tan

3. sin

18



3 4



 D cos 

3 D 4

tan

 2 D sin  3

 D 4

3 D 4

cos

 D 4

 11 D sin 12 12  D sin 3 4     cos sin D sin cos 3 4 3 4 p !     3 1 1 1 D p p 2 2 2 2 p 3 1 D p 2 2

  cos. C x/ D cos 2 . x/   D cos . x/ D cos.

8.

sin.2

9.

sin

10.



x/ D

3 2

x



3 Cx cos 2

!

x/ D

cos x

sin x     D sin  x 2   D sin x  2  D sin x 2 D cos x D cos

3 cos x 2

sin

3 sin x 2

D . 1/. sin x/ D sin x

1 p 2 11.

1

C

  2  5 D cos 12 3 4 2  2  D cos cos C sin sin 3 4 3 4 p !     1 3 1 1 C D p p 2 2 2 2 p 3 1 D p 2 2

where Qm no longer has z (or z) as a root. Thus z and z must have the same multiplicity as roots of P .

Section P.7 The Trigonometric Functions (page 57)



 4 3     D sin cos C cos sin 4 3 p 4 3 p 1 1 3 1 1C 3 D p p Cp D 22 2 2 2 2

D sin

cos x sin x C cos x sin x sin2 x C cos2 x D cos x sin x 1 D cos x sin x

tan x C cot x D

p  3  D sin D 3 3 2

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INSTRUCTOR’S SOLUTIONS MANUAL

12.

 cos x sin x tan x cot x cos x sin x  D  cos x sin x tan x C cot x C cos x sin x ! 2 sin x cos2 x cos x sin x ! D sin2 x C cos2 x cos x sin x 

D sin2 x 13.

cos4 x

sin4 x D .cos2 x

16.

17.



.cos x sin x/2 cos x sin x D cos x C sin x .cos x C sin x/.cos x sin x/ cos2 x 2 sin x cos x C sin2 x D cos2 x sin2 x 1 sin.2x/ D cos.2x/ D sec.2x/ tan.2x/

D 2 sin x cos x C sin x.1 D 3 sin x

sin

x has period 4. 2 y

sin2 x D cos.2x/

sin 3x D sin.2x C x/ D sin 2x cos x C cos 2x sin x

1



Fig. P.7-20

21.

sin x has period 2. y

y D sin.x/

1

1

D 2 cos3 x

D 4 cos3 x

2

sin x/ C sin x

1

Fig. P.7-21

22.

cos

x has period 4. 2 y 1 1

x

1

Fig. P.7-22 2

2 sin3 x

23. y

4 sin x

2

2.1

5 3

3

cos x

4 x

3

2 sin x/

2

1/ cos x

2 x

1

cos 3x D cos.2x C x/ D cos 2x cos x sin 2x sin x D .2 cos2 x

2 x

Fig. P.7-19

sin2 x/.cos2 x C sin2 x/

2

18.

=2

.1 cos x/.1 C cos x/ D 1 cos2 x D sin2 x implies 1 cos x sin x D . Now sin x 1 C cos x   x 1 cos 2 1 cos x  x 2 D sin x sin 2  2  x  1 1 2 sin2 2 D x x 2 sin cos 2 2 x sin 2 D tan x D x 2 cos 2 x  2 sin2 x  1 cos x  2x  D tan2 D 1 C cos x 2 2 cos2 2

D 2 sin x.1

y D cos.2x/

1

20.

D cos x

15.

y

cos2 x

2

14.

SECTION P.7 (PAGE 57)

 y D 2 cos x

 3

1 



2 sin2 x cos x cos2 x/ cos x

3 cos x

x -1 -2 -3

19. cos 2x has period .

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SECTION P.7 (PAGE 57)

ADAMS and ESSEX: CALCULUS 9

24.

  y D 1 C sin x C 4

y 2

29.

sin x D cos x D

1 ; 2p

 0 for

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INSTRUCTOR’S SOLUTIONS MANUAL

Section 1.4 Continuity 1.

SECTION 1.4 (PAGE 87)

(page 87)

8.

g is continuous at x D 2, discontinuous at x D 1; 0; 1, and 2. It is left continuous at x D 0 and right continuous at x D 1. y .1; 2/ 2 y D g.x/

. 1; 1/

-2

1

lim f .x/ D

x! 1

1

2

x

Fig. 1.4-1 2. g has removable discontinuities at x D 1 and x D 2. Redefine g. 1/ D 1 and g.2/ D 0 to make g continuous at those points.

D f . 1/ D

4. Function f is discontinuous at x D 1; 2; 3; 4, and 5. f is left continuous at x D 4 and right continuous at x D 2 and x D 5. y

lim f .x/:

x! 1C

12. C.t / is discontinuous only at the integers. It is continuous on the left at the integers, but not on the right. 13.

1 15.

4

5

6

x 16.

-1

Fig. 1.4-4 5. f cannot be redefined at x D 1 to become continuous there because limx!1 f .x/ .D 1/ does not exist. (1 is not a real number.) 6. sgn x is not defined at x D 0, so cannot be either continuous or discontinuous there. (Functions can be continuous or discontinuous only at points in their domains!)  x if x < 0 is continuous everywhere on the 7. f .x/ D x 2 if x  0 real line, even at x D 0 where its left and right limits are both 0, which is f .0/.

The least integer function dxe is continuous everywhere on

right continuous.

2

3

lim x 2 D

x! 1C

R except at the integers, where it is left continuous but not

14.

y D f .x/

2

1¤1

 2 if x ¤ 0 is continuous everywhere except f .x/ D 1=x 0 if x D 0 at x D 0, where it is neither left nor right continuous since it does not have a real limit there.  2 if x  1 is continuous everywhere ex10. f .x/ D x 0:987 if x > 1 cept at x D 1, where it is left continuous but not right continuous because 0:987 ¤ 1. Close, as they say, but no cigar. 11.

3. g has no absolute maximum value on Œ 2; 2. It takes on every positive real value less than 2, but does not take the value 2. It has absolute minimum value 0 on that interval, assuming this value at the three points x D 2, x D 1, and x D 1.

1

lim x D

x! 1

9.

-1

3



x if x < 1 is continuous everywhere on the x 2 if x  1 real line except at x D 1 where it is right continuous, but not left continuous.

f .x/ D

17.

x2 4 Since D x C 2 for x ¤ 2, we can define the x 2 function to be 2 C 2 D 4 at x D 2 to make it continuous there. The continuous extension is x C 2.

1 C t3 .1 C t /.1 t C t 2 / 1 t C t2 D D for 2 1 t .1 C t /.1 t / 1 t t ¤ 1, we can define the function to be 3=2 at t D 1 to make it continuous there. The continuous extension is 1 t C t2 . 1 t Since

.t 2/.t 3/ t 2 t 2 5t C 6 D D for t ¤ 3, 2 t t 6 .t C 2/.t 3/ t C2 we can define the function to be 1=5 at t D 3 to make it t 2 continuous there. The continuous extension is . t C2 Since p p p xC 2 x2 2 .x 2/.x C 2/ p p D p D x4 4 2/.x C 2/.x 2 C 2/ .x C 2/.x 2 C 2/ p.x for x p ¤ 2, we can define the function to be 1=4 at there. The continuous x D 2 to make it continuous p xC 2 extension is p . (Note: cancelling the .x C 2/.x 2 C 2/ p 2 factors provides a further continuous extension to xC p 2. xD Since

limx!2C f .x/ D k 4 and limx!2 f .x/ D 4 D f .2/. Thus f will be continuous at x D 2 if k 4 D 4, that is, if k D 8.

18. limx!3 g.x/ D 3 m and limx!3C g.x/ D 1 3m D g.3/. Thus g will be continuous at x D 3 if 3 m D 1 3m, that is, if m D 1.

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SECTION 1.4 (PAGE 87)

ADAMS and ESSEX: CALCULUS 9

19. x 2 has no maximum value on 1 < x < 1; it takes all positive real values less than 1, but it does not take the value 1. It does have a minimum value, namely 0 taken on at x D 0. 20. The Max-Min Theorem says that a continuous function defined on a closed, finite interval must have maximum and minimum values. It does not say that other functions cannot have such values. The Heaviside function is not continuous on Œ 1; 1 (because it is discontinuous at x D 0), but it still has maximum and minimum values. Do not confuse a theorem with its converse. 21.

Let the numbers be x and y, where x  0, y  0, and x C y D 8. If P is the product of the numbers, then P D xy D x.8

x/ D 8x

x 2 D 16

.x

f .x/ D

29.

f .x/ D x 3 C x 1, f .0/ D 1, f .1/ D 1. Since f is continuous and changes sign between 0 and 1, it must be zero at some point between 0 and 1 by IVT.

30.

f .x/ D x 3 15x C 1 is continuous everywhere. f . 4/ D 3; f . 3/ D 19; f .1/ D 13; f .4/ D 5: Because of the sign changes f has a zero between 4 and 3, another zero between 3 and 1, and another between 1 and 4.

31.

F .x/ D .x a/2 .x b/2 C x. Without loss of generality, we can assume that a < b. Being a polynomial, F is continuous on Œa; b. Also F .a/ D a and F .b/ D b. Since a < 21 .a C b/ < b, the Intermediate-Value Theorem guarantees that there is an x in .a; b/ such that F .x/ D .a C b/=2.

32.

Let g.x/ D f .x/ x. Since 0  f .x/  1 if 0  x  1, therefore, g.0/  0 and g.1/  0. If g.0/ D 0 let c D 0, or if g.1/ D 0 let c D 1. (In either case f .c/ D c.) Otherwise, g.0/ > 0 and g.1/ < 0, and, by IVT, there exists c in .0; 1/ such that g.c/ D 0, i.e., f .c/ D c.

33.

The domain of an even function is symmetric about the y-axis. Since f is continuous on the right at x D 0, therefore it must be defined on an interval Œ0; h for some h > 0. Being even, f must therefore be defined on Œ h; h. If x D y, then

4/2 :

Therefore P  16, so P is bounded. Clearly P D 16 if x D y D 4, so the largest value of P is 16. 22. Let the numbers be x and y, where x  0, y  0, and x C y D 8. If S is the sum of their squares then S D x 2 C y 2 D x 2 C .8 D 2x 2

x/2 4/2 C 32:

16x C 64 D 2.x

Since 0  x  8, the maximum value of S occurs at x D 0 or x D 8, and is 64. The minimum value occurs at x D 4 and is 32.

23. Since T D 100 30x C 3x 2 D 3.x 5/2 C 25, T will be minimum when x D 5. Five programmers should be assigned, and the project will be completed in 25 days. 24.

lim f .x/ D lim f . y/ D lim f .y/ D f .0/:

x!0

If x desks are shipped, the shipping cost per desk is C D

245x

30x 2 C x 3 D x2 x D .x

34.

This cost is minimized if x D 15. The manufacturer should send 15 desks in each shipment, and the shipping cost will then be $20 per desk. x2

x!0C

x!0

x, we obtain

t!0C

D

t!0C

f .t /

f .0/ D f . 0/ D f .0/:

Therefore f is continuous at 0 and f .0/ D 0.

.x 1/.x C 1/ x2 1 D f .x/ D 2 x 4 .x 2/.x C 2/ f D 0 at x D ˙1. f is not defined at x D ˙2. f .x/ > 0 on . 1; 2/, . 1; 1/, and .2; 1/. f .x/ < 0 on . 2; 1/ and .1; 2/.

32

f odd , f . x/ D f .x/ f continuous on the right , lim f .x/ D f .0/

Therefore, letting t D

.x

26. f .x/ D x 2 C 4x C 3 D .x C 1/.x C 3/ f .x/ > 0 on . 1; 3/ and . 1; 1/ f .x/ < 0 on . 3; 1/. 27.

y!0C

lim f .x/ D lim f . t / D lim

1/.x C 1/ 25. f .x/ D D x x f D 0 at x D ˙1. f is not defined at 0. f .x/ > 0 on . 1; 0/ and .1; 1/. f .x/ < 0 on . 1; 1/ and .0; 1/. 1

y!0C

Thus, f is continuous on the left at x D 0. Being continuous on both sides, it is therefore continuous.

30x C 245 15/2 C 20:

.x C 2/.x 1/ x2 C x 2 D 3 x x3 f .x/ > 0 on . 2; 0/ and .1; 1/ f .x/ < 0 on . 1; 2/ and .0; 1/.

28.

35.

max 1:593 at

0:831, min

0:756 at 0:629

36.

max 0:133 at x D 1:437; min

0:232 at x D

1:805

37. max 10:333 at x D 3; min 4:762 at x D 1:260 38.

max 1:510 at x D 0:465; min 0 at x D 0 and x D 1

39.

root x D 0:682

40.

root x D 0:739

41. roots x D

0:637 and x D 1:410

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42. roots x D

SECTION 1.5 (PAGE 92)

0:7244919590 and x D 1:220744085

43. fsolve gives an approximation to the single real root to 10 significant figures; solve gives the three roots (including a complex conjugate pair) in exact form involving the quan p 1=3 ; evalf(solve) gives approximations tity 108 C 12 69 to the three roots using 10 significant figures for the real and imaginary parts.

Section 1.5 The Formal Definition of Limit (page 92) 1.

We require 39:9  L  40:1. Thus

10. We need 1 0:05  1=.x C 1/  1 C 0:05, or 1:0526  x C 1  0:9524. This will occur if 0:0476  x  0:0526. In this case we can take ı D 0:0476. 11.

x!1

Proof: Let  > 0 be given. Then j.3x C 1/ 4j <  holds if 3jx 1j < , and so if jx 1j < ı D =3. This confirms the limit. 12. To be proved: lim .5 x!2

Let  > 0 be given. p Then jx 2 jx 0j D jxj < ı D .

14.

2. Since 1.2% of 8,000 is 96, we require the edge length x of the cube to satisfy 7904  x 3  8096. It is sufficient that 19:920  x  20:079. The edge of the cube must be within 0.079 cm of 20 cm.

4.

5.

6.

0:02  2x 1  3 C 0:02 3:98  2x  4:02 1:99  x  2:01

2

1 4x 2 D 2. 2x x!1=2 1 Proof: Let  > 0 be given. Then if x ¤ 1=2 we have

provided jx 16.

1  2 C 0:01 x 1 1 x 2:01 1:99 0:5025  x  0:4975

We need 0:03  .3x C 1/ 7  0:03, which is equivalent to 0:01  x 2  0:01 Thus ı D 0:01 will do. p 8. We need 0:01  2x C 3 3  0:01. Thus p 2:99  2x C 3  3:01 8:9401  2x C 3  9:0601 2:97005  x  3:03005 0:02995  x 3  0:03005:

Here ı D 0:02995 will do. 9. We need 8 0:2  x 3  8:2, or 1:9832  x  2:0165. Thus, we need 0:0168  x 2  0:0165. Here ı D 0:0165 will do.

lim

ˇ ˇ 2ˇˇ D j.1 C 2x/ 1 2j

2j D j2x

< ı D =2.

ˇ ˇ 1j D 2 ˇˇx

ˇ 1 ˇˇ 0 be given. For x ¤ 2 we have To be proved:

lim

ˇ 2 ˇ x C 2x ˇ ˇ xC2

7.

2j < 

2j < ı D .

To be proved:

ˇ ˇ 1 4x 2 ˇ ˇ 1 2x

0:01 

3

x 2 D 0. 1 C x2 Proof: Let  > 0 be given. Then ˇ ˇ ˇ ˇ x 2 ˇ D jx 2j  jx ˇ 0 ˇ ˇ 1 C x2 1 C x2

To be proved: lim

provided jx

15.

4 0:1  x 2  4 C 0:1 1:9749  x  2:0024 p 1 0:1  x  1:1 0:81  x  1:21

0j <  holds if

x!2

ı

The temperature should be kept between 12 C and 20 C.

3

To be proved: lim x 2 D 0. x!0

39:9  39:6 C 0:025T  40:1 0:3  0:025T  0:5 12  T  20:

3.

2x/ D 1.

Proof: Let  > 0 be given. Then j.5 2x/ 1j <  holds if j2x 4j < , and so if jx 2j < ı D =2. This confirms the limit. 13.

ı

To be proved: lim .3x C 1/ D 4.

ˇ ˇ . 2/ˇˇ D jx C 2j < 

provided jx C 2j < ı D . This completes the proof.

17.

1 1 D . xC1 2 Proof: Let  > 0 be given. We have ˇ ˇ ˇ ˇ ˇ 1 1 ˇˇ ˇˇ 1 x ˇˇ jx 1j ˇ D ˇ x C 1 2 ˇ ˇ 2.x C 1/ ˇ D 2jx C 1j : To be proved: lim

x!1

If jx 1j < 1, then 0 < x < 2 and 1 < x C 1 < 3, so that jx C 1j > 1. Let ı D min.1; 2/. If jx 1j < ı, then ˇ ˇ ˇ 1 1 ˇˇ 2 jx 1j ˇ ˇ x C 1 2 ˇ D 2jx C 1j < 2 D :

This establishes the required limit.

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SECTION 1.5 (PAGE 92)

ADAMS and ESSEX: CALCULUS 9

1 xC1 D . x2 1 2 Proof: Let  > 0 be given. If x ¤ 1, we have ˇ  ˇ ˇ  ˇ ˇ xC1 jx C 1j 1 ˇˇ ˇˇ 1 1 ˇˇ ˇ D D : ˇ x2 1 2 ˇ ˇx 1 2 ˇ 2jx 1j

18. To be proved:

lim

If jx C 1j < 1, then 2 < x < 0, so 3 < x 1 < 1 and jx 1j > 1. Ler ı D min.1; 2/. If 0 < jx . 1/j < ı then jx 1j > 1 and jx C 1j < 2. Thus ˇ  ˇ ˇ xC1 1 ˇˇ jx C 1j 2 ˇ D < D : ˇ x2 1 2 ˇ 2jx 1j 2

This completes the required proof. p 19. To be proved: lim x D 1.

Proof: Let  > 0 be given. We have ˇ ˇ ˇ x 1 ˇ p ˇ  jx j x 1j D ˇˇ p x C 1ˇ

26.

28.

3

20. To be proved: lim x D 8. x!2

Proof: Let  > 0 be given. We have jx 3 8j D jx 2jjx 2 C2xC4j. If jx 2j < 1, then 1 < x < 3 and x 2 < 9. Therefore jx 2 C 2x C 4j  9 C 2  3 C 4 D 19. If jx 2j < ı D min.1; =19/, then jx 3

  19 D : 2jjx 2 C 2x C 4j < 19

8j D jx

29.

implies jf .x/

ı x 1 > 1=B, be given. We have x 1 that is, if 1 ı < x < 1, where ı D 1=B:. This completes the proof. To be proved: limx!1 p

23. We say that limx!a f .x/ D 1 if the following condition holds: for every number B > 0 there exists a number ı > 0, depending on B, such that 0 < jx 24.

aj < ı

implies f .x/
0 there exists a number R > 0, depending on B, such that x>R

34

implies f .x/ > B:

1 x2

C1

D 0. Proof: Let  > 0

provided x > R, where R D 1=. This completes the proof. 30.

Lj < :

implies f .x/ > B:

ˇ ˇ ˇ ˇ 1 ˇp 1 ˇD p 1 < 0 there exists a number R > 0, depending on , such that

ı 0, depending on , such that a

B:

1 To be proved: limx!1C D 1. Proof: Let B > 0 x 1 1 > B if 0 < x 1 < 1=B, that be given. We have x 1 is, if 1 < x < 1 C ı, where ı D 1=B. This completes the proof.

This completes the proof. 21.

implies f .x/
0 there exists a number ı > 0, depending on B, such that a

1j < 

1j < ı D . This completes the proof.

We say that limx!aC f .x/ D 1 if the following condition holds: for every number B > 0 there exists a number ı > 0, depending on R, such that a B if x > R where R D B . This completes the proof. To be proved: if lim f .x/ D L and lim f .x/ D M , then x!a x!a L D M. Proof: Suppose L ¤ M . Let  D jL M j=3. Then  > 0. Since lim f .x/ D L, there exists ı1 > 0 such that x!a

jf .x/ Lj <  if jx aj < ı1 . Since lim f .x/ D M , there x!a

exists ı2 > 0 such that jf .x/ M j <  if jx Let ı D min.ı1 ; ı2 /. If jx aj < ı, then 3 D jL

aj < ı2 .

M j D j.f .x/ M / C .L f .x/j  jf .x/ M j C jf .x/ Lj <  C  D 2:

This implies that 3 < 2, a contradiction. Thus the original assumption that L ¤ M must be incorrect. Therefore L D M.

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INSTRUCTOR’S SOLUTIONS MANUAL

REVIEW EXERCISES 1 (PAGE 93)

32. To be proved: if lim g.x/ D M , then there exists ı > 0

This completes the proof.

x!a

such that if 0 < jx aj < ı, then jg.x/j < 1 C jM j. Proof: Taking  D 1 in the definition of limit, we obtain a number ı > 0 such that if 0 < jx aj < ı, then jg.x/ M j < 1. It follows from this latter inequality that

36.

To be proved: if lim f .x/ D L and lim f .x/ D M ¤ 0, x!a

x!a

L f .x/ D . x!a g.x/ M Proof: By Exercises 33 and 35 we have

then lim

jg.x/j D j.g.x/ M /CM j  jG.x/ M jCjM j < 1CjM j: lim

x!a

f .x/ 1 1 L D lim f .x/  DL D : x!a g.x/ g.x/ M M

33. To be proved: if lim f .x/ D L and lim g.x/ D M , then x!a

x!a

lim f .x/g.x/ D LM .

x!a

37. To be proved: if f is continuous at L and lim g.x/ D L,

Proof: Let  > 0 be given. Since lim f .x/ D L, there

x!c

x!a

then lim f .g.x// D f .L/.

exists ı1 > 0 such that jf .x/ Lj < =.2.1 C jM j// if 0 < jx aj < ı1 . Since lim g.x/ D M , there ex-

x!c

Proof: Let  > 0 be given. Since f is continuous at L, there exists a number > 0 such that if jy Lj < , then jf .y/ f .L/j < . Since limx!c g.x/ D L, there exists ı > 0 such that if 0 < jx cj < ı, then jg.x/ Lj < . Taking y D g.x/, it follows that if 0 < jx cj < ı, then jf .g.x// f .L/j < , so that limx!c f .g.x// D f .L/.

x!a

ists ı2 > 0 such that jg.x/ M j < =.2.1 C jLj// if 0 < jx aj < ı2 . By Exercise 32, there exists ı3 > 0 such that jg.x/j < 1 C jM j if 0 < jx aj < ı3 . Let ı D min.ı1 ; ı2 ; ı3 /. If jx aj < ı, then jf .x/g.x/

LM D jf .x/g.x/ Lg.x/ C Lg.x/ LM j D j.f .x/ L/g.x/ C L.g.x/ M /j  j.f .x/ L/g.x/j C jL.g.x/ M /j D jf .x/ Ljjg.x/j C jLjjg.x/ M j   < .1 C jM j/ C jLj 2.1 C jM j/ 2.1 C jLj/    C D : 2 2

38.

Thus lim f .x/g.x/ D LM . x!a

34. To be proved: if lim g.x/ D M where M ¤ 0, then

jg.x/

x!a

there exists ı > 0 such that if 0 < jx aj < ı, then jg.x/j > jM j=2. Proof: By the definition of limit, there exists ı > 0 such that if 0 < jx aj < ı, then jg.x/ M j < jM j=2 (since jM j=2 is a positive number). This latter inequality implies that jM j D jg.x/C.M g.x//j  jg.x/jCjg.x/ M j < jg.x/jC

It follows that jg.x/j > jM j required.

jM j : 2

Lj D jg.x/  jg.x/  jh.x/ D jh.x/  jh.x/   < C 3 3

Review Exercises 1 (page 93) 1.

The average rate of change of x 3 over Œ1; 3 is 33 3

x!a

2

there exists ı1 > 0 such that jg.x/ M j < jM j =2 if 0 < jx aj < ı1 . By Exercise 34, there exists ı2 > 0 such that jg.x/j > jM j=2 if 0 < jx aj < ı3 . Let ı D min.ı1 ; ı2 /. If 0 < jx aj < ı, then ˇ ˇ ˇ 1 1 ˇˇ jM g.x/j jM j2 2 ˇ D < D : ˇ g.x/ M ˇ jM jjg.x/j 2 jM j2

f .x/ C f .x/ Lj f .x/j C jf .x/ Lj f .x/j C jf .x/ Lj L C L f .x/j C jf .x/ Lj Lj C jf .x/ Lj C jf .x/ Lj  C D : 3

Thus limx!a g.x/ D L.

.jM j=2/ D jM j=2, as

35. To be proved: if lim g.x/ D M where M ¤ 0, then x!a 1 1 D . lim x!a g.x/ M Proof: Let  > 0 be given. Since lim g.x/ D M ¤ 0,

To be proved: if f .x/  g.x/  h.x/ in an open interval containing x D a (say, for a ı1 < x < a C ı1 , where ı1 > 0), and if limx!a f .x/ D limx!a h.x/ D L, then also limx!a g.x/ D L. Proof: Let  > 0 be given. Since limx!a f .x/ D L, there exists ı2 > 0 such that if 0 < jx aj < ı2 , then jf .x/ Lj < =3. Since limx!a h.x/ D L, there exists ı3 > 0 such that if 0 < jx aj < ı3 , then jh.x/ Lj < =3. Let ı D min.ı1 ; ı2 ; ı3 /. If 0 < jx aj < ı, then

2.

13 26 D D 13: 1 2

The average rate of change of 1=x over Œ 2; 1 is .1=. 1// .1=. 2// D 1 . 2/

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1=2 D 1

1 : 2

35

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REVIEW EXERCISES 1 (PAGE 93)

ADAMS and ESSEX: CALCULUS 9

3. The rate of change of x 3 at x D 2 is lim

h!0

.2 C h/3 h

23

8 C 12h C 6h2 C h3 8 h h!0 D lim .12 C 6h C h2 / D 12:

18.

h!0

19.

lim

h!0



1 3=2



5.

lim .x

4x C 7/ D 1

x!1

22 x2 D D 6. lim 2 x!2 1 x 1 22

3=2 is

20. 21.

23.

25.

lim

9.

10.

2/.x C 2/ xC2 D lim D x!2 x 2/.x 3/ 3

x2

4 xC2 .x 2/.x C 2/ D lim D lim x!2 x 2 x!2 x x!2 4x C 4 .x 2/2 2 does not exist. The denominator approaches 0 (from both sides) while the numerator does not. lim

x2

lim

x2

x!2

xC2 4 D lim D x!2 x 4x C 4 2

1

lim

x! 2C

26.

4 27.

lim p

x2

h!0

15.

lim

h x C 3h

p

x!0C

16.

lim

x!0

p

p

x

x

29.

36

x4

x!1 x 2

lim p

4

D lim

x!1

1 x

lim p

D1

x2

1 D p D2 1=4

1 x

lim sin x does not exist; sin x takes the values

1 and 1

in any interval .R; 1/, and limits, if they exist, must be unique. cos x D 0 by the squeeze theorem, since lim x!1 x 1 cos x 1   for all x > 0 x x x and limx!1 . 1=x/ D limx!1 .1=x/ D 0. 1 D 0 by the squeeze theorem, since x 1 jxj  x sin  jxj for all x ¤ 0 x and limx!0 . jxj/ D limx!0 jxj D 0. lim x sin

1 does not exist; sin.1=x 2 / takes the values 1 x2 and 1 in any interval . ı; ı/, where ı > 0, and limits, if they exist, must be unique. p lim Œx C x 2 4x C 1 lim sin

x! 1

x2 x

.x 2 p x2

4x C 1/

4x C 1 4x 1

p jxj 1 .4=x/ C .1=x 2 / xŒ4 .1=x/ D lim p x! 1 x C x 1 .4=x/ C .1=x 2 / 4 .1=x/ D lim p D 2: x! 1 1 C 1 .4=x/ C .1=x 2 / Note how we have used jxj D x (in the second last line), because x ! 1. p lim Œx C x 2 4x C 1 D 1 C 1 D 1 D lim

x! 1

30. p

1

1

x2 D1 .4=x 2 /

x2

D lim

p p h. x C 3h C x/ .x C 3h/ x h!0 x p p p 2 x x C 3h C x D D lim 3 3 h!0

does not exist because

fined for x < 0.

lim

x! 1

D lim

x2 D 0 x2

x .1=x 2 / x3 1 D lim D 2 x! 1 1 C .4=x 2 / 1 x C4

x!0

x!3

14.

1 3

x!0

28.

x 2 x2 4 D lim D 1 x! 2C C 4x C 4 xC2 p 4 x 2 x 1 D lim 12. lim p D x!4 .2 C x!4 x 4 4 x/.x 4/ p p 2 x 9 .x 3/.x C 3/. x C 3/ 13. lim p p D lim x!3 x!3 x 3 x 3 p p p D lim .x C 3/. x C 3/ D 12 3 11.

x 2 is not de-

.1=x 2 / 1 D .1=x/ .1=x 2 /

lim

x!1

4 3

8.

x

2x C 100 .2=x/ C .100=x 2 / D lim D0 2 1 x C3 x! 1 1 C .3=x 2 /

x!1=2

x2 does not exist. The denominator approaches 0 x!1 1 x2 (from both sides) while the numerator does not.

p

lim

x!0C

4C7D4

4 .x D lim x!2 .x 5x C 6

x!1 3x 2

x!

22.

x2 D lim x!1 3 x 1

1

lim

x!

2 C 2h 3 3 D lim h h!0 2.3 C 2h 3/ D lim 3/h h!0 3.2h 4 4 D lim D : 3/ 9 h!0 3.2h

lim

x2

x 2 does not exist because

x

fined for x > 1. p lim x x2 D 0

2

7.

x!2 x 2

p

x!1

24. 2

lim

x!1

D lim

4. The rate of change of 1=x at x D 1 .3=2/ C h h

17.

x

x!1

x

x2

is not de-

31.

f .x/ D x 3 4x 2 C 1 is continuous on the whole real line and so is discontinuous nowhere.

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INSTRUCTOR’S SOLUTIONS MANUAL

CHALLENGING PROBLEMS 1 (PAGE 94)

x is continuous everywhere on its domain, xC1 which consists of all real numbers except x D 1. It is discontinuous nowhere.  x 2 if x > 2 is defined everywhere and disf .x/ D x if x  2 continuous at x D 2, where it is, however, left continuous since limx!2 f .x/ D 2 D f .2/.  x 2 if x > 1 is defined and continuous evf .x/ D x if x  1 erywhere, and so discontinuous nowhere. Observe that limx!1 f .x/ D 1 D limx!1C f .x/. n 1 if x  1 is defined everywhere f .x/ D H.x 1/ D 0 if x < 1 and discontinuous at x D 1 where it is, however, right continuous. n 1 if 3  x  3 is defined f .x/ D H.9 x 2 / D 0 if x < 3 or x > 3 everywhere and discontinuous at x D ˙3. It is right continuous at 3 and left continuous at 3.

32. f .x/ D

33.

34.

35.

36.

37. f .x/ D jxj C jx C 1j is defined and continuous everywhere. It is discontinuous nowhere. n jxj=jx C 1j if x ¤ 1 38. f .x/ D is defined everywhere 1 if x D 1 and discontinuous at x D 1 where it is neither left nor right continuous since limx! 1 f .x/ D 1, while f . 1/ D 1.

Challenging Problems 1 1.

2.

lim

3.

.c C h/3 h h!0 lim

p

.a2

c3

D lim

4.

h!0

b 2 /=3,

2

2

2

If c D C ab C then 3c D a C ab C b , so the average rate ofpchange over Œa; b is the instantaneous rate of change at .a2 C ab C b 2 /=3. p 2 Claim: .a C ab C b 2 /=3 > .a C b/=2. Proof: Since a2 2ab C b 2 D .a b/2 > 0, we have 2

2

2

4a C 4ab C 4b > 3a C 6ab C 3b s

2

a2 C ab C b 2 a2 C 2ab C b 2 > D 3 4

a2 C ab C b 2 aCb > : 3 2



aCb 2

2

jx C 1j

1j

j5 jx

2xj jx 5j j3x

1j D 1

D lim

For x near 3 we have j5 jx 5j D 5 x, and j3x lim

x!0

x .1

x/

.x C 1/

D

1 : 2

2xj D 2x 5, jx 2j D x 7j D 3x 7. Thus 2x 5 .x 2j D lim x!3 5 7j x .3x x 3 D lim D x!3 4.3 x/

x 1=3 x!64 x 1=2

D lim

y!2

5.

x and jx C 1j D x C 1.

2,

2/ 7/ 1 : 4

Let y D x 1=6 . Then we have lim

y2 4 D lim 3 8 y!2 y

4 1 y C2 D D : y 2 C 2y C 4 12 3

Use a b D

have

a2

4 8 .y 2/.y C 2/ D lim y!2 .y 2/.y 2 C 2y C 4/

a3 b 3 to handle the denominator. We C ab C b 2

p 3Cx 2 lim p x!1 3 7 C x 2 .7 C x/2=3 C 2.7 C x/1=3 C 4 3Cx 4 D lim p  x!1 .7 C x/ 8 3CxC2 .7 C x/2=3 C 2.7 C x/1=3 C 4 4C4C4 D 3: D lim p D x!1 2C2 3CxC2 6.

3c 2 h C 3ch2 C h3 D 3c 2 : h

jx

x!3

Let 0 < a < b. The average rate of change of x 3 over Œa; b is b 3 a3 D b 2 C ab C a2 : b a The instantaneous rate of change of x at x D c is

x

x!0

(page 94)

3

For x near 0 we have jx Thus

1C

p

p

1Ca , r .a/ D . a a a) lima!0 r .a/ does not exist. Observe that the right limit is 1 and the left limit is 1.

rC .a/ D

1Ca

1

b) From the following table it appears that lima!0 rC .a/ D 1=2, the solution of the linear equation 2x 1 D 0 which results from setting a D 0 in the quadratic equation ax 2 C 2x 1 D 0. a

rC .a/

1 0:1 0:1 0:01 0:01 0:001 0:001

0:41421 0:48810 0:51317 0:49876 0:50126 0:49988 0:50013

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37

lOMoARcPSD|6566483

CHALLENGING PROBLEMS 1 (PAGE 94)

p 1Ca 1 a!0 a .1 C a/ 1 D lim p a!0 a. 1 C a C 1/ 1 1 D : D lim p a!0 2 1CaC1

8.

c) lim rC .a/ D lim a!0

7.

ADAMS and ESSEX: CALCULUS 9

TRUE or FALSE

a) If limx!a f .x/ exists and limx!a   g.x/ does not exist, then limx!a f .x/ C g.x/ does not exist.   TRUE, because if limx!a f .x/ C g.x/ were to exist then   lim g.x/ D lim f .x/ C g.x/ f .x/ x!a x!a   lim f .x/ D lim f .x/ C g.x/

9.

x!a

x!a

would also exist. b) If neither  limx!a f .x/  nor limx!a g.x/ exists, then limx!a f .x/ C g.x/ does not exist. FALSE. Neither limx!0 1=x nor limx!0 . 1=x/ exist,  but limx!0 .1=x/ C . 1=x/ D limx!0 0 D 0 exists. c) If f is continuous at a, then so is jf j. TRUE. For any two real numbers u and v we have ˇ ˇ ˇjuj

This follows from juj D ju jvj D jv

ˇ ˇ jvjˇ  ju

v C vj  ju u C uj  jv

Now we have ˇ ˇ ˇjf .x/j

vj:

b) If the domain of the continuous function f is an open interval, the range of f can be any interval (open, closed, half open, finite, or infinite). n x2 1 1 if 1 < x < 1 D . f .x/ D 2 1 if x < 1 or x > 1 jx 1j f is continuous wherever it is defined, that is at all points except x D ˙1. f has left and right limits 1 and 1, respectively, at x D 1, and has left and right limits 1 and 1, respectively, at x D 1. It is not, however, discontinuous at any point, since 1 and 1 are not in its domain. 1 1 1  D D 1 2 . 1 2 1 x x2 x C x x 12 4 4 4 Observe that f .x/  f .1=2/ D 4 for all x in .0; 1/.

10. f .x/ D 11.

Suppose f is continuous on Œ0; 1 and f .0/ D f .1/.

a) To be proved: f .a/ D f .a C 12 / for some a in Œ0; 21 . Proof: If f .1=2/ D f .0/ we can take a D 0 and be done. If not, let g.x/ D f .x C 21 /

vj C jvj; and uj C juj D ju vj C juj:

ˇ ˇ jf .a/jˇ  jf .x/

f .a/j

so the left side approaches zero whenever the right side does. This happens when x ! a by the continuity of f at a. d) If jf j is continuous at a, then so  is f . 1 if x < 0 is FALSE. The function f .x/ D 1 if x  0 discontinuous at x D 0, but jf .x/j D 1 everywhere, and so is continuous at x D 0. e) If f .x/ < g.x/ in an interval around a and if limx!a f .x/ D L and limx!a g.x/ D M both exist, then L < M .  2 if x ¤ 0 and let FALSE. Let g.x/ D x 1 if x D 0 f .x/ D g.x/. Then f .x/ < g.x/ for all x, but limx!0 f .x/ D 0 D limx!0 g.x/. (Note: under the given conditions, it is TRUE that L  M , but not necessarily true that L < M .) 38

a) To be proved: if f is a continuous function defined on a closed interval Œa; b, then the range of f is a closed interval. Proof: By the Max-Min Theorem there exist numbers u and v in Œa; b such that f .u/  f .x/  f .v/ for all x in Œa; b. By the Intermediate-Value Theorem, f .x/ takes on all values between f .u/ and f .v/ at values of x between u and v, and hence at points of Œa; b. Thus the range of f is Œf .u/; f .v/, a closed interval.

f .x/:

Then g.0/ ¤ 0 and g.1=2/ D f .1/

f .1=2/ D f .0/

f .1=2/ D

g.0/:

Since g is continuous and has opposite signs at x D 0 and x D 1=2, the Intermediate-Value Theorem assures us that there exists a between 0 and 1/2 such that g.a/ D 0, that is, f .a/ D f .a C 12 /. b) To be proved: if n > 2 is an integer, then f .a/ D f .a C n1 / for some a in Œ0; 1 n1 . Proof: Let g.x/ D f .x C n1 / f .x/. Consider the numbers x D 0, x D 1=n, x D 2=n, : : : , x D .n 1/=n. If g.x/ D 0 for any of these numbers, then we can let a be that number. Otherwise, g.x/ ¤ 0 at any of these numbers. Suppose that the values of g at all these numbers has the same sign (say positive). Then we have f .1/ > f . n n 1 / >    > f . n2 / >

1 n

> f .0/;

which is a contradiction, since f .0/ D f .1/. Therefore there exists j in the set f0; 1; 2; : : : ; n 1g such that g.j=n/ and g..j C 1/=n/ have opposite sign. By the Intermediate-Value Theorem, g.a/ D 0 for some a between j=n and .j C 1/=n, which we had to prove.

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INSTRUCTOR’S SOLUTIONS MANUAL

CHAPTER 2.

SECTION 2.1 (PAGE 100)

DIFFERENTIATION

7.

Slope of y D

x C 1 at x D 3 is p p 4Ch 2 4ChC2 p m D lim h h!0 4ChC2 4Ch 4 p D lim  h!0 h hChC2 1 1 D : D lim p 4 h!0 4ChC2

Section 2.1 Tangent Lines and Their Slopes (page 100) 1.

Slope of y D 3x m D lim

h!0

1 at .1; 2/ is

3.1 C h/

1 .3  1 h

1/

D lim

h!0

3h D 3: h

The tangent line is y 2 D 3.x 1/, or y D 3x 1. (The tangent to a straight line at any point on it is the same straight line.)

Tangent line is y 8.

2.2 C h/2

5 .2.22 / h h!0 8 C 8h C 2h2 8 D lim h h!0 D lim .8 C 2h/ D 8

5/

3 D 8.x

4. The slope of y D 6

x

6

m D lim

h!0

. 2 C h/ h2

3h

D lim

h!0

2/ or y D 8x

x 2 at x D

h

h

13.

9.

Slope of y D

. 2 C h/2

4

h/ D 3:

h!0

The tangent line at . 2; 4/ is y D 3x C 10. 5. Slope of y D x 3 C 8 at x D

. 2 C h/3 C 8 . 8 C 8/ h h!0 8 C 12h 6h2 C h3 C 8 D lim h h!0  D lim 12 6h C h2 D 12

6. The slope of y D

0

m D lim

h!0

0 D 12.x C 2/ or y D 12x C 24.

1 1 h h2 C 1

1 D lim

The tangent line at .0; 1/ is y D 1.

h!0

h D 0: h2 C 1

1D

1 .x 4

1 .x 54

9/, or

2/,

p

D lim p h!0 5

1 at .0; 1/ is x2 C 1 !

1 3

5 x 2 at x D 1 is p 5 .1 C h/2 2 m D lim h h!0 5 .1 C h/2 4  D lim p h!0 h 5 .1 C h/2 C 2

10. The slope of y D

h!0

Tangent line is y

5.

2x at x D 2 is xC2

Tangent line is y or x 4y D 2.

2 is

m D lim

4y D

2.2 C h/ 1 2ChC2 m D lim h h!0 4 C 2h 2 h 2 D lim h.2 C h C 2/ h!0 1 h D : D lim 4 h!0 h.4 C h/

2 is

D lim .3

3/, or x

The tangent line at .9; 13 / is y D 1 y D 12 54 x.

h!0

Tangent line is y

1 .x 4

! 1 1 1 m D lim p h!0 h 9Ch 3 p p 3 9Ch 3C 9Ch D lim p  p h!0 3h 9 C h 3C 9Ch 9 9 h D lim p p h!0 3h 9 C h.3 C 9 C h/ 1 1 D : D 3.3/.6/ 54

5 at .2; 3/ is

m D lim

2D

1 The slope of y D p at x D 9 is x

2. Since y D x=2 is a straight line, its tangent at any point .a; a=2/ on it is the same line y D x=2. 3. Slope of y D 2x 2

p

2

h

.1 C

h/2

The tangent line at .1; 2/ is y D 2 y D 52 12 x. 11.

C2 1 2 .x

D

1 2

1/, or

Slope of y D x 2 at x D x0 is m D lim

h!0

.x0 C h/2 h

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x02

D lim

h!0

2x0 h C h2 D 2x0 : h

39

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SECTION 2.1 (PAGE 100)

ADAMS and ESSEX: CALCULUS 9

Tangent line is y x02 D 2x0 .x or y D 2x0 x x02 .

x0 /,

19.

1 at .a; a1 / is 12. The slope of y D x ! 1 1 1 a a h 1 . C D D lim m D lim a a2 h!0 h.a C h/.a/ h!0 h a C h 1 1 1 The tangent line at .a; / is y D .x a/, or a a a2 x 2 . yD a a2 p j0 C hj 0 1 D lim does not 13. Since limh!0 h h!0 jhjsgn .h/ p exist (and is not 1 or 1), the graph of f .x/ D jxj has no tangent at x D 0. 14.

The slope of f .x/ D .x m D lim

h!0

.1 C h

0

1=3

D lim h h!0

Slope of y D x 3 at x D a is .a C h/3 a3 h h!0 a3 C 3a2 h C 3ah2 C h3 D lim h h!0 D lim .3a2 C 3ah C h2 / D 3a2

m D lim

a3

h!0

b) We have m D 3 if 3a2 D 3, i.e., if a D ˙1. Lines of slope 3 tangent to y D x 3 are y D 1 C 3.x 1/ and y D 1 C 3.x C 1/, or y D 3x 2 and y D 3x C 2.

20.

The slope of y D x 3

3x at x D a is

i 1h .a C h/3 3.a C h/ .a3 3a/ h!0 h 1h 3 a C 3a2 h C 3ah2 C h3 3a 3h D lim h!0 h D lim Œ3a2 C 3ah C h2 3 D 3a2 3:

m D lim

1/4=3 at x D 1 is

1/4=3 h

a)

D 0:

a3 C 3a

h!0

The graph of f has a tangent line with slope 0 at x D 1. Since f .1/ D 0, the tangent has equation y D 0 15.

The slope of f .x/ D .x C 2/3=5 at x D m D lim

h!0

. 2 C h C 2/3=5 h

0

At points where the tangent line is parallel to the x-axis, the slope is zero, so such points must satisfy 3a2 3 D 0. Thus, a D ˙1. Hence, the tangent line is parallel to the x-axis at the points .1; 2/ and . 1; 2/.

2 is

D lim h

2=5

h!0

The graph of f has vertical tangent x D

D 1:

2 at x D

21.

f .0 C h/ h h!0C f .0 C h/ lim h h!0

f .0/

p

h D1 h p h D1 h

D lim

h!0C

f .0/

D lim h!0

m D lim

The tangent at x D a is parallel to the line y D 2x C 5 if 3a2 1 D 2, that is, if a D ˙1. The corresponding points on the curve are . 1; 1/ and .1; 1/. 22.

h!0

1 h

.x02

1/

2x0 h C h2 D 2x0 : h h!0

D lim

1 a D lim a .a C h/ D h!0 ah.a C h/

1 : a2

The tangent at x D a is perpendicular to the line y D 4x 3 if 1=a2 D 1=4, that is, if a D ˙2. The corresponding points on the curve are . 2; 1=2/ and .2; 1=2/. 23.

The slope of the curve y D x 2 at x D a is m D lim

h!0

If m D 3, then x0 D 32 . The tangent line with slope m D 3 at . 32 ; 54 / is y D 45 3.x C 23 /, that is, 13 y D 3x 4 .

40

The slope of the curve y D 1=x at x D a is 1 a C h m D lim h h!0

1 at x D x0 is Œ.x0 C h/2

.a C h/3

h!0

Thus the graph of f has a vertical tangent x D 0.

18. The slope of y D x 2

x C 1 at x D a is

.a C h/ C 1 .a3 a C 1/ h h!0 3a2 h C 3ah2 C a3 h D lim h h!0 D lim .3a2 C 3ah C h2 1/ D 3a2 1:

m D lim

2.

16. The slope of f .x/ D jx 2 1j at x D 1 is j.1 C h/2 1j j1 1j j2h C h2 j m D limh!0 D lim , h h h!0 which does not exist, and is not 1 or 1. The graph of f has no tangent at x D 1. p x if x  0 p 17. If f .x/ D , then x if x < 0 lim

The slope of the curve y D x 3

.a C h/2 h

a2

D lim .2a C h/ D 2a: h!0

The normal at x D a has slope y

a2 D

1 .x 2a

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a/;

or

1=.2a/, and has equation x 1 C y D C a2 : 2a 2

i

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 2.1 (PAGE 100)

y

This is the line x C y D k if 2a D 1, and so k D .1=2/ C .1=2/2 D 3=4. 24.

The curves y D kx 2 and y D k.x The slope of y D kx 2 at x D 1 is k.1 C h/2 m1 D lim h h!0 The slope of y D k.x m2 D lim

k.2

h!0

k

2

2/2 intersect at .1; k/.

1 -3

-2

-1

D lim .2 C h/k D 2k:

-2

2/2 at x D 1 is k

D lim . 2 C h/k D h!0

x

2

-1

h!0

.1 C h//2 h

1 1j

x

-3 Fig. 2.1-27

2k:

The two curves intersect at right angles if 2k D 1=. 2k/, that is, if 4k 2 D 1, which is satisfied if k D ˙1=2.

y D jx 2

28.

25. Horizontal tangents at .0; 0/, .3; 108/, and .5; 0/. y .3; 108/

Horizontal tangent at .a; 2/ and . a; 2/ for all a > 1. No tangents at .1; 2/ and . 1; 2/. y y D jx C 1j jx 1j 2 1

100 80

-3

-2

-1

60

1

2

x

-1

40 y D x 3 .5

20 -1

1

2

-2

x/2

3

4

5

-3 Fig. 2.1-28

x

-20 Fig. 2.1-25 29. 26. Horizontal tangent at . 1; 8/ and .2; 19/. y

Horizontal tangent at .0; 1/. The tangents at .˙1; 0/ are vertical. y y D .x 2

20 . 1; 8/ 10 -2

-1

y D 2x 3

3x 2

1

2

1/1=3 2 1

12x C 1 3

-3

x

-2

-1

1

2

x

-1

-10 -2 -20

.2; 19/ -3 Fig. 2.1-29

-30 Fig. 2.1-26

27.

Horizontal tangent at . 1=2; 5=4/. No tangents at . 1; 1/ and .1; 1/.

30.

Horizontal tangent at .0; 1/. No tangents at . 1; 0/ and .1; 0/.

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41

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SECTION 2.1 (PAGE 100)

ADAMS and ESSEX: CALCULUS 9

y

2. y

y D ..x 2

1/2 /1=3 2

1 y D g 0 .x/ -1

-2

1

2

x

x

Fig. 2.1-30 31. The graph of the function f .x/ D x 2=3 (see Figure 2.1.7 in the text) has a cusp at the origin O, so does not have a tangent line there. However, the angle between OP and the positive y-axis does ! 0 as P approaches 0 along the graph. Thus the answer is NO.

3. y

y D h0 .x/ x

32. The slope of P .x/ at x D a is m D lim

h!0

P .a C h/ h

P .a/

:

Since P .a C h/ D a0 C a1 h C a2 h2 C    C an hn and P .a/ D a0 , the slope is a0 C a1 h C a2 h2 C    C an hn a0 h h!0 D lim a1 C a2 h C    C an hn 1 D a1 :

m D lim

4. y

h!0

Thus the line y D `.x/ D m.x a/ C b is tangent to y D P .x/ at x D a if and only if m D a1 and b D a0 , that is, if and only if

x

P .x/ `.x/ D a2 .x a/2 C a3 .x a/3 C    C an .x a/n h i D .x a/2 a2 C a3 .x a/ C    C an .x a/n 2 D .x

y D k 0 .x/

a/2 Q.x/

where Q is a polynomial.

Section 2.2 The Derivative

(page 107)

5.

Assuming the tick marks are spaced 1 unit apart, the function f is differentiable on the intervals . 2; 1/, . 1; 1/, and .1; 2/.

6.

Assuming the tick marks are spaced 1 unit apart, the function g is differentiable on the intervals . 2; 1/, . 1; 0/, .0; 1/, and .1; 2/.

7.

y D f .x/ has its minimum at x D 3=2 where f 0 .x/ D 0

1. y 0

y D f .x/

x

42

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lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 2.2 (PAGE 107)

y y D f .x/ D 3x

x

2

y D f .x/ D jx 3

y 1j

1

x

x y y D f 0 .x/

y y D f 0 .x/

x x

Fig. 2.2-7

Fig. 2.2-9

8. y D f .x/ has horizontal tangents at the points near 1=2 and 3=2 where f 0 .x/ D 0 y

10. y D f .x/ is constant on the intervals . 1; 2/, . 1; 1/, and .2; 1/. It is not differentiable at x D ˙2 and x D ˙1. y y D f .x/ D jx 2 1j jx 2 4j

x x y D f .x/ D x 3

3x 2 C 2x C 1 y y D f 0 .x/

y

x x y D f 0 .x/ Fig. 2.2-10 Fig. 2.2-8 11.

y D x2 y 0 D lim

h!0

9. y D f .x/ fails to be differentiable at x D 1, x D 0, and x D 1. It has horizontal tangents at two points, one between 1 and 0 and the other between 0 and 1.

3x .x C h/2

2xh C h2 h h!0 dy D .2x 3/ dx D lim

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3.x C h/ .x 2 h 3h D 2x 3

3x/

43

lOMoARcPSD|6566483

SECTION 2.2 (PAGE 107)

12.

f .x/ D 1 C 4x f 0 .x/ D lim

h!0

D lim

h!0

df .x/ D .4

13.

5x 2

1 C 4.x C h/

4h

ADAMS and ESSEX: CALCULUS 9

10xh h 10x/ dx

17. 5.x C h/2 h 5h2

D4

.1 C 4x

5x 2 /

10x

2 D lim p p h!0 2.t C h/ C 1 C 2t C 1 1 D p 2t C 1 1 dF .t / D p dt 2t C 1

f .x/ D x 3

.x C h/3 x 3 h h!0 3x 2 h C 3xh2 C h3 D lim D 3x 2 h h!0 df .x/ D 3x 2 dx f 0 .x/ D lim

18.

f .x/ D 0

14.

15.

16.

1 3 C 4t   ds 1 1 1 D lim dt 3 C 4t h!0 h 3 C 4.t C h/ 4 3 C 4t 3 4t 4h D D lim .3 C 4t /2 h!0 h.3 C 4t /Œ3 C .4t C h/ 4 dt ds D .3 C 4t /2

2 x g.x/ D 2Cx 2 .x C h/ 2 x 2CxCh 2Cx 0 g .x/ D lim h h!0 .2 x h/.2 C x/ .2 C x C h/.2 D lim h.2 C x C h/.2 C x/ h!0 4 D .2 C x/2 4 dx dg.x/ D .2 C x/2

y 0 D lim

x 1h

1 .x C h/3 .x C h/ . 13 x 3 h 3  1 2 x h C xh2 C 31 h3 h D lim h!0 h D lim .x 2 C xh C 31 h2 1/ D x 2 1 h!0

h!0

dy D .x 2

44

1/ dx

i x/

3 4

p

f .x/ D lim

2 3 4

h!0

3 D lim h!0 4

sD

y D 31 x 3

p

2t C 1 p p 2.t C h/ C 1 2t C 1 F 0 .t / D lim h h!0 2t C 2h C 1 2t 1  D lim p p h!0 h 2.t C h/ C 1 C 2t C 1 F .t / D

D df .x/ D

19.

yDxC

x p 2 "

3

3 4

.x C h/ h 2

p h. 2

p

2

x

2Cx p .x C h/ C 2 x

h

x/

#

p 8 2 x 3 p dx 8 2 x

1 x

1 1 x x C h x y D lim h h!0   x x h D lim 1 C h.x C h/x h!0 1 1 D 1 C lim D1 x2 h!0 .x C h/x   1 dx dy D 1 x2 0

x/

20.

xChC

s 1Cs   dz 1 sCh s D lim ds 1Cs h!0 h 1 C s C h .s C h/.1 C s/ s.1 C s C h/ 1 D lim D h.1 C s/.1 C s C h/ .1 C s/2 h!0 1 dz D ds .1 C s/2 zD

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lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

F .x/ D p

21.

SECTION 2.2 (PAGE 107)

1

25.

1 C x2

1 1 p p 2 1 C x2 1 C .x C h/ F 0 .x/ D lim h h!0 p 26. p 1 C x2 1 C .x C h/2 D lim p p h!0 h 1 C .x C h/2 1 C x 2 1 C x 2 1 x 2 2hx h2 p  27. D lim p p p h!0 h 1 C .x C h/2 1 C x 2 1 C x 2 C 1 C .x C h/2 2x x D 2 3=2 2.1 C x / .1 C x 2 /3=2 x dF .x/ D dx .1 C x 2 /3=2 D

22.

yD

1 x2



28.

23.

yD p

p

2x f .x/

1

ˇ ˇ ˇ 2x/ˇ ˇ

1 p 1Cx

t2 3 t2 C 3   t2 3 1 .t C h/2 3 f 0 .t / D lim .t C h/2 C 3 t 2 C 3 h!0 h 2 Œ.t C h/ 3.t 2 C 3/ .t 2 3/Œ.t C h/2 C 3 D lim h.t 2 C 3/Œ.t C h/2 C 3 h!0 12t h C 6h2 12t D lim D 2 2 2 .t C 3/2 h!0 h.t C 3/Œ.t C h/ C 3 12t df .t / D 2 dt .t C 3/2

f .1/

x 1 0:71000 0:97010 0:99700 0:99970

d 3 .x dx

1CxCh y 0 .x/ D lim h h!0 p p 1Cx 1CxCh D lim p p h!0 h 1 C x C h 1 C x 1Cx 1 x h p D lim p  p p h!0 h 1 C x C h 1 C x 1CxC 1CxCh 1 p D lim p  p p h!0 1CxCh 1Cx 1CxC 1CxCh 1 D 2.1 C x/3=2 1 dy D dx 2.1 C x/3=2 24.

y D x3

0:9 0:99 0:999 0:9999

1 1Cx

h.x/ D jx 2 C 3x C 2j fails to be differentiable where x 2 C 3x C 2 D 0, that is, at x D 2 and x D 1. Note: both of these are single zeros of x 2 C 3x C 2. If they were higher order zeros (i.e. if .x C 2/n or .x C 1/n were a factor of x 2 C 3x C 2 for some integer n  2) then h would be differentiable at the corresponding point.

x



1 1 1 2 x2 h!0 h .x C h/ 2 2 x .x C h/ 2 D lim D x3 h!0 hx 2 .x C h/2 2 dx dy D x3 y 0 D lim

Since f .x/ D x sgn x D jxj, for x ¤ 0, f will become continuous at x D 0 if we define f .0/ D 0. However, f will still not be differentiable at x D 0 since jxj is not differentiable at x D 0.  2 Since g.x/ D x 2 sgn x D xjxj D x 2 if x > 0 , g will x if x < 0 become continuous and differentiable at x D 0 if we define g.0/ D 0.

xD1

x

f .x/

x 1 1:31000 1:03010 1:00300 1:00030

1:1 1:01 1:001 1:0001

D lim

h!0

f .1/

.1 C h/3

2.1 C h/ h

. 1/

h C 3h2 C h3 h h!0 D lim 1 C 3h C h2 D 1

D lim

h!0

29.

f .x/ D 1=x f .x/

x

f .2/

x 2 0:26316 0:25126 0:25013 0:25001

1:9 1:99 1:999 1:9999

x 2:1 2:01 2:001 2:0001

f .x/

f .2/

x 2 0:23810 0:24876 0:24988 0:24999

1 2 2 .2 C h/ 2Ch f .2/ D lim D lim h h!0 h!0 h.2 C h/2 1 1 D lim D .2 C h/2 4 h!0 0

f .t / D

30.

The slope of y D 5 C 4x x 2 at x D 2 is ˇ 5 C 4.2 C h/ .2 C h/2 dy ˇˇ D lim ˇ ˇ dx h h!0

9

xD2

D lim

h!0

h2 D 0: h

Thus, the tangent line at x D 2 has the equation y D 9.

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45

lOMoARcPSD|6566483

SECTION 2.2 (PAGE 107)

31. y D

ADAMS and ESSEX: CALCULUS 9

p

x C 6. Slope at .3; 3/ is p 1 9Ch 3 9Ch 9 p D lim m D lim  D : h 6 h!0 h h!0 9ChC3

Tangent line is y

32. The slope of y D ˇ dy ˇˇ ˇ dt ˇ

tD 2

3D

1 .x 6

t t2

2

3/, or x

at t D

6y D

2 and y D

 2Ch 1 2 h!0 h . 2 C h/2

D lim

D lim

h!0

44.

3 : 2

45.

yD

2 t2 C t

0

17x

35. g .t / D 22t 36. 37. 38. 39. 40.

41.

42.

43.

21

46

xDa

D

1 . a2

1 D a2 .x a

a/,

Slope at t D a is

18

46.

Therefore x D

9 4

18 D 0 2/ D 0:

or x D 2.

dy The slope of y D x 2 is m1 D D 2x. dx 9 9 , m1 D . At x D 2, m1 D 4. At x D 4 2 The slope of x C 4y D 18, i.e. y D 14 x C 18 4 , is m2 D 41 . Thus, at x D 2, the product of these slopes is .4/. 41 / D 1. So, the curve and line intersect at right angles at that point.

for all t

tD4

The intersection points of y D x 2 and x C 4y D 18 satisfy 4x 2 C x .4x C 9/.x

for x ¤ 0

1 dy D x 2=3 for x ¤ 0 dx 3 dy 1 4=3 D x for x ¤ 0 dx 3 d 2:25 t D 2:25t 3:25 for t > 0 dt d 119=4 119 115=4 s D s for s > 0 ds 4 ˇ ˇ 1 d p ˇˇ 1 ˇˇ D : sˇ D p ˇ ˇ ds 6 2 sˇ sD9 sD9   1 1 0 1 ; F D 16 F .x/ D ; F 0 .x/ D x x2 4 ˇ 2 5=3 ˇˇ 1 0 f .8/ D x D ˇ ˇ 3 48 xD8 ˇ ˇ ˇ ˇ dy ˇ 1 1 ˇ D t 3=4 ˇ D p ˇ ˇ dt ˇ 4 8 2 tD4

ˇ 1 ˇˇ ˇ x2 ˇ

Normal has slope a , and equation y 1 or y D a2 x a3 C a

2 2 .a C h/2 C .a C h/ a2 C a m D lim h h!0 2.a2 C a a2 2ah h2 a h/ D lim hŒ.a C h/2 C a C h.a2 C a/ h!0 4a 2h 2 D lim 2 h!0 Œ.a C h/ C a C h.a2 C a/ 4a C 2 D .a2 C a/2 2.2a C 1/ 2 .t a/ Tangent line is y D 2 a C a .a2 C a/2

34. f 0 .x/ D

1 at x D a is Slope of y D x 2

Thus, the tangent line has the equation y D 1 23 .t C 2/, that is, y D 32 t 4. 33.

1 D p : 2 x0

Thus, the equation of the tangent line is x C x0 1 p y D x0 C p .x x0 /, that is, y D p . 2 x0 2 x0

1 is

D

x at x D x0 is

xDx0

15.



p

ˇ dy ˇˇ ˇ dx ˇ

 . 1/

2 C h C Œ. 2 C h/2 hŒ. 2 C h/2 2

The slope of y D

47.

Let theˇ point of tangency be .a; a2 /. Slope of tangent is d 2 ˇˇ x ˇ D 2a dx ˇ xDa

This is the slope from .a; a2 / to .1; 3/, so a2 C 3 D 2a, and a 1 a2 C 3 D 2a2

2a

a2 2a 3 D 0 a D 3 or 1 The two tangent lines are (for a D 3): y 9 D 6.x 3/ or 6x 9 (for a D 1): y 1 D 2.x C 1/ or y D

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2x

1

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 2.2 (PAGE 107)

p p 4a2 4b D a ˙ a2 b. 2 p If b < a2 , i.e. a2 b > 0, then t D a ˙ a2 b has two real solutions. Therefore, there will be two distinct tangent lines passing through .a; b/ with equations  p y D b C 2 a ˙ a2 b .x a/. If b D a2 , then t D a. There will be only one tangent line with slope 2a and equation y D b C 2a.x a/. If b > a2 , then a2 b < 0. There will be no real solution for t . Thus, there will be no tangent line.

y

Hence t D .a;a2 /

y D x2

x

2a ˙

.1; 3/

Fig. 2.2-47

48. The slope of y D

1 at x D a is x ˇ dy ˇˇ ˇ dx ˇ

xDa

or y D

Suppose f is odd: f . x/ D f .x/. Then f . x C h/ f . x/ f 0 . x/ D lim h h!0 f .x h/ f .x/ D lim h h!0 .let h D k/ f .x C k/ f .x/ D lim D f 0 .x/ k k!0 Thus f 0 is even. Now suppose f is even: f . x/ D f .x/. Then f . x C h/ f . x/ f 0 . x/ D lim h h!0 f .x h/ f .x/ D lim h h!0 f .x C k/ f .x/ D lim k k!0 D f 0 .x/ so f 0 is odd.

52.

Let f .x/ D x

1 : a2

1 1 D 2, or a D ˙ p . Therea2 2 equations of the are   two straight lines   p 1 1 2 x p and y D 2 2 xCp , 2 p 2 2x ˙ 2 2.

If the slope is fore, the p yD 2

D

51.

2, then

p 49. Let the point of tangency be ˇ .a; a/ d p ˇˇ 1 Slope of tangent is xˇ D p ˇ dx 2 a xDa p a 0 1 , so a C 2 D 2a, and a D 2. Thus p D aC2 2 a 1 The required slope is p . 2 2 y

p .a; a/ p yD x x

2

Fig. 2.2-49 50. If aˇ line is tangent to y D x 2 at .t; t 2 /, then its slope is dy ˇˇ D 2t . If this line also passes through .a; b/, then ˇ dx ˇ xDt its slope satisfies t2 b D 2t; t a

that is t 2

2at C b D 0:

f 0 .x/ D lim

n

. Then .x C h/

n

x

n

h   1 1 1 D lim .x C h/n x n h!0 h n x .x C h/n D lim n h!0 hx .x C h/n x .x C h/  D lim h!0 hx n ..x C h/n  x n 1 C x n 2 .x C h/ C    C .x C h/n h!0

D

1  nx n x 2n

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1

D

nx

.nC1/

1



:

47

lOMoARcPSD|6566483

SECTION 2.2 (PAGE 107)

53.

ADAMS and ESSEX: CALCULUS 9

f .x/ D x 1=3

If f 0 .aC/ is finite, call the half-line with equation y D f .a/ C f 0 .aC/.x a/, (x  a), the right tangent line to the graph of f at x D a. Similarly, if f 0 .a / is finite, call the half-line y D f .a/ C f 0 .a /.x a/, (x  a), the left tangent line. If f 0 .aC/ D 1 (or 1), the right tangent line is the half-line x D a, y  f .a/ (or x D a, y  f .a/). If f 0 .a / D 1 (or 1), the right tangent line is the half-line x D a, y  f .a/ (or x D a, y  f .a/). The graph has a tangent line at x D a if and only if f 0 .aC/ D f 0 .a /. (This includes the possibility that both quantities may be C1 or both may be 1.) In this case the right and left tangents are two opposite halves of the same straight line. For f .x/ D x 2=3 , f 0 .x/ D 32 x 1=3 : At .0; 0/, we have f 0 .0C/ D C1 and f 0 .0 / D 1. In this case both left and right tangents are the positive y-axis, and the curve does not have a tangent line at the origin. For f .x/ D jxj, we have

.x C h/1=3 x 1=3 h h!0 .x C h/1=3 x 1=3 D lim h h!0 .x C h/2=3 C .x C h/1=3 x 1=3 C x 2=3  .x C h/2=3 C .x C h/1=3 x 1=3 C x 2=3 xCh x D lim h!0 hŒ.x C h/2=3 C .x C h/1=3 x 1=3 C x 2=3  1 D lim h!0 .x C h/2=3 C .x C h/1=3 x 1=3 C x 2=3 1 1 D D x 2=3 3 3x 2=3

f 0 .x/ D lim

54. Let f .x/ D x 1=n . Then .x C h/1=n f 0 .x/ D lim h h!0 a b D lim n bn a!b a D lim

a!b

1 D nb n

55.

an 1

x 1=n

1 C an 2 b C an 1 D x .1=n/ 1 : n 1

(let x C h D an , x D b n )

3 b2

C    C bn

d n .x C h/n x n x D lim dx h h!0  n.n 1/ n 2 2 1 n n n 1 hC x h x C x D lim 1 12 h!0 h  n.n 1/.n 2/ n 3 3 C x h C    C hn x n 123  n.n 1/ n 2 x h D lim nx n 1 C h 12 h!0 ! n.n 1/.n 2/ n 3 2 n 1 C x h C  C h 123 D nx n

f 0 .x/ D sgn .x/ D

1

1

1.

y D 3x 2

2.

y D 4x 1=2

3.

f .x/ D Ax 2 C Bx C C;

4.

f .x/ D

5.

zD

6.

y D x 45

7.

8.

f .a/

h!0C

48

f .a/

1

Section 2.3 Differentiation Rules (page 115)

9. f .a C h/ h f .a C h/ 0 f .a / D lim h h!0

if x > 0 if x < 0.

1

At .0; 0/, f 0 .0C/ D 1, and f 0 .0 / D 1. In this case the right tangent is y D x, .x  0/, and the left tangent is y D x, .x  0/. There is no tangent line.

56. Let f 0 .aC/ D lim

n

10.

5x

7;

5 ; x

y 0 D 2x

2 6 C 2 x3 x

s5

s3 15

2;

45

5:

1=2

C 5x

2

f 0 .x/ D 2Ax C B: f 0 .x/ D

dz 1 D s4 dx 3

;

x

y 0 D 6x

18 x4

4 x3

1 2 s : 5

y 0 D 45x 44 C 45x

46

g.t / D t 1=3 C 2t 1=4 C 3t 1=5 1 3 1 g 0 .t / D t 2=3 C t 3=4 C t 4=5 3 2 5 p 2 3 2=3 2 p D 3t yD3 t 2t 3=2 t3 dy D 2t 1=3 C 3t 5=2 dt 3 5 3=5 u D x 5=3 x 5 3 du D x 2=3 C x 8=5 dx

F .x/ D .3x F 0 .x/ D 3.1

2/.1 5x/ 5x/ C .3x 2/. 5/ D 13

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30x

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

11.

yD

p

 x 5

3p x 2

5 y0 D p 2 x

1

12. g.t / D 13.

14. 15.

2t

3

yD

4 3

x

f .t / D

20.

21.

22.

x 3=2

1 5=2 x 3

2 .2t

3/2

24. 2x C 5 .x 2 C 5x/2

4 x/2

.3

 2

25.

t  2 . / D 2 .2  t / .2  t /2 2

f .x/ D

23.

5 3=2 x 6

g 0 .t / D

;

y0 D

;

y2

1

f 0 .x/ D

19.

p D5 x

1 x 2 C 5x 1 y0 D .2x C 5/ D .x 2 C 5x/2

16. g.y/ D

18.



yD

f 0 .t / D

17.

x2 3

x

SECTION 2.3 (PAGE 115)

g 0 .y/ D

;

4x 2

1

x3 3x

4

Dx

C 4x

3

2

.1

4y y 2 /2

4 x 4x 2 3 D x4

26.

p u u 3 D u 1=2 3u 2 u2 p 1 3=2 12 u u g 0 .u/ D u C 6u 3 D 2 2u3 g.u/ D

27.

p 2 C t C t2 D 2t 1=2 C t C t 3=2 p t 1 3p dy 3t 2 C t 2 D t 3=2 C p C p tD dt 2 2 t 2t t yD

x 1 z D 2=3 D x 1=3 x dz 1 2=3 2 D x C x dx 3 3

x 5=3

x3 4 xC1 .x C 1/.3x 2 / .x 3 0 f .x/ D .x C 1/2 3 2x C 3x 2 C 4 D .x C 1/2 f .x/ D

3 4x 3 C 4x .3 C 4x/. 4/ .3 f 0 .x/ D .3 C 4x/2 24 D .3 C 4x/2

4/.1/

ax C b cx C d .cx C d /a .ax C b/c f 0 .x/ D .cx C d /2 ad bc D .cx C d /2 f .x/ D

t 2 C 7t 8 t2 t C 1 2 .t t C 1/.2t C 7/ .t 2 C 7t F 0 .t / D .t 2 t C 1/2 2 8t C 18t 1 D .t 2 t C 1/2 F .t / D

8/.2t

1/

f .x/ D .1 C x/.1 C 2x/.1 C 3x/.1 C 4x/ f 0 .x/ D .1 C 2x/.1 C 3x/.1 C 4x/ C 2.1 C x/.1 C 3x/.1 C 4x/ C 3.1 C x/.1 C 2x/.1 C 4x/ C 4.1 C x/.1 C 2x/.1 C 3x/ OR f .x/ D Œ.1 C x/.1 C 4x/ Œ.1 C 2x/.1 C 3x/ D 1 C 10x C 25x 2 C 10x 2 .1 C 5x/ C 24x 4

2=3

D

p 1 .1 C t /. p / 2 t p 2 t/

D .1 C 5x C 4x 2 /.1 C 5x C 6x 2 /

0

D 1 C 10x C 35x 2 C 50x 3 C 24x 4

f .x/ D 10 C 70x C 150x 2 C 96x 3

xC2 3x 5=3

28.

f .r/ D .r

2

f 0 .r/ D . 2r

f .x/ D

4x/.4/

Cr

or f .r/ D 0

f .r/ D

t 2 C 2t t2 1 2 .t 1/.2t C 2/ .t 2 C 2t /.2t / z0 D .t 2 1/2 2.t 2 C t C 1/ D .t 2 1/2 zD

p 1C t p 1 t p 1 .1 t/ p ds 2 t D dt .1 1 p D p t .1 t /2 sD

29.

3

3

2

1

4

3r

C .r

2Cr

4/.r 2 C r 3 C 1/

2

Cr 3

/.r 2 C r 3 C 1/

Cr 2

3

Cr

4

4/.2r C 3r 2 /

3

Cr

2r 3r C 1 8r p y D .x 2 C 4/. x C 1/.5x 2=3 2/ p y 0 D 2x. x C 1/.5x 2=3 2/ 1 C p .x 2 C 4/.5x 2=3 2/ 2 x p 10 C x 1=3 .x 2 C 4/. x C 1/ 3 r

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4r 2

4r 3

12r 2

49

lOMoARcPSD|6566483

SECTION 2.3 (PAGE 115)

30.

yD D y0 D

D D

31.

32.

yD

ADAMS and ESSEX: CALCULUS 9

.x 2 C 1/.x 3 C 2/ .x 2 C 2/.x 3 C 1/ x 5 C x 3 C 2x 2 C 2 x 5 C 2x 3 C x 2 C 2 .x 5 C 2x 3 C x 2 C 2/.5x 4 C 3x 2 C 4x/ .x 5 C 2x 3 C x 2 C 2/2 5 .x C x 3 C 2x 2 C 2/.5x 4 C 6x 2 C 2x/ .x 5 C 2x 3 C x 2 C 2/2 2x 7 3x 6 3x 4 6x 2 C 4x .x 5 C 2x 3 C x 2 C 2/2 7 2x 3x 6 3x 4 6x 2 C 4x .x 2 C 2/2 .x 3 C 1/2

36.

37.

1 3x C 1 .6x 2 C 2x C 1/.6x C 1/ .3x 2 C x/.12x C 2/ y0 D .6x 2 C 2x C 1/2 6x C 1 D .6x 2 C 2x C 1/2 2x C

p . x

33.

34.

35.

d dx

d dx



39. 1 p x



ˇˇ ˇ ˇ ˇ

ˇ f .x/ ˇˇ ˇ x2 ˇ

xD2

D

xD2

ˇˇ d  2 x f .x/ ˇˇ dx

50

ˇ f .x/.2x/ x 2 f 0 .x/ ˇˇ D ˇ ˇ Œf .x/2 4f .2/ 4f 0 .2/ D Œf .2/2

ˇ x 2 f 0 .x/ 2xf .x/ ˇˇ D ˇ ˇ x4

!

40.

xD2

18 14 1 .4 C f .2//f 0 .2/ f .2/.4 C f 0 .2// D D D .4 C f .2//2 62 9 ˇ  2   ˇ x 4 d d 8 ˇ j D 1 ˇ xD 2 dx x 2 C 4 dx x2 C 4 ˇ xD 2 ˇ ˇ 8 ˇ D 2 .2x/ˇ ˇ .x C 4/2 D

p #ˇ t .1 C t / ˇˇ ˇ ˇ 5 t ˇ " #tD4 d t C t 3=2 ˇˇ D ˇ ˇ dt 5 t

d dt

"

32 D 64

1 2

tD4 ˇ t /.1 C 23 t 1=2 / .t C t 3=2 /. 1/ ˇˇ ˇ ˇ .5 t /2

.5

tD4

.12/. 1/ D D 16 .1/2 p x f .x/ D xC1 p 1 .x C 1/ p x.1/ 2 x f 0 .x/ D .x C 1/2 p 3 p 2 1 2 2 f 0 .2/ D p D 9 18 2

ˇ ˇ d Œ.1 C t /.1 C 2t /.1 C 3t /.1 C 4t /ˇˇ dt tD0 D .1/.1 C 2t /.1 C 3t /.1 C 4t / C .1 C t /.2/.1 C 3t /.1 C 4t /C ˇ ˇ .1 C t /.1 C 2t /.3/.1 C 4t / C .1 C t /.1 C 2t /.1 C 3t /.4/ˇˇ tD0

D 1 C 2 C 3 C 4 D 10

xD2

4 D 4

1

41. y D

2 p , y0 D 4 x

3

2 p 2 4 x

 3



4 p

2 x



8 D4 . 1/2 2 Tangent line has the equation y D 2 C 4.x 1/ or y D 4x 6 Slope of tangent at .1; 2/ is m D

xD2

4 1 4f 0 .2/ 4f .2/ D D D 16 16 4

xD2

ˇˇ ˇ ˇ ˇ

xD2 ˇ .x 2 C f .x//f 0 .x/ f .x/.2x C f 0 .x// ˇˇ D ˇ ˇ .x 2 C f .x//2

D

.3 C 2x/. 1

x2 f .x/

f .x/ x 2 C f .x/

.1/.4/

4x C 3x 2 / .2 x 2x 2 C x 3 /.2/ .3 C 2x/2 2 .2 x/.1 x / D 2x 3=2 .3 C 2x/ ! 1 4x 3 C 5x 2 12x 7 C 1 p .3 C 2x/2 x



38.

2

1/.2 x/.1 x / p x.3 C 2x/ ! 1 2 x 2x 2 C x 3 D 1 p  3 C 2x x ! 1 3=2 2 x 2x 2 C x 3 x C 1 f 0 .x/ D 2 3 C 2x f .x/ D



xD 2

3x 2 C x D 2 6x C 2x C 1

x

d dx

 ˇˇ D 2xf .x/ C x 2 f 0 .x/ ˇˇ D 4f .2/ C 4f 0 .2/ D 20

42. xD2

For y D

xC1 we calculate x 1

y0 D

.x

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1/.1/ .x

.x C 1/.1/ D 1/2

2 .x

1/2

:

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 2.3 (PAGE 115)

y

At x D 2 we have y D 3 and y 0 D 2. Thus, the equation of the tangent line is y D 3 2.x 2/, or y D 2x C 7. The normal line is y D 3 C 12 .x 2/, or y D 12 x C 2.



b

a;

1 1 0 , y D1 x x2 1 For horizontal tangent: 0 D y 0 D 1 so x 2 D 1 and x2 x D ˙1 The tangent is horizontal at .1; 2/ and at . 1; 2/

43. y D x C

44. If y D x 2 .4 0

y D 2x.4

Fig. 2.3-47 2

2

3

x / C x . 2x/ D 8x

4x D 4x.2

2

x /:

48.

Thus 2x C 1 D 0 and x D

1 2

The tangent is horizontal only at



xD1

2x C 1 . .x 2 C x C 1/2

49.

˙ 12 ,

or .x C 2/ D

xD1

1 : 2

D

1. Hence, the

3a2 C 4 D .a

2/2 .a C 1/:

The two tangent lines to y D x 3 passing through .2; 8/ correspond to a D 2 and a D 1, so their equations are y D 12x 16 and y D 3x C 2.

1 .x C 2/.1/ .x C 1/.1/ D : .x C 2/2 .x C 2/2 50.

The tangent to y D x 2 =.x mD

1 4:

D

ˇ ˇ ˇ ˇ

3=2 ˇ

The tangent to y D x 3 at .a; a3 / has equation y D a3 C 3a2 .x a/, or y D 3a2 x 2a3 . This line passes through .2; 8/ if 8 D 6a2 2a3 or, equivalently, if a3 3a2 C 4 D 0. Since .2; 8/ lies on y D x 3 , a D 2 must be a solution of this equation. In fact it must be a double root; .a 2/2 must be a factor of a3 3a2 C 4. Dividing by this factor, we find that the other factor is a C 1, that is, a3

2

1 x 2

 The product of the slopes is .2/ 12 D two curves intersect at right angles.

 1 4 ; . 2 3

In order to be parallel to y D 4x, the tangent line must have slope equal to 4, i.e.,

.x

1/ at .a; a2 =.a ˇ 1/2x x 2 .1/ ˇˇ a2 D ˇ 2 ˇ .x 1/ .a xDa

1// has slope 2a : 1/2

The equation of the tangent is 3 2

5 . 2

and x D or At x D Hence x C 2 D y D 1, and at x D 52 , y D 3. Hence, the is parallel to y D 4x at the points  tangent 5 3 ; 1 and ; 3 . 2 2 47.

ˇ dy ˇˇ ˇ dx ˇ

xC1 , then xC2

1 D 4; .x C 2/2

1 Since p D y D x 2 ) x 5=2 D 1, therefore x D 1 at x theˇ intersection point. The slope of y D x 2 at x D 1 is ˇ 1 2x ˇˇ D 2. The slope of y D p at x D 1 is x xD1

2x C 1 2 .x C x C 1/2

For horizontal tangent we want 0 D y 0 D

y0 D



x 2 /, then

1 , y0 D 2 x CxC1

46. If y D

1 a

x

The slope of a horizontal line must be zero, so p 4x.2 x 2 / D 0, which impliesp that x D 0 or x D ˙ 2. At x D 0; y D 0 and at x D ˙ 2; y D 4. Hence, there are two horizontal lines that are tangent to the curve. Their equations are y D 0 and y D 4. 45. y D

1 x

yD

3 , 2

Let the point of tangency be .a; a1 /. The slope of the tanb a1 1 2 gent is D . Thus b a1 D a1 and a D . a2 0 a b b2 b2 so has equation y D b x. Tangent has slope 4 4

y

a2 a

1

D

a2 .a

2a .x 1/2

a/:

This line passes through .2; 0/ provided 0

a2 a

1

D

a2 .a

2a .2 1/2

a/;

or, upon simplification, 3a2 4a D 0. Thus we can have either a D 0 or a D 4=3. There are two tangents through .2; 0/. Their equations are y D 0 and y D 8x C 16.

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51

lOMoARcPSD|6566483

SECTION 2.3 (PAGE 115)

51.

ADAMS and ESSEX: CALCULUS 9

p p f .x C h/ f .x/ h f .x C h/ f .x/ 1 p D lim p h h!0 f .x C h/ C f .x/

d p f .x/ D lim dx h!0

Proof: The case n D 2 is just the Product Rule. Assume the formula holds for n D k for some integer k > 2. Using the Product Rule and this hypothesis we calculate .f1 f2    fk fkC1 /0 D Œ.f1 f2    fk /fkC1 0 0 D .f1 f2    fk /0 fkC1 C .f1 f2    fk /fkC1

f 0 .x/ D p 2 f .x/ 2x x d p 2 x C1D p D p dx 2 x2 C 1 x2 C 1  3 52. f .x/ D jx 3 j D x 3 if x  0 . Therefore f is differenx if x < 0 tiable everywhere except possibly at x D 0, However, f .0 C h/ h h!0C f .0 C h/ lim h h!0 lim

f .0/

D .f10 f2    fk C f1 f20    fk C    C f1 f2    fk0 /fkC1 0 C .f1 f2    fk /fkC1

D f10 f2    fk fkC1 C f1 f20    fk fkC1 C    0 C f1 f2    fk0 fkC1 C f1 f2    fk fkC1

D lim h2 D 0

so the formula is also true for n D k C 1. The formula is therefore for all integers n  2 by induction.

D lim . h2 / D 0:

Section 2.4 The Chain Rule

h!0C

f .0/

h!0

Thus f 0 .0/ exists and equals 0. We have  2 f 0 .x/ D 3x 2 3x

1. 2.

if x  0 if x < 0.

n d n=2 D x .n=2/ 1 for n D 1, 2, 3, : : : . x 53. To be proved: dx 2 Proof: It is already known that the case n D 1 is true: the derivative of x 1=2 is .1=2/x 1=2 . Assume that the formula is valid for n D k for some positive integer k: d k=2 k x D x .k=2/ dx 2

3.

4.

5. 1

:

6. d .kC1/=2 d 1=2 k=2 x D x x dx dx 1 k D x 1=2 x k=2 C x 1=2 x .k=2/ 2 2

f .x/ D .4

x 2 /10

f 0 .x/ D 10.4 d p dy D 1 dx dx  F .t / D 2 C

x 2 /9 . 2x/ D

1

D

k C 1 .kC1/=2 x 2

1

:

d 1 d n=2 x D dx dx x m=2 1 m D m x .m=2/ 1 x 2 n m .m=2/ 1 x D x .n=2/ D 2 2

7.

z D .1 C x 2=3 /3=2

y D 8.

:

.f1 f2    fn /0 D f10 f2    fn C f1 f20    fn C    C f1 f2    fn0

2t 2 /

1=3

.1 C x 2=3 /1=2

y D j1

3 2 .1

x 2 j;

3=2

2t 2 /

5=2

y0 D

. 4t / D 6t .1 2xsgn .1

f .t / D j2 C t 3 j f 0 .t / D Œsgn .2 C t 3 /.3t 2 / D

11.

54. To be proved:

/Dx

4x 3 12 . 4/ D .5 4x/2 .5 4x/2

y D .1

y0 D

10.

1=3

3 5

0

9.

1

yD

x 2 /9

20x.4

3x 6x D p 3x 2 D p 2 2 1 3x 1 3x 2  10 3 t     30 3 11 3 11 3 D 2 C 10 2 C t t2 t2 t

z 0 D 32 .1 C x 2=3 /1=2 . 23 x

Thus the formula is also true for n D k C 1. Therefore it is true for all positive integers n by induction. For negative n D m (where m > 0) we have

52

y D .2x C 3/6 ; y 0 D 6.2x C 3/5 2 D 12.2x C 3/5  x 99 yD 1 3     x 98 1 x 98 D 33 1 y 0 D 99 1 3 3 3

F 0 .t / D

Then, by the Product Rule and this hypothesis,

(page 120)

y D 4x C j4x 1j y 0 D 4 C 4.sgn .4x 1//  8 if x > 14 D 0 if x < 14

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2t 2 /

x2/ D

5=2

2x 3 2x j1 x 2 j

3t 2 .2 C t 3 / j2 C t 3 j

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

12.

y D .2 C jxj3 /1=3

y 0 D 31 .2 C jxj3 /

SECTION 2.4 (PAGE 120)

18. y

.3jxj2 /sgn .x/   x D jxj2 .2 C jxj3 / 2=3 D xjxj.2 C jxj3 / jxj

13.

f .x/ D 1 C

D

D

17.

2 3

r

 z D uC dz D du



3  2 p 2 3x C 4 2 C 3x C 4 r

f .x/ D 4 1 C

16.

yD4xCj4x 1j

slope 0

p

0

15.

slope 8

2=3

1 yD p 2 C 3x C 4   3 1 p y0 D   2 p 2 3x C 4 2 C 3x C 4 D

14.

2=3

x

2 3

r

x

x

2 1

2 3

3



!4

!3

1C

r

1 2 x

r 2

3

3

x !3

!  1 2 3

5=3

u 1    8=3  5 1 1 uC 1 3 u 1 .u 1/2   8=3  5 1 1 1 u C 3 .u 1/2 u 1

p x5 3 C x6 yD .4 C x 2 /3     p 3x 5 1 2 3 4 6 C x5 p 3 C x y0 D .4 C x / 5x .4 C x 2 /6 3 C x6 ! h i p x 5 3 C x 6 3.4 C x 2 /2 .2x/ h i .4 C x 2 / 5x 4 .3 C x 6 / C 3x 10 x 5 .3 C x 6 /.6x/ p D .4 C x 2 /4 3 C x 6 60x 4 3x 6 C 32x 10 C 2x 12 D p .4 C x 2 /4 3 C x 6

21=3

d 1=4 d x D dx dx

q

20.

d 3=4 d x D dx dx

q

21.

3 1 d 3=2 d p 3 x D p .3x 2 / D x 1=2 x D dx dx 2 2 x3

22.

d f .2t C 3/ D 2f 0 .2t C 3/ dt

23.

d f .5x dx

24.

25.

26.

27.

28.

29.

t

x

19.

y

yDj2Ct 3 j



1 4 ;1

p

1 1 1 x D pp  p D x 4 2 x 2 x

p 1 x xD p p 2 x x

x 2 / D .5

2x/f 0 .5x

 p

3=4

x xC p 2 x



D

3 x 4

1=4

x2/

  2       3 2 2 2 2 d D3 f f0 f dx x x x x2     2 6 0 2 2 D f f 2 x x x 2f 0 .x/ d p f 0 .x/ 3 C 2f .x/ D p D p dx 2 3 C 2f .x/ 3 C 2f .x/ p p d 2 f . 3 C 2t / D f 0 . 3 C 2t/ p dt 2 3 C 2t p 1 0 D p f . 3 C 2t / 3 C 2t

p p d 1 f .3 C 2 x/ D p f 0 .3 C 2 x/ dx x    d f 2f 3f .x/ dt      0 D f 2f 3f .x/  2f 0 3f .x/  3f 0 .x/      D 6f 0 .x/f 0 3f .x/ f 0 2f 3f .x/

 d  f 2 3f .4 5t / dx    D f 0 2 3f .4 5t / 3f 0 .4 5t / . 5/   D 15f 0 .4 5t /f 0 2 3f .4 5t /

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53

lOMoARcPSD|6566483

SECTION 2.4 (PAGE 120)

30.

31.

32.

!ˇ x 2 1 ˇˇ ˇ x2 C 1 ˇ xD 2 p x 2 x 2 1.2x/ ˇˇ .x C 1/ p 2 ˇ x 1 D ˇ ˇ .x 2 C 1/2 xD   p 2 p 3. 4/ .5/ 2 3 D p D 25 25 3 p

d dx

ˇ ˇ ˇ 7ˇ ˇ

d p 3t dt

3

tD3

D p 2 3t

1 f .x/ D p 2x C 1 0

f .4/ D 33.

ADAMS and ESSEX: CALCULUS 9

ˇ ˇ 1 ˇ ˇ .2x C 1/3=2 ˇ

ˇ ˇ ˇ ˇ 7ˇ

xD4

tD3

34.

xD 1

The tangent p line at . 1; 23=2 / has equation 3=2 2.x C 1/. yD2

2

38.

b The slope of y D .ax C b/8 at x D is a ˇ ˇ ˇ dy ˇˇ 7ˇ D 8a.ax C b/ ˇ D 1024ab 7 : ˇ ˇ dx ˇ xDb=a

3 D p 2 2

y D .2b/8 D 256b 8 is D

 256b 8 C 1024ab 7 x

y D 210 ab 7 x

1 27

y D .x 3 C 9/17=2 ˇ ˇ ˇ ˇ 17 3 0ˇ 15=2 2ˇ yˇ D .x C 9/ 3x ˇ ˇ ˇ 2

xD 2

D

40.

Given that f .x/ D .x f 0 .x/ D m.x

2.1 C x/.2 C x/.3 C x/3 .4 C x/4 C

D .x

3.1 C x/.2 C x/2 .3 C x/2 .4 C x/4 C

F 0 .0/ D .22 /.33 /.44 / C 2.1/.2/.33 /.44 /C D 4.22  33  44 / D 110; 592

0

y D

D

36. The slope of y D ˇ dy ˇˇ ˇ dx ˇ

1=2  6

ˇ ˇ ˇ D p ˇ 2 1 C 2x 2 ˇ 4x

xD2

D

.x

.x

b/n C n.x n 1

b/

.mx

a/m .x mb C nx

b/n

1

na/:

mb C nx

na D 0;

n m aC b: mCn mCn

This point lies lies between a and b. 41. x.x 4 C 2x 2

2/=.x 2 C 1/5=2

42.

4.7x 4

43.

857; 592

44.

5=8

45.

The Chain Rule does not enable you to calculate the derivatives of jxj2 and jx 2 j at x D 0 directly as a composition of two functions, one of which is jxj, because jxj is not differentiable at x D 0. However, jxj2 D x 2 and jx 2 j D x 2 , so both functions are differentiable at x D 0 and have derivative 0 there.

46.

It may happen that k D g.x C h/ g.x/ D 0 for values of h arbitrarily close to 0 so that the division by k in the “proof” is not justified.

4 : 3

Thus, the equation of the tangent line at .2; 3/ is y D 3 C 43 .x 2/, or y D 43 x C 31 :

54

a/

xD

1 C 2x 2 at x D 2 is

xD2

1

m 1

b/n then

which is equivalent to

   1=2  7 5 6 x C .3x/ 2    3=2   1 .3x/5 2 5.3x/4 3  1 2    3=2  15 6 1 .3x/4 .3x/5 2 2    1=2  7  x C .3x/5 2 p

a/m

mx

3.1/.22 /.32 /.44 / C 4.1/.22 /.33 /.43 / 

a/m .x

If x ¤ a and x ¤ b, then f 0 .x/ D 0 if and only if

4.1 C x/.2 C x/2 .3 C x/3 .4 C x/3

2

 b , or a

Slope of y D 1=.x 2 x Cˇ3/3=2 at x D 2 is ˇ 3 5 3 2 D .x xC3/ 5=2 .2x 1/ˇˇ .9 5=2 /. 5/ D 2 2 162 xD 2 1 The tangent line at . 2; / has equation 27 5 1 C .x C 2/. yD 27 162

F 0 .x/ D .2 C x/2 .3 C x/3 .4 C x/4 C

35.

3  28 b 8 .

b and a

39.

17 .12/ D 102 2

F .x/ D .1 C x/.2 C x/2 .3 C x/3 .4 C x/4

  y D x C .3x/5

xDb=a

The equation of the tangent line at x D y

D

xD 2

37. Slope of y D .1 C x 2=3 /3=2ˇ at x D 1 is   p 2 1=3 ˇˇ 3 .1 C x 2=3 /1=2 x D 2 ˇ ˇ 2 3

49x 2 C 54/=x 7

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 2.5 (PAGE 126)

Section 2.5 Derivatives of Trigonometric Functions (page 126)

24.

1.

d d 1 csc x D D dx dx sin x

cos x D sin2 x

2.

d d cos x cot x D D dx dx sin x

cos2 x sin2 x D sin2 x

y0 D

3. y D cos 3x; 4. y D sin

x ; 5

y0 D

y D cot.4

25. csc 2 x

1 x cos : 5 5

y 0 D 3 csc2 .4

3x/;

26.

3 sin 3x 27. 28.

y 0 D a sec ax tan ax:

6. y D sec ax; 7.

csc x cot x

y 0 D  sec2 x

5. y D tan x;

23.

29.

3x/

 x 1  x d sin D cos dx 3 3 3 9. f .x/ D cos.s rx/; f 0 .x/ D r sin.s 8.

rx/

30.

0

10. y D sin.Ax C B/;

y D A cos.Ax C B/

d sin.x 2 / D 2x cos.x 2 / dx p p d 1 12. cos. x/ D p sin. x/ dx 2 x p sin x 13. y D 1 C cos x; y 0 D p 2 1 C cos x 11.

14.

15.

16.

31. 32.

d sin.2 cos x/ D cos.2 cos x/. 2 sin x/ dx D 2 sin x cos.2 cos x/

f .x/ D cos.x C sin x/ f 0 .x/ D .1 C cos x/ sin.x C sin x/

33.

g. / D tan. sin  /

34.

g 0 . / D .sin  C  cos  / sec2 . sin  / 17.

u D sin3 .x=2/;

18. y D sec.1=x/; 19.

u0 D y0 D

F .t / D sin at cos at 0

F .t / D a cos at cos at . D a cos 2at / 20.

21. 22.

3 cos.x=2/ sin2 .x=2/ 2

.1=x 2 / sec.1=x/ tan.1=x/ 1 sin 2at / 2 a sin at sin at

.D

35. 36.

sin a cos b a cos b cos a C b sin a sin b G 0 . / D : cos2 b  d  sin.2x/ cos.2x/ D 2 cos.2x/ C 2 sin.2x/ dx d d .cos2 x sin2 x/ D cos.2x/ dx dx D 2 sin.2x/ D 4 sin x cos x G. / D

d .tan x C cot x/ D sec2 x csc2 x dx d .sec x csc x/ D sec x tan x C csc x cot x dx d .tan x x/ D sec2 x 1 D tan2 x dx d d tan.3x/ cot.3x/ D .1/ D 0 dx dx d .t cos t sin t / D cos t t sin t cos t D t sin t dt d .t sin t C cos t / D sin t C t cos t sin t D t cos t dt d .1 C cos x/.cos x/ sin.x/. sin x/ sin x D dx 1 C cos x .1 C cos x/2 1 cos x C 1 D D 2 .1 C cos x/ 1 C cos x d cos x .1 C sin x/. sin x/ cos.x/.cos x/ D dx 1 C sin x .1 C sin x/2 sin x 1 1 D D .1 C sin x/2 1 C sin x

d 2 x cos.3x/ D 2x cos.3x/ 3x 2 sin.3x/ dx p g.t / D .sin t /=t t cos t sin t 1  g 0 .t / D p t2 2 .sin t /=t t cos t sin t D p 2t 3=2 sin t v D sec.x 2 / tan.x 2 /

v 0 D 2x sec.x 2 / tan2 .x 2 / C 2x sec3 .x 2 / p sin x zD p 1 C cos x p p p p p p .1 C cos x/.cos x=2 x/ .sin x/. sin x=2 x/ p 2 z0 D .1 C cos x/ p 1 1 C cos x D p p p D p 2 x.1 C cos x/2 2 x.1 C cos x/

d sin.cos.tan t // D dt

.sec2 t /.sin.tan t // cos.cos.tan t //

f .s/ D cos.s C cos.s C cos s// f 0 .s/ D Œsin.s C cos.s C cos s//  Œ1 .sin.s C cos s//.1 sin s/

37. Differentiate both sides of sin.2x/ D 2 sin x cos x and divide by 2 to get cos.2x/ D cos2 x sin2 x.

sin2 x and

38.

Differentiate both sides of cos.2x/ D cos2 x divide by 2 to get sin.2x/ D 2 sin x cos x.

39.

Slope of y D sin x at .; 0/ is cos  D 1. Therefore the tangent and normal lines to y D sin x at .; 0/ have equations y D .x / and y D x , respectively.

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SECTION 2.5 (PAGE 126)

ADAMS and ESSEX: CALCULUS 9

40. The slope of y D tan.2x/ at .0; 0/ is 2 sec2 .0/ D 2. Therefore the tangent and normal lines to y D tan.2x/ at .0; 0/ have equations y D 2x and y D x=2, respectively. p 41. Thepslope of y D 2 cos.x=4/ at .; 1/ is . 2=4/ sin.=4/ Dp 1=4. Therefore the tangent and normal lines to y D 2 cos.x=4/ at .; 1/ have equations y D 1 .x /=4 and y D 1 C 4.x /, respectively.

42. The slope of y Dpcos2 x at .=3; 1=4/ is sin.2=3/ D 3=2. Therefore the tangent and normal lines to y D tan.2x/ at .0; 0/ have equations p y D .1=4/ . 3=2/.x .=3// and p y D .1=4/ C .2= 3/.x .=3//, respectively.  x   x   is y 0 D cos . 43. Slope of y D sin.x ı / D sin 180 180 180 At x D 45 the tangent line has equation 1  yD p C p .x 45/. 2 180 2  x  44. For y D sec .x ı / D sec we have 180  x   x   dy D sec tan : dx 180 180 180

p  p  3 .2 3/ D : 180 90 90 Thus, the normal line has slope p and has equation  3 90 yD2 p .x 60/.  3

49.

y D x C sin x has a horizontal tangent at x D  because dy=dx D 1 C cos x D 0 there.

50.

y D 2x C sin x has no horizontal tangents because dy=dx D 2 C cos x  1 everywhere.

51.

y D x C 2 sin x has horizontal tangents at x D 2=3 and x D 4=3 because dy=dx D 1 C 2 cos x D 0 at those points.

52.

y D x C 2 cos x has horizontal tangents at x D =6 and x D 5=6 because dy=dx D 1 2 sin x D 0 at those points.

53. 54.

2 sin.2x/ t an.2x/ D lim D12D2 x!0 x 2x cos.2x/

lim sec.1 C cos x/ D sec.1

x!

55. 56.

57. 58.

At x D 60 the slope is

45. The slope of y D tan x at x D a is sec2 a. The tangent there is parallel to y D 2x if sec2 a D 2, or p cos a D ˙1= 2. The only solutions in . =2; =2/ are a D ˙=4. The corresponding points on the graph are .=4; 1/ and . =4; 1/.

lim

x!0

 x 2 cos x D 12  1 D 1 x!0 x!0 sin x       cos2 x sin x 2 lim cos D cos  D 1 D lim cos  x!0 x!0 x2 x   1 2 sin2 .h=2/ 1 sin.h=2/ 2 1 cos h D D lim D lim lim h2 h2 h=2 2 h!0 h!0 2 h!0 lim x 2 csc x cot x D lim

f will be differentiable at x D 0 if 2 sin 0 C 3 cos 0 D b; and ˇ ˇ d D a: .2 sin x C 3 cos x/ˇˇ dx xD0

Thus we need b D 3 and a D 2. 59.

There are infinitely many lines through the origin that are tangent to y D cos x. The two with largest slope are shown in the figure. y

46. The slope of y D tan.2x/ at x D a is 2 sec2 .2a/. The tangent there is normal to y D x=8 if 2 sec2 .2a/ D 8, or cos.2a/ D ˙1=2. The only solutions in . =4; =4/ are a D points on the graph are p ˙=6. The corresponding p .=6; 3/ and . =6; 3/. 47.

48.



56



2 x

y D cos x

d sin x D cos x D 0 at odd multiples of =2. dx d cos x D sin x D 0 at multiples of . dx d sec x D sec x tan x D 0 at multiples of . dx d csc x D csc x cot x D 0 at odd multiples of =2. dx Thus each of these functions has horizontal tangents at infinitely many points on its graph. d tan x D sec2 x D 0 nowhere. dx d cot x D csc2 x D 0 nowhere. dx Thus neither of these functions has a horizontal tangent.

1/ D sec 0 D 1

Fig. 2.5-59 The tangent to y D cos x at x D a has equation y D cos a .sin a/.x a/. This line passes through the origin if cos a D a sin a. We use a calculator with a “solve” function to find solutions of this equation near a D  and a D 2 as suggested in the figure. The solutions are a  2:798386 and a  6:121250. The slopes of the corresponding tangents are given by sin a, so they are 0:336508 and 0:161228 to six decimal places. 60. 61.

1 p

2 C 3.2 3=2

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4 C 3/=

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INSTRUCTOR’S SOLUTIONS MANUAL

62.

SECTION 2.6 (PAGE 131)

a) As suggested by the figure in the problem, the square of the length of chord AP is .1 cos  /2 C.0 sin  /2 , and the square of the length of arc AP is  2 . Hence

5.

y D x 1=3 x 1=3 1 1 y 0 D x 2=3 C x 4=3 3 3 2 5=3 4 7=3 00 y D x x 9 9 10 8=3 28 10=3 x C x y 000 D 27 27

6.

y D x 10 C 2x 8

.1 C cos  /2 C sin2  <  2 ; and, since squares cannot be negative, each term in the sum on the left is less than  2 . Therefore 0  j1

cos  j < j j;

0

y D 10x C 16x

0  j sin  j < j j: 7.

Since lim!0 j j D 0, the squeeze theorem implies that lim 1 cos  D 0; lim sin  D 0: !0

!0

From the first of these, lim!0 cos  D 1. b) Using the result of (a) and the addition formulas for cosine and sine we obtain 8. lim cos.0 C h/ D lim .cos 0 cos h

h!0

h!0

sin 0 sin h/ D cos 0

lim sin.0 C h/ D lim .sin 0 cos h C cos 0 sin h/ D sin 0 :

h!0

h!0

9. This says that cosine and sine are continuous at any point 0 .

y D .3

1.

0

2.

3.

14.3

2x/6

y 00 D 168.3

2x/5

000

1680.3

D

12.

2x/4

1 x 1 y 0 D 2x C 2 x

y 000 D

6 D 6.x .x 1/2 0 y D 12.x 1/ 3 yD

y 000 D

1/

144.x

p ax C b a y0 D p 2 ax C b yD

2 x3

y 00 D 2

y D x2

y 00 D 36.x

4.

2x/

y D

y

x 1 xC1 2 0 y D .x C 1/2

6 x4

1/

13.

2

2

1/

a2 4.ax C b/3=2 3a3 D 8.ax C b/5=2

y 000

y 000 D sec x tan3 x C 5 sec3 x tan x

y D cos.x 2 /

y 00 D

2x sin.x 2 /

y 000 D

2 sin.x 2 /

4x 2 cos.x 2 /

12x cos.x 2 / C 8x 3 sin.x 2 /

sin x x cos x sin x 0 y D x x2 2 .2 x / sin x 2 cos x y 00 D x3 x2 2 2 3.x 2/ sin x .6 x / cos x C y 000 D 3 4 x x yD

1 Dx x f 0 .x/ D x 2 f .x/ D

.4/

y 00 D

y 00 D sec x tan2 x C sec3 x

y D sec x y 0 D sec x tan x

f 000 .x/ D

5

y 000

y 000 D 2 sec4 x C 4 sec2 x tan2 x

f 00 .x/ D 2x

4

4 .x C 1/3 12 D .x C 1/4

y 00 D

y 00 D 2 sec2 x tan x

y D tan x

y0 D

7

y 000 D 720x 7 C 672x 5

yD

y D sec x

11.

y 00 D 90x 8 C 112x 6

7

p y D .x 2 C 3/ x D x 5=2 C 3x 1=2 5 3 y 0 D x 3=2 C x 1=2 2 2 15 1=2 3 3=2 y 00 D x x 4 4 15 1=2 9 5=2 x C x y 000 D 8 8

0

10.

Section 2.6 Higher-Order Derivatives (page 131)

9

1

3

3Šx

4

5

f .x/ D 4Šx Guess: f .n/ .x/ D . 1/n nŠx .nC1/ ./ Proof: (*) is valid for n D 1 (and 2, 3, 4). .kC1/ Assume f .k/ .x/ D . 1/k kŠx for   some k  1 .kC1/ k Then f .x/ D . 1/ kŠ .k C 1/ x .kC1/ 1

D . 1/kC1 .k C 1/Šx ..kC1/C1/ which is (*) for n D k C 1. Therefore, (*) holds for n D 1; 2; 3; : : : by induction.

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SECTION 2.6 (PAGE 131)

14.

1 Dx 2 x2 f 0 .x/ D 2x 3 f 00 .x/ D 2. 3/x 4 D 3Šx 4 f .3/ .x/ D 2. 3/. 4/x 5 D 4Šx Conjecture:

ADAMS and ESSEX: CALCULUS 9

Thus, the formula is also true for n D k C 1. Hence, it is true for n  2 by induction.

f .x/ D

f .n/ .x/ D . 1/n .n C 1/Šx

17.

5

.nC2/

f 00 .x/ D 2b 2 .a C bx/

for n D 1; 2; 3; : : :

f .kC1/ .x/ D

D . 1/kC1 .k C 2/Šx

Œ.kC1/C2

.kC2/ 1

15.

D .2 2 x f 0 .x/ D C.2 x/ 2 f .x/ D

f 00 .x/ D 2.2

x/

x/

18. f .x/ D x 2=3 f 0 .x/ D 32 x f 00 .x/ D 32 . f 000 .x/ D 32 . Conjecture:

1

3

D .k C 1/Š.2 x/ : Thus (*) holds for n D k C 1 if it holds for k. Therefore, (*) holds for n D 1; 2; 3; : : : by induction. p 16. f .x/ D x D x 1=2 f 0 .x/ D 21 x 1=2 f 00 .x/ D 12 . 12 /x 3=2 f 000 .x/ D 21 . 12 /. 32 /x 5=2 f .4/ .x/ D 21 . 12 /. 32 /. 25 /x 7=2 Conjecture:  3  5    .2n 2n

3/

x

.2n 1/=2

11

 3  5    .2k 2k

3/

x

 4  7     .3k 3k

5/

x

.3k 2/=3

d .k/ f .x/ dx   .3k 2/ 1  4  7     .3k 5/  D 2. 1/k 1 x Œ.3k 2/=3 3 3k 1  4  7     .3k 5/Œ3.k C 1/ 5 Œ3.kC1/ x D 2. 1/.kC1/ 1 3. k C 1/

:

19. f 00 .x/ D

:

d .k/ f .kC1/ .x/ D f .x/ dx   .2k 1/ 1  3  5    .2k 3/  D . 1/k 1 x Œ.2k 1/=2 2 2k 1  3  5    .2k 3/Œ2.k C 1/ 3 Œ2.kC1/ x D . 1/.kC1/ 1 2kC1

1

2=3

:

Thus, the formula is also true for n D k C 1. Hence, it is true for n  2 by induction.

Then

58

11

f .kC1/ .x/ D

.n  2/:

.2k 1/=2

1 4=3 3 /x 1 4 7=3 3 /. 3 /x

Then,

Proof: Evidently, the above formula holds for n D 2; 3 and 4. Assume that it holds for n D k, i.e. f .k/ .x/ D . 1/k

.b/

1=3

f .k/ .x/ D 2. 1/k

..kC1/C1/

11

1

1  4  7     .3n 5/ .3n 2/=3 f .n/ .x/ D 2. 1/n 1 x for 3n n  2. Proof: Evidently, the above formula holds for n D 2 and 3. Assume that it holds for n D k, i.e.

f 000 .x/ D C3Š.2 x/ 4 Guess: f .n/ .x/ D nŠ.2 x/ .nC1/ ./ Proof: (*) holds for n D 1; 2; 3. Assume f .k/ .x/ D kŠ.2 x/ .kC1/ (i.e., (*) holds for n D k)   Then f .kC1/ .x/ D kŠ .k C 1/.2 x/ .kC1/ 1 . 1/

f .n/ .x/ D . 1/n

3

D . 1/kC1 .k C 1/Šb kC1 .a C bx/..kC1/C1/ So (*) holds for n D k C 1 if it holds for n D k. Therefore, (*) holds for n D 1; 2; 3; 4; : : : by induction.

:

Thus, the formula is also true for n D k C 1. Hence it is true for n D 1; 2; 3; : : : by induction. 1

1

f 000 .x/ D 3Šb 3 .a C bx/ 4 Guess: f .n/ .x/ D . 1/n nŠb n .a C bx/ .nC1/ ./ Proof: (*) holds for n D 1; 2; 3 Assume (*) holds for n D k: f .k/ .x/ D . 1/k kŠb k .a C bx/ .kC1/ Then   f .kC1/ .x/ D . 1/k kŠb k .k C 1/ .a C bx/ .kC1/

Proof: Evidently, the above formula holds for n D 1; 2 and 3. Assume it holds for n D k, i.e., f .k/ .x/ D . 1/k .k C 1/Šx .kC2/ : Then d .k/ f .x/ dx D . 1/k .k C 1/ŠŒ. 1/.k C 2/x

1 D .a C bx/ a C bx f 0 .x/ D b.a C bx/ 2 f .x/ D

f .x/ D cos.ax/ f 0 .x/ D a sin.ax/

a2 cos.ax/

f 000 .x/ D a3 sin.ax/

f .4/ .x/ D a4 cos.ax/ D a4 f .x/ It follows that f .n/ .x/ D a4 f .n 4/ .x/ for n  4, and 1

1=2

:

8 n a cos.ax/ ˆ < n a sin.ax/ .n/ f .x/ D n ˆ : a cos.ax/ n a sin.ax/

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if if if if

n D 4k n D 4k C 1 .k D 0; 1; 2; : : :/ n D 4k C 2 n D 4k C 3

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 2.6 (PAGE 131)

Differentiating any of these four formulas produces the one for the next higher value of n, so induction confirms the overall formula. 20.

f .x/ D x cos x f 0 .x/ D cos x x sin x f 00 .x/ D 2 sin x x cos x f 000 .x/ D 3 cos x C x sin x

The pattern suggests that  nŠjxj .nC1/ sgn x f .n/ .x/ D nŠjxj .nC1/

23.

f .4/ .x/ D 4 sin x C x cos x This suggests the formula (for k D 0; 1; 2; : : :) 8 n sin x C x cos x ˆ < n cos x x sin x .n/ f .x/ D ˆ : n sin x x cos x n cos x C x sin x

if if if if

n D 4k n D 4k C 1 n D 4k C 2 n D 4k C 3

Differentiating any of these four formulas produces the one for the next higher value of n, so induction confirms the overall formula. 21.

f .x/ D x sin.ax/ f 0 .x/ D sin.ax/ C ax cos.ax/

f 00 .x/ D 2a cos.ax/ 000

f .x/ D

2

3a sin.ax/

a2 x sin.ax/ a3 x cos.ax/

f 4/ .x/ D 4a3 cos.ax/ C a4 x sin.ax/ This suggests the formula 8 nan 1 cos.ax/ C an x sin.ax/ ˆ ˆ < n 1 na sin.ax/ C an x cos.ax/ f .n/ .x/ D n 1 ˆ na cos.ax/ an x sin.ax/ ˆ : nan 1 sin.ax/ an x cos.ax/

if if if if

n D 4k n D 4k C 1 n D 4k C 2 n D 4k C 3

for k D 0; 1; 2; : : :. Differentiating any of these four formulas produces the one for the next higher value of n, so induction confirms the overall formula.

22. f .x/ D

1 D jxj jxj

1

. Recall that

f 0 .x/ D

jxj

24.

sgn x:

25.

f 00 .x/ D 2jxj

3

3Šjxj

.sgn x/ D 1:

.x/ D 4Šjxj

.sgn x/2 D 2jxj

5

4

:

D k 2 y.2 sec2 .kx/

2

Thus we can calculate successive derivatives of f using the product rule where necessary, but will get only one nonzero term in each case:

f

If y D sec.kx/, then y 0 D k sec.kx/ tan.kx/ and y 00 D k 2 .sec2 .kx/ tan2 .kx/ C sec3 .kx//

d sgn x D 0 and dx

.4/

If y D tan.kx/, then y 0 D k sec2 .kx/ and

D 2k 2 .1 C tan2 .kx// tan.kx/ D 2k 2 y.1 C y 2 /:

If x ¤ 0 we have

f .3/ .x/ D

Differentiating this formula leads to the same formula with n replaced by n C 1 so the formula is valid for all n  1 by induction. p f .x/ D 1 3x D .1 3x/1=2 1 f 0 .x/ D . 3/.1 3x/ 1=2 2  1 1 f 00 .x/ D . 3/2 .1 3x/ 3=2 2 2    1 3 1 . 3/3 .1 3x/ 5=2 f 000 .x/ D 2 2 2     1 1 3 5 f .4/ .x/ D . 3/4 .1 3x/7=2 2 2 2 2 1  3  5      .2n 3/ n 3 Guess: f .n/ .x/ D 2n .2n 1/=2 .1 3x/ ./ Proof: (*) is valid for n D 2; 3; 4; (but not n D 1) Assume (*) holds for n D k for some integer k  2 1  3  5  : : :  .2k 3/ k i.e., f .k/ .x/ D 3 2k .1 3x/ .2k 1/=2 1  3  5      .2k 3/ k .kC1/ Then f .x/ D 3 2k   2.k 1/ .1 3x/ .2k 1/=2 1 . 3/ 2   1  3  5     2.k C 1/ 1 D 3kC1 2kC1 .1 3x/ .2.kC1/ 1/=2 Thus (*) holds for n D k C 1 if it holds for n D k. Therefore, (*) holds for n D 2; 3; 4; : : : by induction. y 00 D 2k 2 sec 2 .kx/t an.kx/

d jxj D sgn x, so dx 2

if n is odd if n is even

sgn x

3

26.

1/ D k 2 y.2y 2

1/:

To be proved: if f .x/ D sin.ax C b/, then  . 1/k an sin.ax C b/ if n D 2k f .n/ .x/ D . 1/k an cos.ax C b/ if n D 2k C 1 for k D 0; 1; 2; : : : Proof: The formula works for k D 0 (n D 2  0 D 0 and n D 2  0 C 1 D 1):  f .0/ .x/ D f .x/ D . 1/0 a0 sin.ax C b/ D sin.ax C b/ f .1/ .x/ D f 0 .x/ D . 1/0 a1 cos.ax C b/ D a cos.ax C b/

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ADAMS and ESSEX: CALCULUS 9

Section 2.7 Using Differentials and Derivatives (page 137)

Now assume the formula holds for some k  0. If n D 2.k C 1/, then f .n/ .x/ D

d .n f dx

1/

d .2kC1/ f .x/ dx   d D . 1/k a2kC1 cos.ax C b/ dx

.x/ D

D . 1/kC1 a2kC2 sin.ax C b/

and if n D 2.k C 1/ C 1 D 2k C 3, then  d . 1/kC1 a2kC2 sin.ax C b/ f .n/ .x/ D dx

1.

2.

3.

D . 1/kC1 a2kC3 cos.ax C b/:

27.

0:01 1 dx D D 0:0025. y  dy D x2 22 If x D 2:01, then y  0:5 0:0025 D 0:4975. 3 dx 3 f .x/  df .x/ D p D .0:08/ D 0:06 4 2 3x C 1 f .1:08/  f .1/ C 0:06 D 2:06.

 t  1 1 h.t /  dh.t / D sin dt .1/ D . 4 4 4 10 40   1 1 1 D :  h.2/ h 2C 10 40 40 s 1 1 u  du D sec2 ds D .2/. 0:04/ D 0:04. 4 4 4 If s D  0:06, then u  1 0:04  0:96.

Thus the formula also holds for k C 1. Therefore it holds for all positive integers k by induction.

4.

If y D tan x, then

5.

If y D x 2 , then y  dy D 2x dx. If dx D .2=100/x, then y  .4=100/x 2 D .4=100/y, so y increases by about 4%.

6.

If y D 1=x, then y  dy D . 1=x 2 / dx. If dx D .2=100/x, then y  . 2=100/=x D . 2=100/y, so y decreases by about 2%.

7.

If y D 1=x 2 , then y  dy D . 2=x 3 / dx. If dx D .2=100/x, then y  . 4=100/=x 2 D . 4=100/y, so y decreases by about 4%.

8.

If y D x 3 , then y  dy D 3x 2 dx. If dx D .2=100/x, then y  .6=100/x 3 D .6=100/y, so y increases by about 6%. p p x, then dy  dy D .1=2 If y D p x/ dx. If x D .2=100/x, then y  .1=100/ x D .1=100/y, so y increases by about 1%.

y 0 D sec2 x D 1 C tan2 x D 1 C y 2 D P2 .y/; where P2 is a polynomial of degree 2. Assume that y .n/ D PnC1 .y/ where PnC1 is a polynomial of degree n C 1. The derivative of any polynomial is a polynomial of one lower degree, so y .nC1/ D

dy d PnC1 .y/ D Pn .y/ D Pn .y/.1Cy 2 / D PnC2 .y/; dx dx

a polynomial of degree n C 2. By induction, .d=dx/n tan x D PnC1 .tan x/, a polynomial of degree n C 1 in tan x. 28.

.fg/00 D .f 0 g C fg 0 / D f 00 g C f 0 g 0 C f 0 g 0 C fg 00 D f 00 g C 2f 0 g 0 C fg 00

29.

.fg/.3/ D

d .fg/00 dx d D Œf 00 g C 2f 0 g 0 C fg 00  dx D f .3/ g C f 00 g 0 C 2f 00 g 0 C 2f 0 g 00 C f 0 g 00 C fg .3/ .3/

.4/

.fg/

00 0

0 00

C 3f 0 g .3/ C f 0 g .3/ C fg .4/

D f .4/ g C 4f .3/ g 0 C 6f 00 g 00 C 4f 0 g .3/ C fg .4/ : nŠ f .n 2/ g 00 .fg/.n/ D f .n/ g C nf .n 1/g 0 C 2Š.n 2/Š nŠ f .n 3/ g .3/ C    C nf 0 g .n 1/ C fg .n/ C 3Š.n 3/Š n X nŠ f .n k/ g .k/ : D kŠ.n k/Š

60

10. If y D x 2=3 , then y  dy D . 2=3/x 5=3 dx. If dx D .2=100/x, then y  . 4=300/x 2=3 D . 4=300/y, so y decreases by about 1.33%. 11.

.3/

D f g C 3f g C 3f g C fg : d .fg/.3/ D dx d D Œf .3/ g C 3f 00 g 0 C 3f 0 g 00 C fg .3/  dx D f .4/ g C f .3/ g 0 C 3f .3/ g 0 C 3f 00 g 00 C 3f 00 g 00

kD0

9.

If V D 34  r 3 , then V  d V D 4 r 2 dr. If r increases by 2%, then dr D 2r=100 and V  8 r 3 =100. Therefore V =V  6=100. The volume increases by about 6%.

12. If V is the volume and x is the edge length of the cube then V D x 3 . Thus V  d V D 3x 2 x. If V D .6=100/V , then 6x 3 =100  3x 2 dx, so dx  .2=100/x. The edge of the cube decreases by about 2%. 13.

14.

Rate change of Area A with respect to side s, where dA A D s 2 , is D 2s: When s D 4 ft, the area is changing ds 2 at rate 8 ft /ft. p p If A D s 2 , then s D A and ds=dA D 1=.2 A/. If A D 16 m2 , then the side is changing at rate ds=dA D 1=8 m/m2 .

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15.

SECTION 2.7 (PAGE 137)

The diameter D and area A of a circle are related by p D D 2 A=. The rate of change of diameter with respect p to area is dD=dA D 1=.A/ units per square unit.

The flow rate will increase by 10% if the radius is increased by about 2.5%. 23.

F D k=r 2 implies that dF=dr D 2k=r 3 . Since dF=dr D 1 pound/mi when r D 4; 000 mi, we have 2k D 4; 0003 . If r D 8; 000, we have dF=dr D .4; 000=8; 000/3 D 1=8. At r D 8; 000 mi F decreases with respect to r at a rate of 1/8 pounds/mi.

24.

If price = $p, then revenue is $R D 4; 000p

16. Since A D D 2 =4, the rate of change of area with respect to diameter is dA=dD D D=2 square units per unit. 17.

Rate of change of V D

4 3  r with respect to radius r is 3

dV D 4 r 2 . When r D 2 m, this rate of change is 16 dr 3 m /m.

a) Sensitivity of R to p is dR=dp D 4; 000 20p. If p D 100, 200, and 300, this sensitivity is 2,000 $/$, 0 $/$, and 2; 000 $/$ respectively.

18. Let A be the area of a square, s be its side length and L be its diagonal. Then, L2 D s 2 C s 2 D 2s 2 and dA D L. Thus, the rate of change of A D s 2 D 12 L2 , so dL the area of a square with respect to its diagonal L is L.

b) The distributor should charge $200. This maximizes the revenue. 25.

19. If the radius of the circle is r then C D 2 r and A D  r 2. r p p A Thus C D 2 D 2  A.  Rate of p change of C with respect to A is  dC 1 D p D . dA r A 20. Let s be the side length and V be the volume of a cube. ds D 31 V 2=3 . Hence, Then V D s 3 ) s D V 1=3 and dV the rate of change of the side length of a cube with respect to its volume V is 31 V 2=3 . 21.

ˇ ˇ ˇ ˇ ˇ

tD5

D

700.20

ˇ ˇ ˇ t /ˇ ˇ

tD5

D

26.

ˇ ˇ ˇ ˇ ˇ

tD15

D

700.20

ˇ ˇ ˇ t /ˇ ˇ

tD15

b) To maximize daily profit, production should be 800 sheets/day.

10; 500:

D

27.

3; 500:

b) Average rate of change between t D 5 and t D 15 is 350  .25 V .5/ D 5 10

225/

D

80; 000 n2 C 4n C n 100 n 80; 000 dC C4C : D dn n2 50 dC (a) n D 100; D 2. Thus, the marginal cost of dn production is $2.

C D

82 dC D  9:11. Thus, the marginal cost dn 9 of production is approximately $9.11.

(b) n D 300;

Water is draining out at 3,500 L/min at that time.

V .15/ 15

Daily profit if production is x sheets per day is $P .x/ where P .x/ D 8x 0:005x 2 1; 000: a) Marginal profit P 0 .x/ D 8 0:01x. This is positive if x < 800 and negative if x > 800.

Water is draining out at 10,500 L/min at that time. At t D 15, water volume is changing at rate dV dt

0:5x 2 if x units are

b) C.101/ C.100/ D 43; 299:50 43; 000 D $299:50 which is approximately C 0 .100/.

a) At t D 5, water volume is changing at rate dV dt

Cost is $C.x/ D 8; 000 C 400x manufactured. a) Marginal cost if x D 100 is C 0 .100/ D 400 100 D $300.

t /2 L at t min.

Volume in tank is V .t / D 350.20

10p 2 .

7; 000:

The average rate of draining is 7,000 L/min over that interval. 22. Flow rate F D kr 4 , so F  4kr 3 r. If F D F=10, then kr 4 F D D 0:025r: r  3 40kr 40kr 3

28.

Daily profit P D 13x

C x D 13x

10x

20

x2 1000

x2 D 3x 20 1000 Graph of P is a parabola opening downward. P will be maximum where the slope is zero: 0D

dP D3 dx

2x so x D 1500 1000

Should extract 1500 tonnes of ore per day to maximize profit.

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ADAMS and ESSEX: CALCULUS 9

29. One of the components comprising C.x/ is usually a fixed cost, $S, for setting up the manufacturing operation. On a per item basis, this fixed cost $S=x, decreases as the number x of items produced increases, especially when x is small. However, for large x other components of the total cost may increase on a per unit basis, for instance labour costs when overtime is required or maintenance costs for machinery when it is over used. C.x/ Let the average cost be A.x/ D . The minimal avx erage cost occurs at point where the graph of A.x/ has a horizontal tangent: 0D

r

30. If y D Cp

If f .x/ D cos x C .x 2 =2/, then f 0 .x/ D x sin x > 0 for x > 0. By the MVT, if x > 0, then f .x/ f .0/ D f 0 .c/.x 0/ for some c > 0, so f .x/ > f .0/ D 1. Thus cos x C .x 2 =2/ > 1 and cos x > 1 .x 2 =2/ for x > 0. Since both sides of the inequality are even functions, it must hold for x < 0 as well.

5.

Let f .x/ D tan x. If 0 < x < =2, then by the MVT f .x/ f .0/ D f 0 .c/.x 0/ for some c in .0; =2/. Thus tan x D x sec2 c > x, since secc > 1.

6.

dA xC 0 .x/ C.x/ : D dx x2

C.x/ D A.x/. x Thus the marginal cost C 0 .x/ equals the average cost at the minimizing value of x.

Hence, xC 0 .x/

4.

C.x/ D 0 ) C 0 .x/ D

7.

f .x/ f .0/ D f 0 .c/ x 0 .1 x/r 1 D r.1 C c/r ) x

p Cp

r

. r/Cp

r 1

D r:

f .x/ D x 2 ; b2 b

.1 C c/r

1

r 1

rx.1 C c/

>1

.since r

< rx

f .b/ a2 D a b

f .a/ a bCa )cD 2

c>0 1Cc >1

.1 C c/r

1

r 1

2. If f .x/ D

1 , and f 0 .x/ D x

f .2/ 2 where c D

p

f .1/ 1 D 1 2

rx.1 C c/

1 then x2 1D

1 D 2

1 D f 0 .c/ c2

0. 8.

If f .x/ D x 3 12x C 1, then f 0 .x/ D 3.x 2 4/. The critical points of f are x D ˙2. f is increasing on . 1; 2/ and .2; 1/ where f 0 .x/ > 0, and is decreasing on . 2; 2/ where f 0 .x/ < 0.

9.

If f .x/ D x 2 4, then f 0 .x/ D 2x. The critical point of f is x D 0. f is increasing on .0; 1/ and decreasing on . 1; 0/.

2 lies between 1 and 2.

3. f .x/ D x 3 3x C 1, f 0 .x/ D 3x 2 3, a D 2, b D 2 f .b/ f .a/ f .2/ f . 2/ D b a 4 8 6 C 1 . 8 C 6 C 1/ D 4 4 D D1 4 0 2 f .c/ D 3c 3 2 3c 2 3 D 1 ) 3c 2 D 4 ) c D ˙ p 3 (Both points will be in . 2; 2/.)

62

1 < 0/;

.since x < 0/:

Hence, .1 C x/r < 1 C rx. If x > 0, then

f 0 .x/ D 2x

D f 0 .c/ D 2c

1

for some c between 0 and x. Thus, .1 C x/r D 1 C rx.1 C c/r 1 . If 1  x < 0, then c < 0 and 0 < 1 C c < 1. Hence

Section 2.8 The Mean-Value Theorem (page 144)

bCa D

Let f .x/ D .1 C x/r where 0 < r < 1. Thus, f 0 .x/ D r.1 C x/r 1 . By the Mean-Value Theorem, for x  1, and x ¤ 0,

, then the elasticity of y is p dy D y dp

1.

Let f .x/ D .1 C x/r 1 rx where r > 1. Then f 0 .x/ D r.1 C x/r 1 r. If 1  x < 0 then f 0 .x/ < 0; if x > 0, then f 0 .x/ > 0. Thus f .x/ > f .0/ D 0 if 1  x < 0 or x > 0. Thus .1 C x/r > 1 C rx if 1  x < 0 or x > 0.

10. If y D 1 x x 5 , then y 0 D 1 5x 4 < 0 for all x. Thus y has no critical points and is decreasing on the whole real line. 11.

If y D x 3 C 6x 2 , then y 0 D 3x 2 C 12x D 3x.x C 4/. The critical points of y are x D 0 and x D 4. y is increasing on . 1; 4/ and .0; 1/ where y 0 > 0, and is decreasing on . 4; 0/ where y 0 < 0.

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SECTION 2.8 (PAGE 144)

12. If f .x/ D x 2 C 2x C 2 then f 0 .x/ D 2x C 2 D 2.x C 1/. Evidently, f 0 .x/ > 0 if x > 1 and f 0 .x/ < 0 if x < 1. Therefore, f is increasing on . 1; 1/ and decreasing on . 1; 1/.

22.

There is no guarantee that the MVT applications for f and g yield the same c.

23.

CPs x D 0:535898 and x D 7:464102

13. f .x/ D x 3 4x C 1 f 0 .x/ D 3x 2 4

24.

CPs x D

1:366025 and x D 0:366025

25.

CPs x D

0:518784 and x D 0

26.

CP x D 0:521350

27.

If x1 < x2 < : : : < xn belong to I , and f .xi / D 0, .1  i  n/, then there exists yi in .xi ; xiC1 / such that f 0 .yi / D 0, .1  i  n 1/ by MVT.

28.

For x ¤ 0, we have f 0 .x/ D 2x sin.1=x/ cos.1=x/ which has no limit as x ! 0. However, f 0 .0/ D limh!0 f .h/= h D limh!0 h sin.1= h/ D 0 does exist even though f 0 cannot be continuous at 0.

29.

If f 0 exists on Œa; b and f 0 .a/ ¤ f 0 .b/, let us assume, without loss of generality, that f 0 .a/ > k > f 0 .b/. If g.x/ D f .x/ kx on Œa; b, then g is continuous on Œa; b because f , having a derivative, must be continuous there. By the Max-Min Theorem, g must have a maximum value (and a minimum value) on that interval. Suppose the maximum value occurs at c. Since g 0 .a/ > 0 we must have c > a; since g 0 .b/ < 0 we must have c < b. By Theorem 14, we must have g 0 .c/ D 0 and so f 0 .c/ D k. Thus f 0 takes on the (arbitrary) intermediate value k.  2 f .x/ D x C 2x sin.1=x/ if x ¤ 0 0 if x D 0.

2 f 0 .x/ > 0 if jxj > p 3 2 0 f .x/ < 0 if jxj < p 3

2 2 p / and . p ; 1/: 3 3 2 2 f is decreasing on . p ; p /: 3 3 f is increasing on . 1;

14.

If f .x/ D x 3 C 4x C 1, then f 0 .x/ D 3x 2 C 4. Since f 0 .x/ > 0 for all real x, hence f .x/ is increasing on the whole real line, i.e., on . 1; 1/.

15.

f .x/ D .x 2 4/2 f 0 .x/ D 2x2.x 2 4/ D 4x.x 2/.x C 2/ f 0 .x/ > 0 if x > 2 or 2 < x < 0 f 0 .x/ < 0 if x < 2 or 0 < x < 2 f is increasing on . 2; 0/ and .2; 1/. f is decreasing on . 1; 2/ and .0; 2/. 2x 1 then f 0 .x/ D . Evidently, x2 C 1 .x 2 C 1/2 f 0 .x/ > 0 if x < 0 and f 0 .x/ < 0 if x > 0. Therefore, f is increasing on . 1; 0/ and decreasing on .0; 1/.

16. If f .x/ D

17.

f .x/ D x 3 .5 0

2

f .x/ D 3x .5 2

D x .5

x/2

30. 2

3

x/ C 2x .5

x/.15

x/. 1/

f .0 C h/ f .0/ h h!0 h C 2h2 sin.1= h/ D lim h h!0 D lim .1 C 2h sin.1= h/ D 1;

a) f 0 .0/ D lim

5x/

D 5x 2 .5 x/.3 x/ f .x/ > 0 if x < 0, 0 < x < 3, or x > 5 f 0 .x/ < 0 if 3 < x < 5 f is increasing on . 1; 3/ and .5; 1/. f is decreasing on .3; 5/. 0

h!0

because j2h sin.1= h/j  2jhj ! 0 as h ! 0. b) For x ¤ 0, we have

18. If f .x/ D x 2 sin x, then f 0 .x/ D 1 2 cos x D 0 at x D ˙=3 C 2nfor n D 0; ˙1; ˙2; : : :. f is decreasing on . =3 C 2n;  C 2n/. f is increasing on .=3 C 2n; =3 C 2.n C 1// for integers n.

f 0 .x/ D 1 C 4x sin.1=x/

There are numbers x arbitrarily close to 0 where f 0 .x/ D 1; namely, the numbers x D ˙1=.2n/, where n D 1, 2, 3, : : : . Since f 0 .x/ is continuous at every x ¤ 0, it is negative in a small interval about every such number. Thus f cannot be increasing on any interval containing x D 0.

19. If f .x/ D x C sin x, then f 0 .x/ D 1 C cos x  0 f 0 .x/ D 0 only at isolated points x D ˙; ˙3; :::. Hence f is increasing everywhere. 20. If f .x/ D x C 2 sin x, then f 0 .x/ D 1 C 2 cos x > 0 if cos x > 1=2. Thus f is increasing on the intervals . .4=3/ C 2n; .4=3/ C 2n/ where n is any integer. 21.

f .x/ D x 3 is increasing on . 1; 0/ and .0; 1/ because f 0 .x/ D 3x 2 > 0 there. But f .x1 / < f .0/ D 0 < f .x2 / whenever x1 < 0 < x2 , so f is also increasing on intervals containing the origin.

2 cos.1=x/:

31.

Let a, b, and c be three points in I where f vanishes; that is, f .a/ D f .b/ D f .c/ D 0. Suppose a < b < c. By the Mean-Value Theorem, there exist points r in .a; b/ and s in .b; c/ such that f 0 .r/ D f 0 .s/ D 0. By the MeanValue Theorem applied to f 0 on Œr; s, there is some point t in .r; s/ (and therefore in I ) such that f 00 .t / D 0.

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ADAMS and ESSEX: CALCULUS 9

32. If f .n/ exists on interval I and f vanishes at n C 1 distinct points of I , then f .n/ vanishes at at least one point of I . Proof: True for n D 2 by Exercise 8. Assume true for n D k. (Induction hypothesis) Suppose n D k C 1, i.e., f vanishes at k C 2 points of I and f .kC1/ exists. By Exercise 7, f 0 vanishes at k C 1 points of I . By the induction hypothesis, f .kC1/ D .f 0 /.k/ vanishes at a point of I so the statement is true for n D k C 1. Therefore the statement is true for all n  2 by induction. (case n D 1 is just MVT.)

3.

x 2 C xy D y 3 Differentiate with respect to x: 2x C y C xy 0 D 3y 2 y 0 2x C y y0 D 2 3y x

4.

x 3 y C xy 5 D 2 3x 2 y C x 3 y 0 C y 5 C 5xy 4 y 0 D 0 3x 2 y y 5 y0 D 3 x C 5xy 4

5.

x 2 y 3 D 2x y 2xy 3 C 3x 2 y 2 y 0 D 2 2 2xy 3 y0 D 3x 2 y 2 C 1

33. Given that f .0/ D f .1/ D 0 and f .2/ D 1: a) By MVT, f 0 .a/ D

1 f .0/ D 0 2

f .2/ 2

0 1 D 0 2

6.

for some a in .0; 2/. b) By MVT, for some r in .0; 1/, f 0 .r/ D

f .1/ 1

7.

f .0/ 0 D 0 1

0 D 0: 0

Also, for some s in .1; 2/, f 0 .s/ D

f .2/ 2

f .1/ 1 D 1 2

0 D 1: 1

8.

Then, by MVT applied to f 0 on the interval Œr; s, for some b in .r; s/, 1 f 0 .s/ f 0 .r/ D s r s 1 1 D > s r 2

f 00 .b/ D

since s

0 r

r < 2.

c) Since f 00 .x/ exists on Œ0; 2, therefore f 0 .x/ is continuous there. Since f 0 .r/ D 0 and f 0 .s/ D 1, and since 0 < 71 < 1, the Intermediate-Value Theorem assures us that f 0 .c/ D 71 for some c between r and s.

Section 2.9 Implicit Differentiation (page 149) 1.

xy x C 2y D 1 Differentiate with respect to x: y C xy 0 1 C 2y 0 D 0 1 y Thus y 0 D 2Cx

2. x 3 C y 3 D 1

3x 2 C 3y 2 y 0 D 0, so y 0 D

64

9.

x2 . y2

x 2 C 4.y 2x C 8.y

y0

1/2 D 4 1/y 0 D 0, so y 0 D

x 4.1

y/

x2 x2 C y x y D C1D xCy y y Thus xy y 2 D x 3 Cx 2 y Cxy Cy 2 , or x 3 Cx 2 y C2y 2 D 0 Differentiate with respect to x: 3x 2 C 2xy C x 2 y 0 C 4yy 0 D 0 3x 2 C 2xy y0 D x 2 C 4y p x x C y D 8 xy 1 p xCyCx p .1 C y 0 / D y xy 0 2 xCy p 2.x C y/ C x.1 C y 0 /p D 2 x C y.y C xy 0 / 3x C 2y C 2y x C y y0 D p x C 2x x C y 2x 2 C 3y 2 D 5 4x C 6yy 0 D 0

At .1; 1/: 4 C 6y 0 D 0, y 0 D 2 Tangent line: y 1 D .x 3

2 3 1/ or 2x C 3y D 5

10. x 2 y 3 x 3 y 2 D 12 2xy 3 C 3x 2 y 2 y 0 3x 2 y 2 2x 3 yy 0 D 0 At . 1; 2/: 16 C 12y 0 12 C 4y 0 D 0, so the slope is 28 7 12 C 16 D D : y0 D 12 C 4 16 4 Thus, the equation of the tangent line is y D 2 C 74 .x C 1/, or 7x 4y C 15 D 0: 11.

x  y 3 C D2 y x x 4 C y 4 D 2x 3 y 4x 3 C 4y 3 y 0 D 6x 2 y C 2x 3 y 0 at . 1; 1/: 4 4y 0 D 6 2y 0 2y 0 D 2, y 0 D 1 Tangent line: y C 1 D 1.x C 1/ or y D x.

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INSTRUCTOR’S SOLUTIONS MANUAL

12. x C 2y C 1 D

SECTION 2.9 (PAGE 149)

y2

19.

1 1/2yy 0 y 2 .1/ 1 C 2y D .x 1/2 At .2; 1/ we have 1 C 2y 0 D 2y 0 1 so y 0 D Thus, the equation of the tangent is y D 1 21 .x 2/, or x C 2y D 0: p 13. 2x C y p 2 sin.xy/ D =2 2 C y0 2 cos.xy/.y C xy 0 / D 0 At .=4; 1/: 2 C y 0 .1 C .=4/y 0 / D 0, so 0 y D 4=.4 /. The tangent has equation 4

yD1 14.

3x 2



1 2.

20.

 : 4

x

 2 1 C .x C /: 2 4. 1/

17.

21.

y 00 D D 22.

0

y 00 D

8.y 0 /2 D 8y

1 4y

1C

Ax 2 C By 2 D C

x2 D 16y 3

4y 2 x 2 D 16y 3

1 : 4y 3

Ax By

2A C 2B.y 0 /2 C 2Byy 00 D 0. Thus,

A

B.y 0 /2 D By D

2 C 8.y 0 /2 C 8yy 00 D 0.

x y

x2 y2

2Ax C 2Byy 0 D 0 ) y 0 D

0

18. x 2 C 4y 2 D 4; 2x C 8yy 0 D 0; x Thus, y 0 D and 4y

0 2

1 C .y / D y y a2 y2 C x2 D y3 y3

y 00 D

y 1 y C xy D 1 C y ) y D 1 x y 0 C y 0 C xy 00 D y 00 2.y 1/ 2y 0 D Therefore, y 00 D 1 x .1 x/2

2

x 2 C y 2 D a2 2x C 2yy 0 D 0 so x C yy 0 D 0 and y 0 D 1 C y 0 y 0 C yy 00 D 0 so

xy D x C y 0

x 3 3xy C y 3 D 1 3x 2 3y 3xy 0 C 3y 2 y 0 D 0 6x 3y 0 3y 0 3xy 00 C 6y.y 0 /2 C 3y 2 y 00 D 0 Thus

2

17 x D x y 2  y i .xy 0 y/ 2xy x 2 y 0 sin D : 2 x p x y2 3 .3y 0 1/ D 6 9y 0 , At .3; 1/: 2 p 9 p so y 0 D .108 3/=.162 3 3/. The tangent has equation p 3 108 p .x 3/: y D1C 162 3 3

16. cos h

6x

y x2 y2 x 2x C 2y 0 2y.y 0 /2 y 00 D y2 x "    2 # 2 y x2 y x2 D 2 xC y y x y2 x y2 x   2 4xy 2xy D 2 D : y x .y 2 x/2 .x y 2 /3

x sin.xy y 2 / D x 2 1 sin.xy y 2 / C x.cos.xy y 2 //.y C xy 0 2yy 0 / D 2x. At .1; 1/: 0 C .1/.1/.1 y 0 / D 2, so y 0 D 1. The tangent has equation y D 1 .x 1/, or y D 2 x.  y 

2yy 0 C 3y 2 y 0 D 1 ) y 0 D

y0 D

tan.xy 2 / D .2=/xy .sec2 .xy 2 //.y 2 C 2xyy 0 / D .2=/.y C xy 0 /. At . ; 1=2/: 2..1=4/ y 0 / D .1=/ 2y 0 , so y 0 D . 2/=.4. 1//. The tangent has equation yD

15.

4



y2 C y3 D x

1 3x 2 3y 2 2y 6x 2.y 0 /2 2yy 00 C 6y.y 0 /2 C 3y 2 y 00 D 0 .1 3x 2 /2 .2 6y/ 0 2 .2 6y/.y / 6x .3y 2 2y/2 y 00 D D 3y 2 2y 3y 2 2y .2 6y/.1 3x 2 /2 6x D 2 3 2 .3y 2y/ 3y 2y

x

.x

0

x3

23.

Maple gives 0 for the value.

24.

Maple gives the slope as

25.

Maple gives the value

26.

Maple gives the value

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A

B



Ax By

2

By A.By 2 C Ax 2 / D B 2y3

AC : B 2y3

206 . 55 26. 855; 000 . 371; 293

65

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SECTION 2.9 (PAGE 149)

27.

ADAMS and ESSEX: CALCULUS 9

Ellipse: x 2 C 2y 2 D 2 2x C 4yy 0 D 0

30.

x Slope of ellipse: D 2y Hyperbola: 2x 2 2y 2 D 1 4x 4yy 0 D 0 x 0 Slope of hyperbola: yH D  2 y 2 x C 2y D 2 At intersection points 2x 2 2y 2 D 1 1 3x 2 D 3 so x 2 D 1, y 2 D 2 x2 x x 0 0 D 1 D yH D Thus yE 2y y 2y 2 Therefore the curves intersect at right angles. 0 yE

2x C 4yy 0 C y C xy 0 D 0

Similarly, the slope of the hyperbola .x; y/ satisfies 2x A2

2y 0 y D 0; B2

y2 D 1 at B2

x2 A2

or y 0 D

B 2x : A2 y

2

2

2 2

Section 2.10 Antiderivatives and Initial-Value Problems (page 155) 1.

b CB A a x D  2 . y2 B 2 b2 a A2 Since a2 b 2 D A2 C B 2 , therefore B 2 C b 2 D a2 A2 , x2 A2 a2 and 2 D 2 2 . Thus, the product of the slope of the y B b two curves at .x; y/ is

3. 4. 5.

Thus,

b2 x B 2 x  D a2 y A2 y

b 2 B 2 A2 a2  D a2 A2 B 2 b 2

1:

Therefore, the curves intersect at right angles.

6. 7.

8. 9.

29. If z D tan.x=2/, then 1 C tan2 .x=2/ dx 1 C z 2 dx 1 dx D D : 1 D sec2 .x=2/ 2 dz 2 dz 2 dz Thus dx=dz D 2=.1 C z 2 /. Also cos x D 2 cos2 .x=2/ D

2 1 C z2

1D

1D

2

1 z2 1 C z2

sin x D 2 sin.x=2/ cos.x=2/ D

66

10. 11.

sec2 .x=2/

2x C y : 4y C x

the only solution is x D 0, y D 0, and these values do not satisfy the original equation. There are no points on the given curve.

2.

If the point .x; y/ is an intersection of the two curves, then y2 x2 y2 x2 C D 2 2 b A2 B 2   a 1 1 1 1 2 2 D y : C x A2 a2 B2 b2 2

y0 D

1 7 y 7 x C xy C y 2 C y 2 D 0; or .x C /2 C y 2 D 0; 4 4 2 4

b2 x : a2 y

i.e. y 0 D

)

However, since x 2 C 2y 2 C xy D 0 can be written

x2 y2 28. The slope of the ellipse 2 C 2 D 1 is found from a b 2x 2y C 2 y 0 D 0; a2 b

x x y D C 1 , xy y 2 D x 2 C xy C xy C y 2 xCy y , x 2 C 2y 2 C xy D 0 Differentiate with respect to x:

1

12.

2 tan.x=2/ 2z : D 2 1 C tan .x=2/ 1 C z2

13.

Z

Z

Z

Z

Z

5 dx D 5x C C x 2 dx D 31 x 3 C C p

x dx D

x 12 dx D x 3 dx D

2 3=2 x CC 3 1 13 13 x

CC

1 4 x CC 4

Z

.x C cos x/ dx D

Z

1 C cos3 x dx D cos2 x

x2 C sin x C C 2 Z Z tan x cos x dx D sin x dx D cos x C C

Z

Z

Z

.a2

Z

.sec2 xCcos x/ dx D tan xCsin xCC

x 2 / dx D a2 x

1 3 x CC 3

.A C Bx C C x 2 / dx D Ax C .2x 1=2 C 3x 1=3 dx D

B 2 C 3 x C x CK 2 3

4 3=2 9 4=3 x C x CC 3 4

Z

Z 6.x 1/ dx D .6x 1=3 6x 4=3 / dx x 4=3 D 9x 2=3 C 18x 1=3 C C  Z  3 x2 1 4 1 3 1 2 x C x 1 dx D x x C x 3 2 12 6 2

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x CC

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INSTRUCTOR’S SOLUTIONS MANUAL

14.

105

Z

SECTION 2.10

.1 C t 2 C t 4 C t 6 / dt

29.



30.

Given that

D 105.t C 13 t 3 C 15 t 5 C 17 t 7 / C C

D 105t C 35t 3 C 21t 5 C 15t 7 C C Z 1 15. cos.2x/ dx D sin.2x/ C C 2 Z x  x  16. sin dx D 2 cos CC 2 2 Z 1 dx D CC 17. .1 C x/2 1Cx Z 18. sec.1 x/ tan.1 x/ dx D sec.1 19.

Z

p

20. Since

21.

Z

p

23. 24. 25. 26.

27.

Z

Z

Z

Z

(

tan2 x dx D

p Z

2x x2 C 1

sin x cos x dx D cos2 x dx D sin2 x dx D 0

y Dx

2

Thus y D

1 2 x 2

y.0/ D 3

Z

then y D

Z

33.

2

interval . 1; 0/.

x

3

/ dx D

x

34.

1 . 2

x

yD

Z

For



C 12 x

2

2

CC

9=7

dx D

9=7

4;

2=7 7 2x 7 2

C C.

cos x dx D sin x C C C D

3 2

y 0 D sin.2x/ , we have y.=2/ D 1 Z

1 cos.2x/ C C 2 1 1 1 1D cos  C C D C C ÷ C D 2 2 2  1 yD 1 cos.2x/ (for all x): 2

yD

35.

1/ C C so C D 32 . . 1/ C 1 1 3 C which is valid on the x 2x 2 2 1

Z

y0 D x y.1/ D

 1 CC D CC ÷ 6 2 3 (for all x): y D sin x C 2

3

1



2 D sin

2x C 3 for all x. y0 D x 2 x y. 1/ D 0;

C 5 which is valid on the whole real

Also, 4 D y.1/ D C C , so C D 12 . Hence, 7 1 2=7 y D 2x 2 , which is valid in the interval .0; 1/.  0 y D cos x , we have For y.=6/ D 2

1 cos.2x/ C C 4

cos.2x/ x sin.2x/ dx D CC 2 2 4 1 ) y D x 2 2x C C 2 ) 3 D 0 C C therefore C D 3

and 0 D y. 1/ D Hence, y.x/ D

1 sin.2x/ dx D 2

C C and 5 D y.0/ D C .

Given that

xCC

1

 .x

1/ dx D tan x

x sin.2x/ 1 C cos.2x/ dx D C CC 2 2 4

28. Given that Z

Z

3 4=3 4x

32.

then y D

p dx D 2 x 2 C 1 C C:

.sec2 x

3 4=3 4x

y 0 D x 1=3 y.0/ D 5;

Since y 0 D Ax 2 C Bx C C we have B A y D x 3 C x 2 C C x C D. Since y.1/ D 1, therefore 3 2 A B A B C, 1 D y.1/ D C C C C D. Thus D D 1 3 2 3 2 and B A y D .x 3 1/ C .x 2 1/ C C.x 1/ C 1 for all x 3 2

cos.x 2 / C C

d p 2 x 22. Since x C1D p , therefore 2 dx x C1 Z

x 1=3 dx D

15

31. x/ C C

p 4 dx D 8 x C 1 C C: xC1

2x sin.x 2 / dx D



Hence, y.x/ D line.

d p 1 xC1D p , therefore dx 2 xC1 Z

Z

then y D

1 .2x C 3/3=2 C C 3

2x C 3 dx D

p y 0 D 3 x ) y D 2x 3=2 C C y.4/ D 1 ) 1 D 16 C C so C D Thus y D 2x 3=2 15 for x > 0.

(PAGE 155)

sin.2x/ dx D



y 0 D sec2 x ; we have y.0/ D 1 Z y D sec2 x dx D tan x C C

For

1 D tan 0 C C D C ÷ C D 1 y D tan x C 1 (for =2 < x < =2/.

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SECTION 2.10 (PAGE 155)

36. For



ADAMS and ESSEX: CALCULUS 9

8 00 < y D cos x 41. For y.0/ D 0 we have : 0 y .0/ D 1

y 0 D sec2 x , we have y./ D 1 yD

Z

sec2 x dx D tan x C C

y0 D

1 D tan  C C D C ÷ C D 1 y D tan x C 1 (for =2 < x < 3=2/:

then y 0 D

Z

4

x 0

dx D

Since 2 D y .1/ D and y 0 D 13 x 3 C yD

Z 

1 3 7 3.

1 x 3 3

1 x 3 3

7 3

C 7 3



C C.

dx D 61 x

2

C 73 x C D;

C D, so that D D 23 . Hence, which is valid in the interval

3 , 2

43.

1 4 x x C C1 . 4 0 Since y .0/ D 0, therefore 0 D 0 0 C C1 , and 1 y 0 D x 4 x. 4 1 5 1 2 x x C C2 . Thus y D 20 2 Since y.0/ D 8, we have 8 D 0 0 C C2 . 1 5 1 2 Hence y D x x C 8 for all x. 20 2 40. Given that 8 < y 00 D 5x 2 3x 1=2 y 0 .1/ D 2 : y.1/ D 0; Z we have y 0 D 5x 2 3x 1=2 dx D 53 x 3 6x 1=2 C C . 1, therefore y 0 D

5 3 6x 1=2 C 19 3 ,

Also, 2 D y 0 .1/ D y 0 D 35 x 3 yD

Z 

5 3 x 3

6x

1=2

C

6 C C so that C D

19 . Thus, 3

and

19 3



dx D

4x

C

19 x C D: 3

5 4 C 19 Finally, 0 D y.1/ D 12 3 C D so that D D 5 4 11 3=2 Hence, y.x/ D 12 x 4x C 19 3 x 4 .

68

y0 D

Z

yD

x3 6

.x C sin x/ dx D

sin x C x C 2:

B . Then y 0 D A x Thus, for all x ¤ 0, Let y D Ax C

x 2 y 00 C xy 0

yD

11 4 .

2B C Ax x

B 2B , and y 00 D 3 . x2 x B x

B D 0: x

Ax

We will also have y.1/ D 2 and y 0 .1/ D 4 provided A C B D 2;

and A

B D 4:

These equations have solution A D 3, B D 1, so the initial value problem has solution y D 3x .1=x/. 44.

Let r1 and r2 be distinct rational roots of the equation ar.r 1/ C br C c D 0 Let y D Ax r1 C Bx r2 .x > 0/ Then y 0 D Ar1 x r1 1 C Br2 x r2 1 , and y 00 D Ar1 .r1 1/x r1 2 C Br2 .r2 1/x r2 2 . Thus ax 2 y 00 C bxy 0 C cy 1/x r1

r1 1

3=2

C2 D 1

8 00 < y D x C sin x we have For y.0/ D 2 : 0 y .0/ D 0

D ax 2 .Ar1 .r1

5 4 x 12

÷

x2 cos x C C1 2 0 D 0 cos 0 C C1 ÷ C1 D 1  Z  2 x x3 yD cos x C 1 dx D sin x C x C C2 2 6 2 D 0 sin 0 C 0 C C2 ÷ C2 D 2

C C , therefore C D 37 , Thus

and 1 D y.1/ D 16 C y.x/ D 16 x 2 C 37 x .0; 1/.

39. Since y 00 D x 3

0 D cos 0 C 0 C C2 y D 1 C x cos x:

42.

8 < y 00 D x 4 y 0 .1/ D 2 : y.1/ D 1;

cos x dx D sin x C C1

1 D sin 0 C C1 ÷ C1 D 1 Z y D .sin x C 1/ dx D cos x C x C C2

37. Since y 00 D 2, therefore y 0 D 2x C C1 . Since y 0 .0/ D 5, therefore 5 D 0 C C1 , and y 0 D 2x C 5. Thus y D x 2 C 5x C C2 . Since y.0/ D 3, therefore 3 D 0C0CC2 , and C2 D 3. Finally, y D x 2 C 5x 3, for all x. 38. Given that

Z

2

C Br2 .r2 r2 1

1/x r2

C bx.Ar1 x C Br2 x / C c.Ax   r1 D A ar1 .r1 1/ C br1 C c x  C B.ar2 .r2 1/ C br2 C c x r2

D 0x r1 C 0x r2  0 .x > 0/

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r1

2

C Bx r2 /

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INSTRUCTOR’S SOLUTIONS MANUAL

8 < 4x 2 y 00 C 4xy 0 45. y.4/ D 2 : 0 y .4/ D 2

yD0

Auxilary Equation: 4r.r 4r 2

./

SECTION 2.11

) a D 4; b D 4; c D

1/ C 4r

1

d) never accelerating to the left e) particle is speeding up for t > 2

1D0

1D0 1 r D˙ 2 By #31, y D Ax 1=2 C Bx 1=2 solves ./ for x > 0. A B 3=2 Now y 0 D x 1=2 x 2 2 Substitute the initial conditions: 2 D 2A C 2D

A 4

B 2 B 16

)1 D A C )

f) slowing down for t < 2 g) the acceleration is 2 at all times h) average velocity over 0  t  4 is

B : 4

2.

2.

d) The point is accelerating to the left if a < 0, i.e., for all t . e) The particle is speeding up if v and a have the same sign, i.e., for t > 52 . f) The particle is slowing down if v and a have opposite sign, i.e., for t < 52 .

Since this equation must hold for all x > 0, we must have

g) Since a D

6D0

r2 r 6 D 0 .r 3/.r C 2/ D 0: There are two roots: r1 D 2, and r2 D 3. Thus the differential equation has solutions of the form y D Ax 2 C Bx 3 . Then y 0 D 2Ax 3 C 3Bx 2 . Since 1 D y.1/ D A C B and 1 D y 0 .1/ D 2A C 3B, therefore A D 52 and B D 35 . Hence, y D 25 x 2 C 53 x 3 .

Section 2.11 Velocity and Acceleration (page 162) 1.

2t , a D

D0

c) The point is accelerating to the right if a > 0, but a D 2 at all t ; hence, the point never accelerates to the right.

1/x r 2  6x r D 0 Œr.r 1/ 6x r D 0:

1/

t 2, v D 5

3

b) The point is moving to the left if v < 0, i.e., when t > 25 .

Let y D x r ; y 0 D rx r 1 ; y 00 D r.r 1/x r 2 . Substituting these expressions into the differential equation we obtain

r.r

x D 4 C 5t

16 C 3 4

a) The point is moving to the right if v > 0, i.e., when t < 25 .

B 7 , so B D 18, A D . 2 2 7 1=2 x C 18x 1=2 (for x > 0). Thus y D 2 46. Consider 8 < x 2 y 00 6y D 0 y.1/ D 1 : 0 y .1/ D 1: Hence 9 D

x 2 Œr.r

16 x.0/ D 0

x.4/ 4

B 4

8DA

(PAGE 162)

dx dv xDt 4t C 3, v D D 2t 4, a D D2 dt dt a) particle is moving: to the right for t > 2 2

b) to the left for t < 2 c) particle is always accelerating to the right

3.

2 at all t , a D

2 at t D

5 2

when v D 0.

h) The average velocity over Œ0; 4 is 8 4 x.4/ x.0/ D D 1. 4 4 dx dv x D t 3 4t C 1, v D D 3t 2 4, a D D 6t dt dt p a) particlepmoving: to the right for t < 2= 3 or t > 2= 3, b) to the left for

p p 2= 3 < t < 2= 3

c) particle is accelerating: to the right for t > 0 d) to the left for t < 0

p e) particle p is speeding up for t > 2= 3 or for 2= 3 < t < 0 p f) particle is slowing down for t < 2= 3 or for p 0 < t < 2= 3 p g) velocity is zeropat t D ˙2= 3. Acceleration at these times is ˙12= 3. h) average velocity on Œ0; 4 is

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43

44C1 4 0

1

D 12

69

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SECTION 2.11 (PAGE 162)

4.

ADAMS and ESSEX: CALCULUS 9

.t 2 C 1/.1/ .t /.2t / 1 t2 t ; vD D 2 ; 2 2 C1 .t C 1/ .t C 1/2 2t .t 2 3/ .t 2 C 1/2 . 2t / .1 t 2 /.2/.t 2 C 1/.2t / aD D 2 : 2 4 .t C 1/ .t C 1/3

xD

7.

D D t 2 , D in metres, t in seconds dD D 2t velocity v D dt Aircraft becomes airborne if 500 200; 000 D m/s: v D 200 km/h D 3600 9 250 Time for aircraft to become airborne is t D s, that is, 9 about 27:8 s. Distance travelled during takeoff run is t 2  771:6 metres.

8.

Let y.t / be the height of the projectile t seconds after it is fired upward from ground level with initial speed v0 . Then

t2

a) The point is moving to the right if v > 0, i.e., when 1 t 2 > 0, or 1 < t < 1. b) The point is moving to the left if v < 0, i.e., when t < 1 or t > 1. c) The point is accelerating to the right if a > 0, i.e., whenp2t .t 2 p3/ > 0, that is, when t > 3 or 3 < t < 0.

y 00 .t / D

d) The point p to the left if a < 0, i.e., for p is accelerating t< 3 or 0 < t < 3.

Two antidifferentiations give

2. 2/ D At t D 1, a D .2/3

yD

2. 2/ 1 D . .2/3 2

1 . 2

9.

tD1

Ball strikes the ground when y D 0, .t > 0/, i.e., 0 D t .9:8 4:9t / so t D 2. Velocity at t D 2 is 9:8 9:8.2/ D 9:8 m/s. Ball strikes the ground travelling at 9.8 m/s (downward).

hD

6. Given that y D 100 2t 4:9t , the time t at which the ball reaches the ground is the positive root of the equation y D 0, i.e., 100 2t 4:9t 2 D 0, namely, tD

2C

p

4 C 4.4:9/.100/  4:318 s: 9:8

100 The average velocity of the ball is D 23:16 m=s. 4:318 Since 23:159 D v D 2 9:8t , then t ' 2:159 s.

70

v2 v0 g v02  2 C v0  D 0: 2 g g 2g

An initial speed of 2v0 means the maximum height will be 4v02 =2g D 4h. To get a maximum height of 2h an p initial speed of 2v0 is required. 10. To get to 3h metres above Mars, the ball would have to be thrown upward with speed q p p vM D 6gM h D 6gM v02 =.2g/ D v0 3gM =g: Since gM D 3:72 and g D 9:80, we have vM  1:067v0 m/s.

11. 2

1:86t /:

The height of the ball after t seconds is y.t / D .g=2/t 2 C v0 t m if its initial speed was v0 m/s. Maximum height h occurs when dy=dt D 0, that is, at t D v0 =g. Hence

2

4:9t metres (t in seconds) dy D 9:8 9:8t velocity v D dt dv acceleration a D D 9:8 dt The acceleration is 9:8 m/s2 downward at all times. Ball is at maximum height ˇwhen v D 0, i.e., at t D 1. ˇ Thus maximum height is y ˇ D 9:8 4:9 D 4:9 metres.

1:86t 2 C v0 t D t .49

The time taken to fall back to ground level on Mars would be t D 49=1:86  26:3 s.

h) The average velocity over Œ0; 4 is 4 0 x.4/ x.0/ 1 D 17 D . 4 4 17 5. y D 9:8t

4:9t /:

Since the projectile returns to the ground at t D 10 s, we have y.10/ D 0, so v0 D 49 m/s. On Mars, the acceleration of gravity is 3.72 m/s2 rather than 9.8 m/s2 , so the height of the projectile would be

f) The particle is slowing down if v and a have opposite p 3 < t < 1, or 0 < t < 1 or sign,pi.e., for t > 3. 1, a D

4:9t 2 C v0 t D t .v0

yD

e) The particle is speeding p up if v and a have the same sign, i.e.,pfor t < 3, or 1 < t < 0 or 1 < t < 3.

g) v D 0 at t D ˙1. At t D

9:8; y 0 .0/ D v0 ; y.0/ D 0:

If the cliff is h ft high, then the height of the rock t seconds after it falls is y D h p 16t 2 ft. The rock hits the ground (y D 0) at time p t D h=16 s. Its speedpat that time is v D 32t D 8 h D 160 ft/s. Thus h D 20, and the cliff is h D 400 ft high.

12. If the cliff is h ft high, then the height of the rock t seconds after it is thrown down is y D h 32t 16t 2 ft. The rock hits the ground (y D 0) at time p 1p 32 C 322 C 64h D 1C tD 16 C h s: 32 4

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 2.11

v

Its speed at that time is vD

32

32t D

p 8 16 C h D

(PAGE 162)

.4; 96/

160 ft/s:

Solving this equation for h gives the height of the cliff as 384 ft.

t

13. Let x.t / be the distance travelled by the train in the t seconds after the brakes are applied. Since d 2 x=dt 2 D 1=6 m/s2 and since the initial speed is v0 D 60 km/h D 100=6 m/s, we have 1 2 100 x.t / D t C t: 12 6 The speed of the train at time t is v.t / D .t =6/ C .100=6/ m/s, so it takes the train 100 s to come to a stop. In that time it travels x.100/ D 1002 =12 C 1002 =6 D 1002 =12  833 metres. 14.

15.

x D At 2 C Bt C C; v D 2At C B. The average velocity over Œt1 ; t2  is x.t2 / x.t1 / t2 t1 At22 C Bt1 C C At12 Bt1 C D t2 t1 A.t22 t12 / C B.t2 t1 / D .t2 t1 / A.t2 C t1 /.t2 t1 / C B.t2 t1 / D .t2 t1 / D A.t2 C t1 / C B. The velocity atthe midpoint of Œt1 ; t2  is    instantaneous t2 C t1 t 2 C t1 D 2A C B D A.t2 C t1 / C B. v 2 2 Hence, the average velocity over the interval is equal to the instantaneous velocity at the midpoint. 8 < t2 0t 2 s D 4t 4 2 jhj ! 1 ˇ ˇ ˇ h jhj jhj

f .0 C h/

76

h/

D lim

h!0

27a3 27 C 2 8 4a

27 27a3 C 2 8 4a f .0/ D 1:

Thus f .0/ D 1.

jhj

h

jhj

D lim

h!0

0 D 0: h

 3a : 2

 x

 a

3a 2



D 0:

If a ¤ 0, the x-axis is another tangent to y D x 3 that passes through .a; 0/. The number of tangents to y D x 3 that pass through .x0 ; y0 / is

f .x/ f .x/

h!0

h/

This line passes through .a; 0/ because

6. Given that f .0/ D k, f .0/ ¤ 0, and f .x C y/ D f .x/f .y/, we have

f .x C h/ f .x/ D lim h h!0 f .x/f .h/ D lim h h!0

f .x h

The tangent to y D x 3 at x D 3a=2 has equation

0

0

f .0 2h

yD

as h ! 0. Therefore f 0 .0/ does not exist.

f .0/ D 0 or

f .x/

c) If f .x/ D jxj, then f 0 .0/ does not exist, but

:

5. If h ¤ 0, then

÷

lim

and

:

are always equal if either exists.

f is differentiable elsewhere, including at x D 1 where its derivative is 2.

f .0/ D f .0C0/ D f .0/f .0/

f .x/

h/

D f .x/f 0 .0/ D kf .x/:

three, if x0 ¤ 0 and y0 is between 0 and x03 ;

two, if x0 ¤ 0 and either y0 D 0 or y0 D x03 ;

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INSTRUCTOR’S SOLUTIONS MANUAL

CHALLENGING PROBLEMS 2 (PAGE 164)

The curve y D Ax 2 C Bx C C has slope m D 2Aa C B at .a; Aa2 C Ba C C /. Thus a D .m B/=.2A/, and the tangent has equation

one, otherwise. This is the number of distinct real solutions b of the cubic equation 2b 3 3b 2 x0 C y0 D 0, which states that the tangent to y D x 3 at .b; b 3 / passes through .x0 ; y0 /.

y D Aa2 C Ba C C C m.x

10. By symmetry, any line tangent to both curves must pass through the origin. y y D x 2 C 4x C 1

where f .m/ D C 14. x

a/

B/2 B.m B/ D mx C C CC 4A 2A 2 .m B/ .m B/2 D mx C C C 4A 2A D mx C f .m/; .m

B/2 =.4A/.

.m

Parabola y D x 2 has tangent y D 2ax a2 at .a; a2 /. Parabola y D Ax 2 C Bx C C has tangent Ab 2 C C

y D .2Ab C B/x x 2 C 4x

yD

1

at .b; Ab 2 C Bb C C /. These two tangents coincide if 2Ab C B D 2a

Fig. C-2-10

Ab

2

The tangent to y D x C 4x C 1 at x D a has equation y D a2 C 4a C 1 C .2a C 4/.x D .2a C 4/x

.a2

a/

11.

The slope of y D x 2 at x D a is 2a. The slope of the line from .0; b/ to .a; a2 / is .a2 b/=a. This line is normal to y D x 2 if either a D 0 or 2a..a2 b/=a/ D 1, that is, if a D 0 or 2a2 D 2b 1. There are three real solutions for a if b > 1=2 and only one (a D 0) if b  1=2. 2

2

12. The point Q D .a; a / on y D x that is closest to P D .3; 0/ is such that PQ is normal to y D x 2 at Q. Since PQ has slope a2 =.a 3/ and y D x 2 has slope 2a at Q, we require a2 1 D ; a 3 2a which simplifies to 2a3 C a 3 D 0. Observe that a D 1 is a solution of this cubic equation. Since the slope of y D 2x 3 C x 3 is 6x 2 C 1, which is always positive, the cubic equation can have only one real solution. Thus Q D .1; 1/ is the point on y D x 2 that is closest p to P . The distance from P to the curve is jPQj D 5 units. 13. The curve y D x 2 has slope m D 2a at .a; a2 /. The tangent there has equation y D a2 C m.x

a/ D mx

m2 : 4

2

./

2

C Da :

The two curves have one (or more) common tangents if ./ has real solutions for a and b. Eliminating a between the two equations leads to

1/;

which passes through the origin if a D ˙1. The two common tangents are y D 6x and y D 2x.

m.m B/ 2A

.2Ab C B/2 D 4Ab 2

4C;

or, on simplification, 4A.A

1/b 2 C 4ABb C .B 2 C 4C / D 0:

This quadratic equation in b has discriminant D D 16A2 B 2 16A.A 1/.B 2 C4C / D 16A.B 2 4.A 1/C /: There are five cases to consider: CASE I. If A D 1, B ¤ 0, then ./ gives bD

B 2 C 4C ; 4B

aD

B2

4C : 4B

There is a single common tangent in this case. CASE II. If A D 1, B D 0, then ./ forces C D 0, which is not allowed. There is no common tangent in this case. CASE III. If A ¤ 1 but B 2 D 4.A bD

B 2.A

1/

1/C , then

D a:

There is a single common tangent, and since the points of tangency on the two curves coincide, the two curves are tangent to each other. CASE IV. If A ¤ 1 and B 2 4.A 1/C < 0, there are no real solutions for b, so there can be no common tangents.

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ADAMS and ESSEX: CALCULUS 9

b) The tangent to y D x 4

CASE V. If A ¤ 1 and B 2 4.A 1/C > 0, there are two distinct real solutions for b, and hence two common tangent lines. y y

y D a4

D 4a.a

2x 2 at x D a has equation

2a2 C .4a3

2

4a/.x

a/

3a4 C 2a2 :

1/x

Similarly, the tangent at x D b has equation x

y D 4b.b 2

x

one common two common tangent tangents tangent curves y

1/x

These tangents are the same line (and hence a double tangent) if 4a.a2

y

1/ D 4b.b 2

3a4 C 2a2 D

x

x

Fig. C-2-14 a) The tangent to y D x 3 at .a; a3 / has equation y D 3a2 x

0 D a2 C b 2

2a3 :

x

.x

2

3a x C 2a D 0

a/2 .x C 2a/ D 0:

b) The slope of y D x 3 at x D 2a is 3. 2a/2 D 12a2 , which is four times the slope at x D a.

17.

a) The tangent to y D f .x/ D ax 4 C bx 3 C cx 2 C dx C e

3

c) If the tangent to y D x at x D a were also tangent at x D b, then the slope at b would be four times that at a and the slope at a would be four times that at b. This is clearly impossible. d) No line can be tangent to the graph of a cubic polynomial P .x/ at two distinct points a and b, because if there was such a double tangent y D L.x/, then .x a/2 .x b/2 would be a factor of the cubic polynomial P .x/ L.x/, and cubic polynomials do not have factors that are 4th degree polynomials. 16.

a) y D x 4 2x 2 has horizontal tangents at points x satisfying 4x 3 4x D 0, that is, at x D 0 and x D ˙1. The horizontal tangents are y D 0 and y D 1. Note that y D 1 is a double tangent; it is tangent at the two points .˙1; 1/.

78

b/2 > 0:

c) If y D Ax C B is a double tangent to y D x 4 2x 2 C x, then y D .A 1/x C B is a double tangent to y D x 4 2x 2 . By (b) we must have A 1 D 0 and B D 1. Thus the only double tangent to y D x 4 2x 2 C x is y D x 1.

3

The tangent also intersects y D x 3 at .b; b 3 /, where b D 2a.

2ab D .a

Thus y D 1 is the only double tangent to y D x 4 2x 2 .

For intersections of this line with y D x 3 we solve 3

1/

3b 4 C 2b 2 :

The second equation says that either a2 D b 2 or 3.a2 C b 2 / D 2; the first equation says that a3 b 3 D a b, or, equivalently, a2 C ab C b 2 D 1. If a2 D b 2 , then a D b (a D b is not allowed). Thus a2 D b 2 D 1 and the two points are .˙1; 1/ as discovered in part (a). If a2 Cb 2 D 2=3, then ab D 1=3. This is not possible since it implies that

no common tangent

15.

3b 4 C 2b 2 :

at x D p has equation y D .4ap 3 C3bp 2 C2cpCd /x 3ap 4 2bp 3 cp 2 Ce: This line meets y D f .x/ at x D p (a double root), and xD

2ap



p

b2

4ac 2a

4abp

8a2 p 2

:

These two latter roots are equal (and hence correspond to a double tangent) if the expression under the square root is 0, that is, if 8a2 p 2 C 4abp C 4ac

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b 2 D 0:

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INSTRUCTOR’S SOLUTIONS MANUAL

CHALLENGING PROBLEMS 2 (PAGE 164)

This quadratic has two real solutions for p provided its discriminant is positive, that is, provided 16a2 b 2

4.8a2 /.4ac

b 2 / > 0:

This condition simplifies to 3b 2 > 8ac: For example, for y D x 4 2x 2 C x 1, we have a D 1, b D 0, and c D 2, so 3b 2 D 0 > 16 D 8ac, and the curve has a double tangent. b) From the discussion above, the second point of tangency is

so the formula above is true for n D 1. Assume it is true for n D k, where k is a positive integer. Then    d kC1 d k k cos.ax/ D a cos ax C dx 2 dx kC1    k k Da a sin ax C 2   .k C 1/ kC1 Da cos ax C : 2 Thus the formula holds for n D 1; 2; 3; : : : by induction. b) Claim:

qD

2ap b D 2a

p

b : 2a

The slope of PQ is f .q/ q

b3 f .p/ D p

4abc C 8a2 d : 8a2

Calculating f 0 ..p C q/=2/ leads to the same expression, so the double tangent PQ is parallel to the tangent at the point horizontally midway between P and Q. c) The inflection points are the real zeros of f 00 .x/ D 2.6ax 2 C 3bx C c/: This equation has distinct real roots provided 9b 2 > 24ac, that is, 3b 2 > 8ac. The roots are rD sD

p 9b 2 p12a 3b C 9b 2 12a

3b

b3 f .r/ D r

so the formula above is true for n D 1. Assume it is true for n D k, where k is a positive integer. Then    d kC1 k d k a sin ax C sin.ax/ D dx 2 dx kC1    k k D a a cos ax C 2   .k C 1/ kC1 Da sin ax C : 2

c) Note that

4abc C 8a2 d ; 8a2

so this line is also parallel to the double tangent.

18.

  d sin.ax/ D a cos.ax/ D a sin ax C ; dx 2

:

The slope of the line joining these inflection points is f .s/ s

Proof: For n D 1 we have

Thus the formula holds for n D 1; 2; 3; : : : by induction.

24ac 24ac

 n  dn sin.ax/ D an sin ax C . n dx 2

 dn n  n cos.ax/ D a cos ax C . dx n 2 Proof: For n D 1 we have

d .cos4 x C sin4 x/ D 4 cos3 x sin x C 4 sin3 x cos x dx D 4 sin x cos x.cos2 sin2 x/ D 2 sin.2x/ cos.2x/   D sin.4x/ D cos 4x C : 2 It now follows from part (a) that

a) Claim:

d cos.ax/ D dx

  a sin.ax/ D a cos ax C ; 2

dn .cos4 x C sin4 x/ D 4n dx n

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1

 n  cos 4x C : 2

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CHALLENGING PROBLEMS 2 (PAGE 164)

19.

ADAMS and ESSEX: CALCULUS 9

v (m/s)

d) The upward acceleration in Œ0; 3 was 39:2=3  13:07 m/s2 .

.3; 39:2/

40

e) The maximum height achieved by the rocket is the distance it fell from t D 7 to t D 15. This is the area under the t -axis and above the graph of v on that interval, that is,

30 20 10 t (s) -10

2

4

6

8

10

12

14

12

.15; 1/

7 2

.49/ C

49 C 1 .15 2

12/ D 197:5 m:

-20 -30

f) During the time interval Œ0; 7, the rocket rose a distance equal to the area under the velocity graph and above the t -axis, that is,

-40 .12; 49/ Fig. C-2-19

1 .7 2

a) The fuel lasted for 3 seconds. b) Maximum height was reached at t D 7 s. c) The parachute was deployed at t D 12 s.

80

0/.39:2/ D 137:2 m:

Therefore the height of the tower was 197:5 137:2 D 60:3 m.

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INSTRUCTOR’S SOLUTIONS MANUAL

CHAPTER 3. FUNCTIONS

TRANSCENDENTAL

Section 3.1 Inverse Functions 1.

SECTION 3.1 (PAGE 171)

f .x1 / D f .x2 / , x12 D x22 ; .x1  0; x2  0/ , x1 D x2 Thus f is one-to-one. Let y D f 1 .x/. Then x D f .y/ p D y 2 .y  0/. p x and f 1 .x/ D x. therefore y D D.f / D . 1; 0 D R.f 1 /, D.f 1 / D Œ0; 1/ D R.f /.

(page 171)

f .x/ D x 1 f .x1 / D f .x2 / ) x1 1 D x2 1 ) x1 D x2 . Thus f is one-to-one. Let y D f 1 .x/. Then x D f .y/ D y 1 and y D x C 1. Thus f 1 .x/ D x C 1. D.f / D D.f 1 / D R D R.f / D R.f 1 /.

2. f .x/ D 2x 1. If f .x1 / D f .x2 /, then 2x1 1 D 2x2 1. Thus 2.x1 x2 / D 0 and x1 D x2 . Hence, f is one-toone. Let y D f 1 .x/. Thus x D f .y/ D 2y 1, so y D 21 .x C 1/. Thus f 1 .x/ D 12 .x C 1/. D.f / D R.f 1 / D . 1; 1/. R.f / D D.f 1 / D . 1; 1/.

8.

f .x/ D .1 2x/3 . If f .x1 / D f .x2 /, then .1 2x1 /3 D .1 2x2 /3 and x1 D x2 . Thus, f is one-toone. 1 3 Let y D f p .x/. Then x D f .y/ D .1 2y/ p so y D 21 .1 3 x/. Thus, f 1 .x/ D 12 .1 3 x/. D.f / D R.f 1 / D . 1; 1/. R.f / D D.f 1 / D . 1; 1/.

9.

f .x/ D

p 3. f .x/ D x 1 p p f .x1 / D f .x2 / , x1 1 D x2 1; .x1 ; x2  1/ , x1 1 D x2 1 D 0 , x1 D x2 Thus f is one-to-one.pLet y D f 1 .x/. Then x D f .y/ D y 1, and y D 1 C x 2 . Thus f 1 .x/ D 1 C x 2 , .x  0/. D.f / D R.f 1 / D Œ1; 1/, R.f / D D.f 1 / D Œ0; 1/. p x 1 for x  1. 4. f .x/ D p p If f .x1 / D f .x2 /, then x1 1 D x2 1 and x1 1 D x2 1. Thus x1 D x2 and f is one-to-one. p y 1 so Let y D f 1 .x/. Then x D f .y/ D 2 2 1 x D y 1 and y D x C 1. Thus, f .x/ D x 2 C 1. D.f / D R.f 1 / D Œ1; 1/. R.f / D D.f 1 / D . 1; 0. 5. f .x/ D x 3 f .x1 / D f .x2 / , x13 D x23

) .x1 x2 /.x12 C x1 x2 C x22 / D 0 ) x1 D x2 Thus f is one-to-one. Let y D f 1 .x/. Then x D f .y/ D y 3 so y D x 1=3 . Thus f 1 .x/ D x 1=3 . D.f / D D.f 1 / D R D R.f / D R.f 1 /.

p 6. f .x/ pD 1 C 3 x. p If f .x1 / D f .x2 /, then 1 C 3 x 1 D 1 C 3 x 2 so x1 D x2 . Thus, f is oneto-one. p Let y D f 1 .x/ so that x D f .y/ D 1 C 3 y. Thus 3 1 3 y D .x 1/ and f .x/ D .x 1/ . D.f / D R.f 1 / D . 1; 1/. R.f / D D.f 1 / D . 1; 1/.

f .x/ D x 2 ; .x  0/

7.

1 : D.f / D fx W x ¤ 1g D R.f xC1 1 1 D f .x1 / D f .x2 / , x1 C 1 x2 C 1 , x2 C 1 D x1 C 1 , x2 D x1 Thus f is one-to-one; Let y D f 1 .x/. 1 Then x D f .y/ D y C1 1 1 and y D f 1 .x/ D 1. so y C 1 D x x 1 D.f / D fx W x ¤ 0g D R.f /.

1

/.

x . If f .x1 / D f .x2 /, then 10. f .x/ D 1Cx x1 x2 D . Hence x1 .1 C x2 / D x2 .1 C x1 / 1 C x1 1 C x2 and, on simplification, x1 D x2 . Thus, f is one-to-one. y Let y D f 1 .x/. Then x D f .y/ D and 1Cy x D f 1 .x/. x.1 C y/ D y. Thus y D 1 x D.f / D R.f 1 / D . 1; 1/ [ . 1; 1/. R.f / D D.f 1 / D . 1; 1/ [ .1; 1/. 11.

1 2x : D.f / D fx W x ¤ 1g D R.f 1 / 1Cx 1 2x2 1 2x1 D f .x1 / D f .x2 / , 1 C x1 1 C x2 , 1 C x2 2x1 2x1 x2 D 1 C x1 2x2 2x1 x2 , 3x2 D 3x1 , x1 D x2 Thus f is one-to-one. Let y D f 1 .x/. 1 2y Then x D f .y/ D 1Cy so x C xy D 1 2y 1 x . and f 1 .x/ D y D 2Cx 1 D.f / D fx W x ¤ 2g D R.f /. f .x/ D

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SECTION 3.1 (PAGE 171)

ADAMS and ESSEX: CALCULUS 9

x . If f .x1 / D f .x2 /, then x2 C 1 x1 x2 q D q : ./ 2 x1 C 1 x22 C 1

12. f .x/ D p

20.

Thus x12 .x22 C 1/ D x22 .x12 C 1/ and x12 D x22 . From (*), x1 and x2 must have the same sign. Hence, x1 D x2 and f is one-to-one. y , and Let y D f 1 .x/. Then x D f .y/ D p 2 y C1 x2 x 2 .y 2 C 1/ D y 2 . Hence y 2 D . Since f .y/ and y 1 x2 x , so have the same sign, we must have y D p 1 x2 x . f 1 .x/ D p 1 x2 1 D.f / D R.f / D . 1; 1/. R.f / D D.f 1 / D . 1; 1/.

21.

13. g.x/ D f .x/ 2 Let y D g 1 .x/. Then x D g.y/ D f .y/ 2, so f .y/ D x C 2 and g 1 .x/ D y D f 1 .x C 2/. 14.

15.

f .x/ D x 2 C 1 if x  0, and f .x/ D x C 1 if x < 0. If f .x1 / D f .x2 / then if x1  0 and x2  0 then x12 C 1 D x22 C 1 so x1 D x2 ; if x1  0 and x2 < 0 then x12 C 1 D x2 C 1 so x2 D x12 (not possible); if x1 < 0 and x2  0 then x1 D x22 (not possible); if x1 < 0 and x2 < 0 then x1 C 1 D x2 C 1 so x1 D x2 . Therefore f is Let y D f 1 .x/. Then  one-to-one. y 2 C 1 if y  0 x D f .y/ D y C 1  if y < 0. p 1 x 1 if x  1 Thus f .x/ D y D x 1 if x < 1. y

h.x/ D f .2x/. Let y D h 1 .x/. Then x D h.y/ D f .2y/ and 2y D f 1 .x/. Thus h 1 .x/ D y D 21 f 1 .x/.

1

y D f .x/

k.x/ D 3f .x/. Let y D k 1 .x/. Then x and x D k.y/ D 3f .y/, so f .y/ D 3  x 1 1 . k .x/ D y D f 3

16. m.x/ D f .x 2/. Let y D m 1 .x/. Then x D m.y/ D f .y 2/, and y 2 D f 1 .x/. Hence m 1 .x/ D y D f 1 .x/ C 2. 17.

1 C f .x/ . Let y D s 1 .x/. 1 f .x/ 1 C f .y/ Then x D s.y/ D . Solving for f .y/ we obtain 1 f .y/   x 1 x 1 . Hence s 1 .x/ D y D f 1 . f .y/ D xC1 xC1 s.x/ D

1 . Let y D p 1 .x/. p.x/ D 1 C f .x/ 1 1 so f .y/ D Then x D p.y/ D 1 C f .y/ x  1 1 . and p 1 .x/ D y D f 1 x

x

Fig. 3.1-21 22.

g.x/ D x 3 if x  0, and g.x/ D x 1=3 if x < 0. Suppose f .x1 / D f .x2 /. If x1  0 and x2  0 then x13 D x23 so x1 D x2 . Similarly, x1 D x2 if both are negative. If x1 and x2 have opposite sign, then so do g.x1 / and g.x2 /. Therefore g is Let y D g 1 .x/. Then  one-to-one. 3 y if y  0 x D g.y/ D y 1=3 if y < 0. 1=3 if x  0 Thus g 1 .x/ D y D x 3 x if x < 0.

23.

If x1 and x2 are both positive or both negative, and h.x1 / D h.x2 /, then x12 D x22 so x1 D x2 . If x1 and x2 have opposite sign, then h.x1 / and h.x2 / are on opposite sides of 1, so cannot be equal. Hence h is one-to-one. y2 C 1 if y  0 . If If y D h 1 .x/, then x D h.y/ D 2 y C 1 if y < 0 p p y  0, then y D px 1. If y < 0, then y D 1 x. Thus h 1 .x/ D px 1 if x  1 1 x if x < 1

24.

y D f 1 .x/ , x D f .y/ D y 3 C y. To find y D f 1 .2/ we solve y 3 C y D 2 for y. Evidently y D 1 is the only solution, so f 1 .2/ D 1.

1,

f .x/ 3 Let y D q 1 .x/. Then 2 f .y/ 3 and f .y/ D 2x C 3. Hence x D q.y/ D 2 1 1 q .x/ D y D f .2x C 3/.

18. q.x/ D

19. r.x/ D 1 2f .3 4x/ Let y D r 1 .x/. Then x D r.y/ D 1 f .3 3

4y/ D

f

x 2  1

4y D f

 1 and r 1 .x/ D y D 3 4

82

1

1



2f .3

1

x 2

1

x 2



 .

4y/.

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 3.1 (PAGE 171)

25. g.x/ D 1 if x 3 C x D 10, that is, if x D 2. Thus g 1 .1/ D 2. 26. h.x/ D 3 if xjxj D h 1 . 3/ D 2. 27.

If y D f

4, that is, if x D

31.

2. Thus 32.

1

.x/ then x D f .y/. dy dy 1 1 Thus 1 D f 0 .y/ so D 0 D Dy 1 dx dx f .y/ y (since f 0 .x/ D 1=x).

dy dx D .2 C cos y/ dx dx ˇ dy ˇˇ 1 1 0 .g / .2/ D  0:36036: D ˇ dx ˇ 2 C cos y

1D

xD2

4x 3 , then x2 C 1

4x 2 .x 2 C 3/ .x 2 C 1/.12x 2 / 4x 3 .2x/ D : f .x/ D 2 2 .x C 1/ .x 2 C 1/2

33.

0

Since f 0 .x/ > 0 for all x, except x D 0, f must be oneto-one and so it has an inverse. 4y 3 , and If y D f 1 .x/, then x D f .y/ D 2 y C1 1 D f 0 .y/ D

.y 2 C 1/2 . Since f .1/ D 2, therefore 4y 4 C 12y 2 1 f .2/ D 1 and f

ˇ .y 2 C 1/2 ˇˇ .2/ D 4 ˇ 4y C 12y 2 ˇ

yD1

p 30. If f .x/ D x 3pC x 2 and y D f x D f .y/ D y 3 C y 2 , so, p 2yy 0 1 D y 3 C y2 C y p 2 3 C y2 0

Since f . 1/ D 2 implies that f f

 1 0

If f .x/ D x sec x, then f 0 .x/ D sec x C x sec x tan x  1 for x in . =2; =2/. Thus f is increasing, and so oneto-one on that interval. Moreover, limx! .=2/C f .x/ D 1 and limx!.=2/C f .x/ D 1, so, being continuous, f has range . 1; 1/, and so f 1 has domain . 1; 1/. Since f .0/ D 0, we have f 1 .0/ D 0, and .f

.y 2 C 1/.12y 2 y 0 / 4y 3 .2yy 0 / : .y 2 C 1/2

Thus y 0 D

 1 0

g.x/ D 2x C sin x ) g 0 .x/ D 2 C cos x  1 for all x. Therefore g is increasing, and so one-to-one and invertible on the whole real line. y D g 1 .x/ , x D g.y/ D 2y C sin y. For y D g 1 .2/, we need to solve 2y C sin y 2 D 0. The root is between 0 and 1; to five decimal places g 1 .2/ D y  0:68404. Also

28. f .x/ D 1 C 2x 3 Let y D f 1 .x/. Thus x D f .y/ D 1 C 2y 3 . 1 dy 1 dy D so .f 1 /0 .x/ D D 1 D 6y 2 dx dx 6y 2 6Œf 1 .x/2 29. If f .x/ D

p y D f 1 .2/ , 2 D f .y/ D y 2 =.1 C y/. We must solve p 2 2 C 2 y D y for y. There is a root between 2 and 3: f 1 .2/  2:23362 to 5 decimal places.

1

D

1 : 4

35.

.x/, then

) 1

0

y D

. 2/ D

ˇ p 3 C y 2 ˇˇ . 2/ D ˇ 3 C 2y 2 ˇ

yD 1

D

34.

p

3 C y2 : 3 C 2y 2

1, we have 2 : 5

p Note: f .x/ D x 3 C x 2 D 2 ) x 2 .3 C x 2 / D 4 4 2 ) x C 3x 4 D 0 ) .x 2 C 4/.x 2 1/ D 0. 2 Since .x C 4/ D 0 has no real solution, therefore x 2 1 D 0 and x D 1 or 1. Since it is given that f .x/ D 2, therefore x must be 1.

1 0

/ .0/ D

1 f 0 .f

1 .0/

D

1 D 1: f 0 .0/

If y D .f ı g/ 1 .x/, then x D f ı g.y/ D f .g.y//. Thus g.y/ D f 1 .x/ and y D g 1 .f 1 .x// D g 1 ı f 1 .x/. That is, .f ı g/ 1 D g 1 ı f 1 . x a bx c y a and Let y D f 1 .x/. Then x D f .y/ D by c cx a bxy cx D y a so y D . We have bx 1 cx a x a D , which simplifies to f 1 .x/ D f .x/ if bx c bx 1 f .x/ D

b.1

c/x 2 C .c 2

1/x C a..1

c/  0:

This equation is satisfied for (almost) all values of x provided that c D 1 a and b arbitrary, or c D 1 and a D b D 0. In the latter case f .x/  x, which is certainly self-inverse. For the former case, f will be self-inverse provided f is one-to-one and so has an inverse. Since, for c D 1, ab 1 f 0 .x/ D .bx 1/2 is positive (or negative) for all x ¤ Ê1=b provided ab > 1 (or ab < 1), we have that f is self-inverse in c D 1, and a and b are arbitrary except that ab ¤ 1.

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ADAMS and ESSEX: CALCULUS 9

36. Let f .x/ be an even function. Then f .x/ D f . x/. Hence, f is not one-to-one and it is not invertible. Therefore, it cannot be self-inverse. An odd function g.x/ may be self-inverse if its graph is symmetric about the line x D y. Examples are g.x/ D x and g.x/ D 1=x.

37. No. A function that is one-to-one on a single interval need not be either increasing or decreasing. For example, consider the function defined on Œ0; 2 by f .x/ D



if 0  x  1 if 1 < x  2.

x x

7.

log1=3 32x D log1=3

8.

43=2 D 8

9.

10

D

2x

D 3 2

2x )

p 2log4 8 D 23=2 D 2 2

1 Dx 1=x

 10. Since loga x 1=.loga x/ D x 1=.loga x/ D a1 D a.

1 loga x D 1, therefore loga x

.loga b/.logb a/ D loga a D 1   12. logx x.logy y 2 / D logx .2x/ D logx x C logx 2 11.

It is one-to-one but neither increasing nor decreasing on all of Œ0; 2. 38. First we consider the case where the domain of f is a closed interval. Suppose that f is one-to-one and continuous on Œa; b, and that f .a/ < f .b/. We show that f must be increasing on Œa; b. Suppose not. Then there are numbers x1 and x2 with a  x1 < x2  b and f .x1 / > f .x2 /. If f .x1 / > f .a/, let u be a number such that u < f .x1 /, f .x2 / < u, and f .a/ < u. By the Intermediate-Value Theorem there exist numbers c1 in .a; x1 / and c2 in .x1 ; x2 / such that f .c1 / D u D f .c2 /, contradicting the one-to-oneness of f . A similar contradiction arises if f .x1 /  f .a/ because, in this case, f .x2 / < f .b/ and we can find c1 in .x1 ; x2 / and c2 in .x2 ; b/ such that f .c1 / D f .c2 /. Thus f must be increasing on Œa; b.

D 1 C logx 2 D 1 C

1 log2 x

1 D1 2

13.

.log4 16/.log4 2/ D 2 

14.

log15 75 C log15 3 D log15 225 D 2

.since 152 D 225/

15. 16.

17.

A similar argument shows that if f .a/ > f .b/, then f must be decreasing on Œa; b.

1.

log4 8 D

)

log10 .1=x/

  1 3

log6 9 C log6 4 D log6 36 D 2  2 2 4 3 2 log3 12 4 log3 6 D log3 24  34 D log3 .3 2 / D 2 loga .x 4 C 3x 2 C 2/ C loga .x 4 C 5x 2 C 6/ p 4 loga x 2 C 2     D loga .x 2 C 2/.x 2 C 1/ C loga .x 2 C 2/.x 2 C 3/ 2 log1 .x 2 C 2/

Finally, if the interval I where f is defined is not necessarily closed, the same argument shows that if Œa; b is a subinterval of I on which f is increasing (or decreasing), then f must also be increasing (or decreasing) on any intervals of either of the forms Œx1 ; b or Œa; x2 , where x1 and x2 are in I and x1  a < b  x2 . So f must be increasing (or decreasing) on the whole of I .

18.

Section 3.2 Exponential and Logarithmic Functions (page 175)

19.

p

20.

log3 5 D .log10 5/=.log10 3  1:46497

21.

22x D 5xC1 , 2x log10 2 D .x C 1/ log10 5, x D .log10 5/=.2 log10 2 log10 5/  7:21257 p p x D log10 3, x 2 D 3, 2 log p 10 x D 10.log10 3/= 2  2:17458

33 p D 33 35

2. 2

1=2 1=2

3. .x

D2

8

3

/

2

5=2

Dx

4. . 21 /x 4x=2

D 31=2 D

1=2 3=2

2

6

D loga .x 4 C 4x 2 C 3/

3

2

D2 D4 22.

2x D x D1 2

5. log5 125 D log5 53 D 3

6. If log4 . 18 / D y then 4y D 18 , or 22y D 2 2y D 3 and log4 . 18 / D y D 32 .

84

D loga .x 2 C 1/ C loga .x 2 C 3/

3

. Thus

log .1

cos x/ C log .1 C cos x/ 2 log sin x  sin2 x .1 cos x/.1 C cos x/ D log D log  sin2 x sin2 x D log 1 D 0 p p 2 yD3 p , log10 y D 2 log10 3, y D 10 2 log10 3  4:72880 

23.

logx 3 D 5, .log10 3/=.log10 x/ D 5, log10 x D .log10 3/=5, x D 10.log10 3/=5  1:24573

24.

log3 x D 5, .log10 x/=.log10 3/ D 5, log10 x D 5 log10 3, x D 105 log10 3 D 35 D 243

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INSTRUCTOR’S SOLUTIONS MANUAL

  1 1 then au D D x x x and u D  logax. 1 D loga x. Thus, loga x

25. Let u D loga

26. Let loga x D u, loga y D v. Then x D au , y D av . au x D v D au v Thus y  a x and loga D u v D loga x y 27.

1

SECTION 3.3 (PAGE 183)

. Hence, a

u

Dx

35.

h!0

1 h

D k. Thus

axCh ax h h!0 ax ah ax D lim h h!0 h a 1 D ax f 0 .0/ D ax k D kf .x/: D ax lim h h!0

f 0 .x/ D lim

loga y. 36.

Let u D loga .x y /, then au D x y and au=y D x. u D loga x, or u D y loga x. Therefore y y Thus, loga .x / D y loga x.

1

yDf

Thus .f

28. Let logb x D u, logb a D v. Thus b u D x and b v D a. Therefore x D b u D b v.u=v/ D au=v u logb x and loga x D D . v logb a 29.

ah

f .x/ D ax and f 0 .0/ D lim

.x/ ) x D f .y/ D ay dx dy )1D D kay dx dx 1 1 dy D D : ) dx kay kx 1 0

/ .x/ D 1=.kx/.

Section 3.3 The Natural Logarithm and Exponential Functions (page 183)

1.

e3 p D e3 e5

2.

ln.e 1=2 e 2=3 / D

3.

e 5 ln x D x 5

4.

e .3 ln 9/=2 D 93=2 D 27

5.

ln

log3 x 2 C log3 x 1=2 D 10

6.

x 5=2 D 310 ; so x D .310 /2=5 D 34 D 81

 2 e 2 ln cos x C ln e sin x D cos2 x C sin2 x D 1

7.

3 ln 4

8.

4 ln

9.

2 ln x C 5 ln.x

log4 .x C 4/

2 log4 .x C 1/ D

1 2

xC4 1 D 2 .x C 1/ 2 xC4 1=2 D4 D2 .x C 1/2 2x 2 C 3x 2 D 0 but we need x C 1 > 0, so x D 1=2. log4

30. First observe that log9 x D log3 x= log3 9 D 2 log3 x C log9 x D 10

1 2

log3 x. Now

log3 x 5=2 D 10

31. Note that logx 2 D 1= log2 x. Since limx!1 log2 x D 1, therefore limx!1 logx 2 D 0. 32. Note that logx .1=2/ D logx 2 D 1= log2 x. Since limx!0C log2 x D 1, therefore limx!0C logx .1=2/ D 0. 33. Note that logx 2 D 1= log2 x. Since limx!1C log2 x D 0C, therefore limx!1C logx 2 D 1. 34. Note that logx 2 D 1= log2 x. Since limx!1 log2 x D 0 , therefore limx!1 logx 2 D 1.

5=2

1 D ln e e 3x

p

p

D e 1=2 D 1 2

C

3x

D

4 ln 3 D ln

2 3

D

e

7 6

3x

64 43 D ln 34 81

x C 6 ln.x 1=3 / D 2 ln x C 2 ln x D 4 ln x  2/ D ln x 2 .x

2/5



10. ln.x 2 C 6x C 9/ D lnŒ.x C 3/2  D 2 ln.x C 3/ 11.

2xC1 D 3x .x C 1/ ln 2 D x ln 3 ln 2 ln 2 xD D ln 3 ln 2 ln.3=2/

12.

3x D 91 )

x

) 3x D 32.1

x D 2.1

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x/

)

x/

xD

2 3

85

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SECTION 3.3 (PAGE 183)

13.

14.

ADAMS and ESSEX: CALCULUS 9

5 1 D xC3 2x 8 x ln 2 D ln 5 .x C 3/ ln 8 D ln 5 .3x C 9/ ln 2 2x ln 2 D ln 5 9 ln 2 ln 5 9 ln 2 xD 2 ln 2 2x

2

3

2

D 4x D 22x ) x 2

y D ln ln x

34.

y D x ln x

x   1 y D ln x C x x 0

35.

3 D 2x

x 2x 3 D 0 ) .x Hence; x D 1 or 3:

3/.x C 1/ D 0

x2 2 x2 0 y D 2x ln x C x

36.

y D ln j sin xj;

37.

y D 52xC1

16. ln.x 2 x 2/ D lnŒ.x 2/.x C 1/ is defined if .x 2/.x C 1/ > 0, that is, if x < 1 or x > 2. The domain is the union . 1; 1/ [ .2; 1/.

38.

17.

ln.2x 5/ > ln.7 2x/ holds if 2x 5 > 0, 7 2x > 0, and 2x 5 > 7 2x, that is, if x > 5=2, x < 7=2, and 4x > 12 (i.e., x > 3). The solution set is the interval .3; 7=2/.

2 2 18. ln.x 2 2/  ln x holds 2  x. p if x > 2, x > 0, and x Thus we need x > 2 and x 2 x 2  0. This latter inequality says that .x 2/.x C 1/  0, so it holds for 1  x  2. The solution set of the given inequality is p . 2; 2.

39. 40. 41.

D .1

2x/e

22. y D x 2 e x=2 ; 23. y D ln.3x

42.

24.

y D ln j3x

y0 D

2j;

0

3x 2 ex y0 D 1 C ex

2

27.

yD

ex C e 2

f 0 .x/ D .2x/e x

x

y0 D

;

x

30. y D

32. y D e

86

y 0 D e x e .e

ex D1 1 C ex

31. y D e x sin x; x

ex

e

44.

2

x

2

45.

dx 1 D 3e 3t ln t C e 3t dt t

28. x D e 3t ln t; 29. y D e .e / ;

2 3

cos x;

x/

D e xCe

1 ; 1 C ex

ex .1 C e x /2

y 0 D e x .sin x C cos x/ y0 D

e

x

cos x

e

3xC8/

h.t / D t x

xt ;

y 0 D .2x

;

x

sin x

46.

3/.ln 2/2.x

g 0 .x/ D t x x t ln t C t xC1 x t h0 .t / D xt x

f .s/ D loga .bs C c/ D

1

2

3xC8/

1

x t ln x

ln.bs C c/ ln a

b .bs C c/ ln a

ln.2x C 3/ g.x/ D logx .2x C 3/ D ln x     2 1 ln x Œln.2x C 3/ 2x C 3 x 0 g .x/ D .ln x/2 2x ln x .2x C 3/ ln.2x C 3/ D x.2x C 3/.ln x/2 yDx

p

x

p

De 

x ln x

p  ln x x p C x 2 x    p 1 1 ln x C 1 Dx x p x 2  ln x 1 Given that y D , let u D ln x. Then x D e u and x  u 1 2 yD D .e u /u D e u . Hence, eu     1 dy du 2 ln x 1 ln x dy 2 : D  D . 2ue u / D dx du dx x x x p

x ln x

y D ln j sec x C tan xj

sec x tan x C sec2 x sec x C tan x D sec x p y D ln jx C x 2 a2 j 2x 1C p 2p x 2 a2 D p 1 y0 D x C x 2 a2 x 2 a2 y0 D

x

y0 D

2

g.x/ D t x x t ;

y0 D e

3 3x

y D

25. y D ln.1 C e x / 26. f .x/ D e x ;

43.

y 0 D 2xe x=2 C 12 x 2 e x=2 2/

y D 2.x

f 0 .s/ D

1

2x

2x D 2x ln x 2 cos x D cot x y0 D sin x

y 0 D 2.52xC1 / ln 5 D .2 ln 5/52xC1

19. y D e 5x ; y 0 D 5e 5x

20. y D xe x x; y 0 D e x C xe x x 21. y D 2x D xe 2x e y 0 D e 2x 2xe 2x

1 D ln x

y D x 2 ln x

ln.x=.2 x// is defined if x=.2 x/ > 0, that is, if 0 < x < 2. The domain is the interval .0; 2/.

15.

1 x ln x

y0 D

33.

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INSTRUCTOR’S SOLUTIONS MANUAL

47.

48.

p y D ln. x 2 C a2 x/ x 1 p x 2 C a2 0 y D p x 2 C a2 x 1 D p x 2 C a2 x

y D .cos x/

x

cos x

53.

b)

De

x ln cos x

x

f .x/ D .x x /x D x .x



x tan x/

f 0 D xx

54.

f 00 .x/ D e ax .2a C a2 x/

Given that x x

f 000 .x/ D e ax .3a2 C a3 x/ :: : 1

2 C1

xx

.2 ln x C 1/

!

f .x/ D xe ax f 0 .x/ D e ax .1 C ax/

f .n/ .x/ D e ax .nan

2/

g.x/ D x ln g D x x ln x xx 1 0 g D x x .1 C ln x/ ln x C 0 g x   1 0 xx x g Dx x C ln x C .ln x/2 x Evidently g grows more rapidly than does f as x grows large.

.cos x/.ln x/

1 sin x ln x C cos x x

cos x

a)

ln f .x/ D x 2 ln x 1 0 f D 2x ln x C x f

e #  1 0 x ln cos x . sin x/ ln cos x C x y De cos x " # 1 .cos x/.ln x/ sin x ln x C cos x e x "

D .cos x/x .ln cos x

49.

SECTION 3.3 (PAGE 183)

:: x:

D a where a > 0, then ln a D x x

C an x/

Thus ln x D

50. Since

:: x:

ln x D a ln x:

1 ln a D ln a1=a , so x D a1=a . a

d .ax 2 C bx C c/e x D .2ax C b/e x C .ax 2 C bx C c/e x dx D Œax 2 C .2a C b/x C .b C c/e x D ŒAx 2 C Bx C C e x : 2

55.

x

Thus, differentiating .ax C bx C c/e produces another function of the same type with different constants. Any number of differentiations will do likewise. 51.

y D ex

2

y 0 D 2xe x

2

2

2

y 00 D 2e x C 4x 2 e x D 2.1 C 2x 2 /e x 2

2

2

y .4/ D 4.3 C 6x 2 /e x C 4.3x C 2x 3 /2xe x

52.

f .x/ D ln.2x C 1/ 00

2

f .x/ D . 1/2 .2x C 1/ f .4/ .x/ D

.3Š/24 .2x C 1/

2

2

2

56. f 0 .x/ D 2.2x C 1/

2

000

4

3

1

f .x/ D .2/2 .2x C 1/

Thus, if n D 1; 2; 3; : : : we have f .n/ .x/ D . 1/n 1 .n 1/Š2n .2x C 1/

4/

2

y 000 D 2.4x/e x C 2.1 C 2x 2 /2xe x D 4.3x C 2x 3 /e x D 4.3 C 12x 2 C 4x 4 /e x

f .x/ D .x 1/.x 2/.x 3/.x 4/ ln f .x/ D ln.x 1/ C ln.x 2/ C ln.x 3/ C ln.x 1 1 1 1 1 f 0 .x/ D C C C f .x/ x 1 x 2 x 3 x 4   1 1 1 1 C C C f 0 .x/ D f .x/ x 1 x 2 x 3 x 4

n

.

3

p

1 C x.1 x/1=3 .1 C 5x/4=5 1 ln F .x/ D 2 ln.1 C x/ C 13 ln.1 x/ 54 ln.1 C 5x/ 1 1 4 F 0 .x/ D F .x/ 2.1 C x/ 3.1 x/ .1 C 5x/ # "   1 1 4 23 1 1 0 4 D F .0/ D F .0/ D .1/ 2 3 1 2 3 6

F .x/ D

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SECTION 3.3 (PAGE 183)

57.

ADAMS and ESSEX: CALCULUS 9

.x 2 1/.x 2 2/.x 2 3/ .x 2 C 1/.x 2 C 2/.x 2 C 3/ 321 1 f .2/ D D ; f .1/ D 0 567 35 2 2 ln f .x/ D ln.x 1/ C ln.x 2/ C ln.x 2

61.

f .x/ D

2

2

3/

xDa

2

ln.x C 1/ ln.x C 2/ ln.x C 3/ 1 2x 2x 2x 0 f .x/ D 2 C 2 C 2 f .x/ x 1 x 2 x 3 2x 2x 2x x2 C 1  x2 C 2 x2 C 3 1 1 1 C 2 C 2 f 0 .x/ D 2xf .x/ 2 x 1 x 2 x 3  1 1 1 x2 C 1 x2 C 2 x2 C 3   4 1 1 1 1 1 1 f 0 .2/ D C C 35 3 2 1 5 6 7 139 556 4  D D 35 105 3675 2 Since f .x/ D .x 1/g.x/ where g.1/ ¤ 0, then f 0 .x/ D 2xg.x/ C .x 2 1/g 0 .x/ and 1 . 1/. 2/ D . f 0 .1/ D 2g.1/ C 0 D 2  234 6 x2

58. Since y D x 2 e y 0 D 2xe

x2

Let the point of tangency be .a; e a /. Tangent line has slope ˇ d x ˇˇ ea 0 D e ˇ D ea : a 0 dx ˇ

Therefore, a D 1 and line has slope e. The line has equation y D ex. y

.a;e a /

y D ex x

Fig. 3.3-61 62.

, then

ˇ ˇ 1 1 ˇ The slope of y D ln x at x D a is y 0 D ˇ D : The xˇ a xDa line from .0; 0/ to .a; ln a/ is tangent to y D ln x if ln a 0 1 D a 0 a

2x 3 e

x2

D 2x.1

x/.1 C x/e

The tangent is horizontal at .0; 0/ and

x2

:

i.e., if ln a D 1, or a D e. Thus, the line is y D

  1 . ˙1; e

y

x . e

.a; ln a/ 59. f .x/ D xe f 0 .x/ D e

x x

.1

x/,

C.P. x D 1, f .1/ D

f 0 .x/ > 0 if x < 1 (f increasing) f 0 .x/ < 0 if x > 1 (f decreasing)

x

1 e

y D ln x Fig. 3.3-62

y .1;1=e/ y

Dxe

x

63. x

Let the point of tangency be .a; 2a /. Slope of the tangent is ˇ d x ˇˇ 2a 0 D 2 ˇ D 2a ln 2: a 1 dx ˇ xDa

1 1 ; a D1C . Thus a 1 D ln 2 ln 2 So the slope is 2a ln 2 D 21C.1= ln 2/ ln 2 D 2e ln 2. 1 (Note: ln 21= ln 2 D ln 2 D 1 ) 21= ln 2 D e) ln 2 The tangent line has equation y D 2e ln 2.x 1/.

Fig. 3.3-59 64. 1 D 4 then x D 14 and x y D ln 41 D ln 4. The tangent line of slope 4 is y D ln 4 C 4.x 14 /, i.e., y D 4x 1 ln 4.

60. Since y D ln x and y 0 D

88

The tangent line to y D ax which passes through the origin is tangent at the point .b; ab / where ˇ d x ˇˇ ab 0 D a ˇ D ab ln a: b 0 dx ˇ

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xDb

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 3.3 (PAGE 183)

1 D ln a, so ab D a1= ln a D e. The line y D x b will intersect y D ax provided the slope of this tangent e line does not exceed 1, i.e., provided  1, or e ln a  1. b Thus we need a  e 1=e . Thus

70.

y

(a) If Aa CBb D 1 and Ba Ab D 0, then A D

.b; ab /

and B D Z

y D ax x

1 x DxC y y   y y xy 0 x D1 e xy .y C xy 0 / ln C e xy y x y2   1 At e; we have e   1 1 C ey 0 2 C e 2 .e e 3 y 0 / D 1 e 2 y 0 e e e 2 C 2e 2 y 0 C 1 e 2 y 0 D 1 e 2 y 0 . 1 Thus the slope is y 0 D . e2

b (b) If Aa CBb D 0 and Ba Ab D 1, then A D 2 a C b2 a and B D 2 . Thus a C b2

65. e xy ln

1 0 y y2

Z

e ax sin bx dx  1 ae ax sin bx D 2 2 a Cb

66. xe y C y 2x D ln 2 ) e y C xe y y 0 C y 0 2 D 0: At .1; ln 2/, 2 C 2y 0 C y 0 2 D 0 ) y 0 D 0. Therefore, the tangent line is y D ln 2.

68.

b . Thus a2 C b 2

a a2 C b 2

e ax cos bx dx   1 ae ax cos bx C be ax sin bx C C: D 2 2 a Cb

Fig. 3.3-64

67.

d .Ae ax cos bx C Be ax sin bx/ dx D Aae ax cos bx Abe ax sin bx C Bae ax sin bx C Bbe ax cos bx D .Aa C Bb/e ax cos bx C .Ba Ab/e ax sin bx:

f .x/ D Ax cos ln x C Bx sin ln x f 0 .x/ D A cos ln x A sin ln x C B sin ln x C B cos ln x D .A C B/ cos ln x C .B A/ sin ln x 1 If A D B D then f 0 .x/ D cos ln x. Z 2 1 1 Therefore cos ln x dx D x cos ln x C x sin ln x C C . 2 2 1 1 If B D , A D then f 0 .x/ D sin ln x. 2 Z 2 1 1 x cos ln x C C . Therefore sin ln x dx D x sin ln x 2 2 FA;B .x/ D Ae x cos x C Be x sin x d FA;B .x/ dx D Ae x cos x Ae x sin x C Be x sin x C Be x cos x D .A C B/e x cos x C .B A/e x sin x D FACB;B A .x/

71.

 be ax cos bx C C:

    1 1 d 1 1 C D ln C ln x D dx x 1=x x 2 x

1 1 C D 0: x x

1 C ln x D C (constant). Taking x D 1, we x 1 get C D ln 1 C ln 1 D 0. Thus ln D ln x. x   x 1 1 ln D ln x D ln x C ln D ln x ln y: y y y

Therefore ln

72.

73.

r rx r 1 r r d Œln.x r / r ln x D D D 0. dx xr x x x Therefore ln.x r / r ln x D C (constant). Taking x D 1, we get C D ln 1 r ln 1 D 0 0 D 0. Thus ln.x r / D r ln x.

74. Let x > 0, and F .x/ be the area bounded by y D t 2 , the t -axis, t D 0 and t D x. For h > 0, F .x C h/ F .x/ is the shaded area in the following figure. y

d FA;B .x/ D FACB;B A .x/ we have 69. Since dx 2 d d FA;B .x/ D FACB;B A .x/ D F2B; 2A .x/ a) dx 2 dx d3 x d3 d b) e cos x D F1;0 .x/ D F0; 2 .x/ 3 3 dx dx dx x x D F 2; 2 .x/ D 2e cos x 2e sin x

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y D t2

x

xCh

t

Fig. 3.3-74

89

lOMoARcPSD|6566483

SECTION 3.3 (PAGE 183)

ADAMS and ESSEX: CALCULUS 9

c) The tangent to y D 1=t at t D 2 has slope equation is

Comparing this area with that of the two rectangles, we see that hx 2 < F .x C h/

F .x/ < h.x C h/2 :

Hence, the Newton quotient for F .x/ satisfies F .x C h/ x < h 2

F .x/

h!0C

F .x C h/ h

< .x C h/ :

F .x/

yD

1 3

F .x C h/ h

F .x/

h!0

F .x C h/ h

F .x/

< x2;

A2 D

D x2:

1

1

t

A2 2

0

lim x 3 e

x

x!1

2.

lim x

x!1



1 2



D lim

x : 9

3 1 C 4 2



D

5 : 8

4 1 C 9 3



D

7 : 18

x!1

3 x

e D lim

x!1

ex D1 x3

2e x 3 2 3e D lim x!1 e x C 5 x!1 1 C 5e

4.

x 2e x!1 x C 3e

lim

lim

x x

D lim

lim x ln x D 0 .power wins/

x!0C t

6. 2

b) If f .t / D 1=t , then f .t / D 1=t and f 00 .t / D 2=t 3 > 0 for t > 0. Thus f 0 .t / is an increasing function of t for t > 0, and so the graph of f .t / bends upward away from any of its tangent lines. (This kind of argument will be explored further in Chapter 5.)

lim

x!0C

7.

ln x D x

1

lim x.ln jxj/2 D 0

x!0

8.

D

2 0 D2 1C0

1 2=.xe x / 1 0 D D1 x!1 1 C 3=.xe x / 1C0

x x

(page 191)

x3 D 0 (exponential wins) ex

3.

5. 3

Fig. 3.3-75

90

1.

yD1=t

2

1 2

Section 3.4 Growth and Decay

a) The shaded area A in part (i) of the figure is less than the area of the rectangle (actually a square) with base from t D 1 to t D 2 and height 1=1 D 1. Since ln 2 D A < 1, we have 2 < e 1 D e; i.e., e > 2. (i) (ii) y y

A1

2 3

7 73 5 C D > 1. 8 18 72 1 Thus 3 > e D e. Combining this with the result of (a) we conclude that 2 < e < 3.

F .0/ D C D 0, therefore F .x/ D 31 x 3 . For x D 2, the area of the region is F .2/ D 83 square units.

A

3/ or y D

1=9. Its

e) ln 3 > A1 C A2 D

F .x C h/ F .x/ d F .x/ D lim D x2: dx h h!0 Z Therefore F .x/ D x 2 dx D 31 x 3 C C . Since

yD1=t

x : 4

The trapezoid bounded by x D 2, x D 3, y D 0, and y D .2=3/ .x=9/ has area

Combining these two limits, we obtain

75.

1 .x 9

A1 D

so similarly, lim

or y D 1

d) The trapezoid bounded by x D 1, x D 2, y D 0, and y D 1 .x=4/ has area

D x2:

If h < 0 and 0 < x C h < x, then .x C h/2
5 we have dx=dt D k2 x, so that x.t / D x.5/e k2 .t

5/

x.7/ D x.5/e 2k2 D 3;000

÷

 5=2 x.10/ D x.5/35k2 D x.5/ e 2k2  142:

3;000 22;918   3;000 5=2  22;918 22;918

25.

e 2k2 

so there are approximately 142 rabbits left after 10 years. 22. Let N.t / be the number of rats on the island t months after the initial population was released and before the first cull. Thus N.0/ D R and N.3/ D 2R. Since N.t / D Re k t , we have e 3k D 2, so e k D 21=3 . Hence N.5/ D Re 5k D 25=3 R. After the first 1,000 rats are killed the number remaining is 25=3 R 1;000. If this number is less than R, the number at the end of succeeding 5-year periods will decline. The minimum value of R for which this won’t happen must satisfy 25=3 R 1;000 D R, that is, R D 1;000=.25=3 1/  459:8. Thus R D 460 rats should be brought to the island initially.

dx D a bx.t /. dt This says that x.t / is increasing if it is less than a=b and decreasing if it is greater than a=b. Thus, the limiting concentration is a=b.

a) The concentration x.t / satisfies

b) The differential equation for x.t / resembles that of Exercise 21(b), except that y.x/ is replaced by x.t /, and b is replaced by b. Using the result of Exercise 21(b), we obtain, since x.0/ D 0,  a a  bt e C x.t / D x.0/ b  b a D 1 e bt : b

x.t / D x.0/e k1 t D 1;000e k1 t

x.5/ D 1;000e 5k1

26.

Let T .t / be the reading t minutes after the Thermometer is moved outdoors. Thus T .0/ D 72, T .1/ D 48. dT D k.T 20/. By Newton’s law of cooling, dt dV If V .t / D T .t / 20, then D kV , so dt kt kt V .t / D V .0/e D 52e . Also 28 D V .1/ D 52e k , so k D ln.7=13/. Thus V .5/ D 52e 5 ln.7=13/  2:354. At t D 5 the thermometer reads about T .5/ D 20 C 2:354 D 22:35 ı C. Let T .t / be the temperature of the object t minutes after its temperature was 45 ı C. Thus T .0/ D 45 and dT D k.T C 5/. Let T .40/ D 20. Also dt u.t / D T .t / C 5, so u.0/ D 50, u.40/ D 25, and dT du D D k.T C 5/ D ku. Thus, dt dt u.t / D 50e k t ;

23. f 0 .x/ D a C bf .x/.

92

a : b

b) If

in one year, if compounding is performed n times per year. For i D 9:5 and n D 12, we have

21.

 a D C e bx

25 D u.40/ D 50e 40k ; 1 25 1 1 )k D ln D ln : 40 50 40 2

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 3.5 (PAGE 199)

We wish to know t such that T .t / D 0, i.e., u.t / D 5, hence 5 D u.t / D 50e k t   5 40 ln 50   D 132:88 min: tD 1 ln 2 Hence, it will take about .132:88 more to cool to 0 ı C. 27.

30.

40/ D 92:88 minutes

Let T .t / be the temperature of the body t minutes after it was 5 ı . Thus T .0/ D 5, T .4/ D 10. Room temperature = 20ı . dT By Newton’s law of cooling (warming) D k.T 20/. dt dV If V .t / D T .t / 20 then D kV , dt so V .t / D V .0/e k t D 15e k t .   2 1 . Also 10 D V .4/ D 15e 4k , so k D ln 4 3 kt If T .t / D 15ı , then 5 D  V.t / D 15e 1   ln 1 1 3 D 4    10:838. so t D ln 2 k 3 ln 3 It will take a further 6.84 minutes to warm to 15 ı C.

31.

Ly0 y0 C .L y0 /e

k

y2 D

;

Ly0 y0 C .L y0 /e

Thus y1 .L y0 /e k D .L y1 /y0 , and y2 .L y0 /e 2k D .L y2 /y0 . Square the first equation and thus eliminate e 

.L y1 /y0 y1 .L y0 /

2

D

32.

t!1

k

:

y12 .y0 C y2 / 2y0 y1 y2 . y12 y0 y2 If y0 D 3, y1 D 5, y2 D 6, then 25.9/ 180 45 LD D  6:429. 25 18 7

29. The rate of growth of y in the logistic equation is

Since dy D dt

 k y L

L 2

2

C

kL ; 4

L 1 C Me k t L 200 D y.0/ D 1CM L 1; 000 D y.1/ D 1 C Me k 10; 000 D lim y.t / D L y.t / D

Thus 200.1 C M / D L D 10; 000, so M D 49. Also 1; 000.1 C 49e k / D L D 10; 000, so e k D 9=49 and k D ln.49=9/  1:695. 33.

L 10; 000 D  7671 cases 1 C 49.9=49/3 1 C Me 3k LkMe 3k  3; 028 cases/week: y 0 .3/ D .1 C Me 3k /2 y.3/ D

Section 3.5 The Inverse Trigonometric Functions (page 199)

Assuming L ¤ 0, L D

dy D ky 1 dt

kt

Assuming k and L are positive, but y0 is negative, we have t  > 0. The solution is therefore valid on . 1; t  /. The solution approaches 1 as t ! t  .

2k

.L y2 /y0 y2 .L y0 /

 y : L

Ly0 y0 C .L y0 /e

of the logistic equation is valid on any interval containing t D 0 and not containing any point where the denominator is zero. The denominator is zero if y0 D .y0 L/e k t , that is, if   y0 1  ln : t Dt D k y0 L

Now simplify: y0 y2 .L y1 /2 D y12 .L y0 /.L y2 / y0 y2 L2 2y1 y0 y2 LCy0 y12 y2 D y12 L2 y12 .y0 Cy2 /LCy0 y12 y2



The solution yD

28. By the solution given for the logistic equation, we have y1 D

L dy is greatest when y D . dt 2 Ly0 The solution y D is valid on the y0 C .L y0 /e k t largest interval containing t D 0 on which the denominator does not vanish. If y0 > L then y0 C .L y0 /e k t D 0 if y0 1 ln . t D t D k y0 L Then the solution is valid on .t  ; 1/. limt!t  C y.t / D 1. thus

p

3  D 2 3   2 1 D 2 3

1.

sin

1

2.

cos

1

3.

tan

1

4.

sec

1

5.

sin.sin

 4

. 1/ D p

2D

1

 4

0:7/ D 0:7

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93

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SECTION 3.5 (PAGE 199)

6.

1

cos.sin

q

0:7/ D

p

D tan

1

8. sin

1

7.

9.

10.

11.

cos



tan

1



 sin cos

1

 cos tan

sin.cos

14.

cos.sin

15.

cos.tan

18.

D tan

1

1



1 3/

.

1

1

17.

1

1

p

.

D p

.cos 40ı / D 50ı

1 2



q 1 q D 1

cos2 . arccos . 13 / p p 8 2 2 1 D D 9 3 3

D

D

D p 20.

1

 sec tan



1 2 1 D s  1 C tan2 tan 1

1

21.

22.

q x/ D 1 x/ D

x/ 24.

sin

1 sec.tan

2

1

sin

x/

1



x D

D p

p

1

cos.sec

94

1

25. x2

1

26.

27. p

1 x2 1 1 D 2 x jxj p ) tan.sec 1 x/ D x 2 1 sgn x p x2 1 if x  1 p D x 2 1 if x  1 1

x/ D

1 a b/ a2

1

a2

1

1

u D z 2 sec

1

x

xCp

1

f .t / D t tan

(assuming) a > 0/:

b/2

.x

f .x/ D x sin

tC 1

x x2

1

:

t t 1 C t2

.1 C z 2 /

1

.1 C z 2 / C

F .x/ D .1 C x 2 / tan

y D sin y0 D r

sin.cos x/ cos.cos 1 x p 1 x2 .by # 13/ D x 1 ) sin.sec x

a : 1 C .ax C b/2

2

.x

1

F .x/ D 2x tan

x/ D

x/ D

D p

y0 D

b a 1

0

1

r

x2

x

1

r

4x C 1/

z 2 .2z/ p .1 C .1 C z 2 /2 2 2z sgn .z/ p D 2z sec 1 .1 C z 2 / C .1 C z 2 / z 2 C 2

1C 1 ) cos. arctan x/ D p 1 C x2 x ) sin. arctan x/ D p 1 C x2

tan.cos

3 2

.ax C b/;

y D cos

1

tan. arctan x/ D x ) sec. arctan x/ D

2x

2Cx 1



2 2 3 1

.4x 2 1

9

du D 2z sec dz

x2

1 C x2 p

3



f 0 .t / D tan

x2

1

1

f .x/ D sin

2

23. cos2 .cos 1

2x

0

200/ D 200 p x/ D 1 p D 1



1

y D tan

y0 D

2  D p5 1

1

y D sin y0 D s

 3

3/ D

1

cos

19.

    sin. 0:2/ D sin 1 sin. 0:2/ 2  D C 0:2 2

1

16.



sin2 . arcsin 0:7/ p 0:49 D 0:51

1

.cos 40ı / D 90ı

12. tan.tan 13.

2 3

ADAMS and ESSEX: CALCULUS 9

1

a x

1  a 2

1

G.x/ D

1

x

1

z2/

x

xC1 h

.jxj > jaj/ a i a D p x2 jxj x 2

a2

sin 1 x sin 1 .2x/ sin

1

.2x/ p

1

sin

1

xp

2

1 4x 2 2 1 .2x/ p p 1 2 1 4x sin .2x/ 2 1 x 2 sin 1 x D  2 p p 1 x 2 1 4x 2 sin 1 .2x/

G 0 .x/ D

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x2

1  sin

1

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

28.

sin 1 t sin  t

H.t / D

sin t 0

H .t / D

29.

30.

35.

p



1

t2 sin2 t

1

1 p .sin t / 1

D

SECTION 3.5 (PAGE 199)

1

sin

t cos t

csc t cot t sin

t2

1

t

f .x/ D .sin 1 x 2 /1=2 2x 1 f 0 .x/ D .sin 1 x 2 / 1=2 p 2 1 x4 x D p p 1 x 4 sin 1 x 2   a 1 y D cos p a2 C x 2 ! 1=2 " a 2 a2 0 .a C x 2 / y D 1 2 2 a Cx 2 asgn .x/ a2 C x 2 p y D a2 x 2 C a sin

36.

3=2

#

.2x/

37.

1 d sin 1 x D p > 0 on . 1; 1/. dx 1 x2 1 Therefore, sin is increasing. 1 d tan 1 x D > 0 on . 1; 1/: dx 1 C x2 1 Therefore tan is increasing. d 1 < 0 on . 1; 1/. cos 1 x D p dx 1 x2 1 Therefore cos is decreasing. Since the domain of sec 1 consists of two disjoint intervals . 1; 1 and Œ1; 1/, the fact that the derivative of sec 1 is positive wherever defined does not imply that sec 1 is increasing over its whole domain, only that it is increasing on each of those intervals taken independently. In fact, sec 1 . 1/ D  > 0 D sec 1 .1/ even though 1 < 1. d csc dx

1

D

31.

y0 D

p

D p

32.

x a2

a

x2 x

x2  y D a cos 1 1 0

y D

a2

"

a 1 x

D p

D

 1

1

1 a x a2

D

2

then p

1

1 x2

x, then y 0 D p

D 2 so that x D ˙

1 of the two tangentplines are   3  and y D y D C2 x 3 2



1 y

x

y D csc

1

x

. 1; =2/

38.

cot 1 x D arctan .1=x/I d 1 1 cot 1 x D D 1 x2 dx 1C 2 x y

1 1 C x2 =2

y D cot

1

x x

=2

Fig. 3.5-38

x2

p

1 x2

Fig. 3.5-37

1 1

1 x

.1;=2/

a x .a > 0/ aCx  p x 2ax x 2 .a > 0/ a  # 1=2   1 2a 2x x 2 p a a 2 2ax x 2

2ax x 2   2x x 33. tan 1 D 2 y y 1 2y 2xy 0 y 2 2xyy 0 D 2 2 y y4 4x 1C 2 y 4 4y 0 1 4 2y 0 D At .1; 2/ 2 4 16  2 8 4y 0 D 4 4y 0 ) y 0 D  1  2 At .1; 2/ the slope is  1 34. If y D sin

1

1 x2 1 p jxj x 2 1

1

Cr r

x a a

d sin dx 1 D r

xD

. If the slope is 2

3 : Thus the equations 2 p   3  C2 xC . 3 2

Remark: the domain of cot 1 can be extended to include 0 by defining, say, cot 1 0 D =2. This will make cot 1 right-continuous (but not continuous) at x D 0. It is also possible to define cot 1 in such a way that it is continuous on the whole real line, but we would then lose the identity cot 1 x D tan 1 .1=x/, which we prefer to maintain for calculation purposes.

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95

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SECTION 3.5 (PAGE 199)

39.

ADAMS and ESSEX: CALCULUS 9

  d 1 tan 1 x C tan 1 dx x   1 1 1 D 0 if x ¤ 0 D C 1 1 C x2 x2 1C 2 x Thus tan 1 x C cot 1 x D C1 (const. for x > 0)   At x D 1 we have C D C1 4 4  for x > 0. Thus tan 1 x C cot 1 x D 2 1 1 Also tan x C cot x D C2 for .x < 0/.   D C2 . At x D 1, we get 4 4  Thus tan 1 x C cot 1 x D for x < 0. 2 d .tan dx

1

1

x C cot

40. If g.x/ D tan.tan

1

x/ D

42.

1

1 .cos x/ D p . sin x/ 1 cos2 x n 1 if sin x > 0 D 1 if sin x < 0

sin 1 .cos x/ is continuous everywhere and differentiable everywhere except at x D n for integers n. y y D sin 1 .cos x/ =2 

Fig. 3.5-42

1

43.

.tan x/ then h is periodic with period , h0 .x/ D

y

d 1 tan 1 .tan x/ D .sec2 x/ D 1 except at odd dx 1 C tan2 x multiples of =2. tan 1 .tan x/ is continuous and differentiable everywhere except at x D .2n C 1/=2 for integers n. It is not defined at those points. y y D tan 1 .tan x/ =2

sec2 x D1 1 C tan2 x

provided that x ¤ .k C 21 / where k is an integer. h.x/ is  not defined at odd multiples of . 2 y



.=2;=2/ yDtan.tan

1



 yDtan

Fig. 3.5.40(a) d cos dx

1



x

Fig. 3.5-43

1 .tan x/

Fig. 3.5.40(b)

1 .cos x/ D p . sin x/ 2x 1 cos n 1 if sin x > 0 D 1 if sin x < 0

44.

1

cos .cos x/ is continuous everywhere and differentiable everywhere except at x D n for integers n. y y D cos 1 .cos x/ 

1 d tan 1 .cot x/ D . csc2 x/ D dx 1 C cot2 x integer multiples of .





1 except at

tan 1 .cot x/ is continuous and differentiable everywhere except at x D n for integers n. It is not defined at those points. y y D tan 1 .cot x/ =2 



x

Fig. 3.5-41

96

x

x/ x

41.

 x

sec .tan x/ 1 C x2 1 C x2 1 C Œtan.tan 1 x/2 D D 1: D 2 1Cx 1 C x2

If h.x/ D tan and

1

x/ then

2

g 0 .x/ D

d sin dx

Fig. 3.5-44

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x

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INSTRUCTOR’S SOLUTIONS MANUAL

45. If jxj < 1 and y D tan and

tan y D p

1

p

x x2

1

SECTION 3.5 (PAGE 199)

x

1

sec2 y D 1 C .x 2 sec y D x;

x2

f 0 .x/  0 on . 1; 1/  x 1 tan Thus f .x/ D tan 1 xC1

1

D

1

x D C on . 1; 1/:

Evaluate the limit as x ! 1: lim f .x/ D tan

x! 1

Thus tan

50.

1



x 1 xC1

Since f .x/ D x



tan

tan

1

1

1

  3 D 2 4

1

xD

3 on . 1; 1/: 4

.tan x/ then sec2 x D1 1 C tan2 x

f 0 .x/ D 1

Thus sec y D x and y D sec 1p x. x2 1 If x  1 and y D  C sin 1 , then 2  y < x and sec y < 0. Therefore ! p p x2 1 x2 1 1 sin y D sin  C sin D x x 2

49.

1/ D x 2

because both x and sec y are negative. Thus y D sec 1 x in this case also. x , then y > 0 , x > 0 and 47. If y D sin 1 p 1 C x2 x sin y D p 1 C x2 1 x2 D cos2 y D 1 sin2 y D 1 2 1Cx 1 C x2 2 2 2 tan y D sec y 1 D 1 C x 1 D x2 tan y D x: x Thus y D tan 1 x and tan 1 x D sin 1 p . 1 C x2 p x2 1 48. If x  1 and y D sin 1 , then 0  y < 2 and x p x2 1 sin y D x 1 x2 1 D 2 cos2 y D 1 x2 x sec2 y D x 2 :

x

1

x

x2 1 x2 D sec2 y D 1 C 1 x2 1 x2 sin2 y D 1 cos2 y D 1 .1 x 2 / D x 2 sin y D x: x Thus y D sin 1 x and sin 1 x D tan 1 p . 1 x2 An alternative method of proof involves showing that the derivative of the left side minus the right side is 0, and both sides are 0 at x D 0. p p 46. If x  1 and y D tan 1 x 2 1, then tan y D x 2 1 and sec y D x, so that y D secp1 x. If x  1 and y D  tan 1 x 2 1, then 2 < y < 3 2 , so sec y < 0. Therefore p p tan y D tan. tan 1 x 2 1/ D x2 1

cos2 y D 1

because both x and sec y are negative. Thus y D sec in this case also.

, then y > 0 , x > 0

1D0

1 2 /

where k is an integer. Thus, f is  constant on intervals not containing odd multiples of . 2 f .0/ D 0 but f ./ D   0 D . There is no contradiction here because f 0 is not defined, so f is not constant 2 on the interval containing 0 and . if x ¤

51.

.k C

f .x/ D x 0

sin

1

.sin x/ 1

.   x  /

cos x 1 sin2 x cos x D1 j cos xj 8   < 0 if 1/ x2 1 R dx D tanh 1 x C C . 1 < x < 1/ 1 x2

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x

y D sech x

x

1

y D csch x D

2 ex C e

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 3.6 (PAGE 205)

y

6. Let y D sinh Thus,

1

x  a

d sinh dx

Z

dy , x D a sinh y ) 1 D a.cosh y/ . dx x

1

a

D

x

1

1 a cosh y

x

1

p

dx

a2

C

x2

D sinh

1

x C C: a

.a > 0/

x , x D a Cosh y D a cosh y a dy for y  0, x  a. We have 1 D a.sinh y/ . Thus, dx 1

Fig. 3.6-8 9.

x 1 D a a sinh y 1 1 D q D p 2 2 x a2 a cosh y 1

d cosh dx

p

1

1 1 D q D p 2 C x2 2 a a 1 C sinh y

Let y D cosh

Z

y D coth

1

dx

x2

a2

D cosh

1

x C C: a

Since sech 1 x D cosh 1 .1=x/ is defined in terms of the restricted function Cosh, its domain consists of the reciprocals of numbers in Œ1; 1/, and is therefore the interval .0; 1. The range of sech 1 is the domain of Cosh, that is, Œ0; 1/. Also, d sech dx

1

.a > 0; x  a/

x dy Let y D tanh 1 , x D a tanh y ) 1 D a.sech2 y/ . a dx Thus, x 1 d tanh 1 D dx a a sech2 y a a D D 2 2 2 tanh2 x a x2 a a Z 1 x dx D tanh 1 C C: a2 x 2 a a   1 1 1 x2 1 7. a) sinh ln x D .e ln x e ln x / D x D 2 2 x 2x   2 1 1 x C1 1 ln x xC D b) cosh ln x D .e C e ln x / D 2 2 x 2x sinh ln x x2 1 c) tanh ln x D D 2 cosh ln x x C1 x 2 C 1 C .x 2 1/ cosh ln x C sinh ln x D 2 D x2 d) cosh ln x sinh ln x .x C 1/ .x 2 1/   1 xC1 1 8. The domain of coth x D ln consists of all x 2 x 1 xC1 > 0. Since satisfying jxj > 1. For such x, we have x 1 this fraction takes very large values for x close to 1 and values close to 0 for x close to 1, the range of coth 1 x consists of all real numbers except 0. d coth dx

1

d 1 cosh 1 dx x  1 1 1 D p : D s  2 2 x x 1 x2 1 1 x

xD

y

y D Sech

1

x

x

1

Fig. 3.6-9 10.

csch 1 has domain and range consisting of all real numbers x except x D 0. We have d csch dx

1

d 1 sinh 1 dx x   1 1 1 D s  2 x 2 D jxjpx 2 C 1 : 1 1C x

xD

d 1 tanh 1 dx x 1 1 1 D D 2 : 2 2 1 .1=x/ x x 1

y

y D csch

1

x

x

xD

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Fig. 3.6-10

99

lOMoARcPSD|6566483

SECTION 3.6 (PAGE 205)

11.

fA;B .x/ D Ae kx C Be

0 fA;B .x/ D 00 fA;B .x/ D 00 Thus fA;B

kAe

kx

ADAMS and ESSEX: CALCULUS 9

kx

kBe

kx

k 2 Ae kx C k 2 Be k 2 fA;B D 0

auxiliary eqn

a/ C M sinh k.x

where A D 12 e

kx

ka

auxiliary eqn r 2 C 7r C 10 D 0 .r C 5/.r C 2/ D 0 C Be

2t

) rD

5; 2

C Be 3t

1 2;

) r D 0;

r2 D

3 2;

3/ D 0

and y D Ae

r 2 C 8r C 16 D 0

auxiliary eqn

y D Ae

4t

1; r D 3

2

2t

y 00 C 8y 0 C 16y D 0

5.

y 00

) rD

3 D 0 ) .2r C 1/.2r

C Bt e

.1=2/t

) rD

C Be .3=2/t :

4;

4

4t

2y 0 C y D 0

y 00

a/

r

6y 0 C 10y D 0

2

6r C 10 D 0

y D Ae 8.

3t

) r D3˙i

cos t C Be 3t sin t

9y 00 C 6y 0 C y D 0

9r 2 C 6r C 1 D 0 ) .3r C 1/2 D 0

Thus; r D

auxiliary eqn

y 00 C 7y 0 C 10y D 0

100

4r

M /.

Section 3.7 Second-Order Linear DEs with Constant Coefficients (page 212)

3D0

3y D 0

9.

k 2 y D 0 ) y D hL;M .x/ D L cosh k.x a/ C M sinh k.x y.a/ D y0 ) y0 D L C 0 ) L D y0 , v0 y 0 .a/ D v0 ) v0 D 0 C M k ) M D k Therefore y D hy0 ;v0 =k .x/ D y0 cosh k.x a/ C .v0 =k/ sinh k.x a/.

5t

4y 0

auxiliary eqn

D fA;B .x/

y D Ae

2

Thus; r1 D

a/

y 00

1.

4y 00 4r

k 2 y D 0 and

.L C M / and B D 12 e ka .L

t

r 2 2r C 1 D 0 ) .r 1/2 D 0 Thus; r D 1; 1; and y D Ae t C Bt e t :

hL;M .x/  M  L  kx ka e C e kxCka C e kx ka e kxCka D 2 2 ! ! L ka M ka kx L ka M ka e C e e e D e C e kx 2 2 2 2

13.

4.

7.

hence, hL;M .x/ is a solution of y 00

D Ae kx C Be

2r

y D A C Be

a/

a/ C M k 2 sinh k.x

3y D 0

r 2 C 2r D 0

auxiliary eqn

6.

D k hL;M .x/

2

y 00 C 2y 0 D 0

3.

12. Since

2

2y 0

y D Ae

00 gC;D .x/ D k 2 C cosh kx C k 2 D sinh kx 00 k 2 gC;D D 0 Thus gC;D cosh kx C sinh kx D e kx cosh kx sinh kx D e kx Thus fA;B .x/ D .A C B/ cosh kx C .A B/ sinh kx, that is, fA;B .x/ D gACB;A B .x/, and c D gC;D .x/ D .e kx C e kx / C .e kx e kx /, 2 2 that is gC;D .x/ D f.C CD/=2;.C D/=2 .x/.

00 hL;M .x/ D Lk 2 cosh k.x

r

kx

gC;D .x/ D C cosh kx C D sinh kx 0 gC;D .x/ D kC cosh kx C kD sinh kx

hL;M .x/ D L cosh k.x

y 00

2.

1 3;

1 3;

and y D Ae

.1=3/t

C Bt e

.1=3/t

:

y 00 C 2y 0 C 5y D 0

r 2 C 2r C 5 D 0 ) r D 1 ˙ 2i y D Ae t cos 2t C Be t sin 2t

10. For y 00 4y 0 C 5y D 0 the auxiliary equation is r 2 4r C 5 D 0, which has roots r D 2 ˙ i . Thus, the general solution of the DE is y D Ae 2t cos t C Be 2t sin t . 11.

For y 00 C 2y 0 C 3y D 0 the auxiliary equation isp r 2 C 2r C 3 D 0, which has solutions r D 1 ˙ 2i . Thus the general solution of the givenpequation is p y D Ae t cos. 2t / C Be t sin. 2t /.

12. Given that y 00 C y 0 C y D 0, hence r 2 C r C 1 D 0. Since a D 1, b D 1 and c D 1, the discriminant is D D b 2 4ac D 3 < 0 and .b=2a/ D 21 and p ! D 3=2. Thus, the general solution is p   p  3 3 t C Be .1=2/t sin t . y D Ae .1=2/t cos 2 2

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 3.7 (PAGE 212)

8 00 < 2y C 5y 0 3y D 0 13. y.0/ D 1 : 0 y .0/ D 0 The DE has auxiliary equation 2r 2 C 5y 3 D 0, with roots r D 12 and r D 3. Thus y D Ae t=2 C Be 3t . A Now 1 D y.0/ D A C B, and 0 D y 0 .0/ D 3B. 2 Thus B D 1=7 and A D 6=7. The solution is 6 1 y D e t=2 C e 3t . 7 7 14.

00

0

Given that y C 10y C 25y D 0, hence r 2 C 10r C 25 D 0 ) .r C 5/2 D 0 ) r D y D Ae

y0 D

5t

5e

C Bt e

5t

5. Thus,

0

.A C Bt / C Be

2 D y .1/ D

5

5e

C Be 5

5t

0

2t

cos t C Be

y D . 2Ae

2t

C Be

2t

.Ae

1/e

2t

4ac < 0

t!1

5

;

y.t / D Ae r1 t C Bt e r2 t :

5.t 1/

.

sin t

/ cos t

4ac < b

therefore r1 and r2 are negative. The general solution is

5

2t

4ac < b 2

Case 2: If D D b 2 4ac D 0 then the two equal roots r1 D r2 D b=.2a/ are negative. The general solution is

8 00 < y C 4y 0 C 5y D 0 y.0/ D 2 : 0 y .0/ D 0 The auxiliary equation for the DE is r 2 C 4r C 5 D 0, which has roots r D 2 ˙ i . Thus y D Ae

b2 p ˙ b2 p b ˙ b2

If t ! 1, then e r1 t ! 0 and e r2 t ! 0. Thus, lim y.t / D 0.

:

5

we have A D 2e and B D 2e . Thus, y D 2e 5 e 5t C 2t e 5 e 5t D 2.t 15.

Since

y.t / D Ae r1 t C Be r2 t :

.A C B/ C Be

5

Given that a > 0, b > 0 and c > 0: Case 1: If D D b 2 4ac > 0 then the two roots are p b ˙ b 2 4ac : r1;2 D 2a

5t

Since 0 D y.1/ D Ae

17.

C 2Be

2t

/ sin t:

Now 2 D y.0/ D A ) A D 2, and 2 D y 0 .0/ D 2A C B ) B D 6. Therefore y D e 2t .2 cos t C 6 sin t /.

If t ! 1, then e r1 t ! 0 and e r2 t ! 0 at a faster rate than Bt ! 1. Thus, lim y.t / D 0. t!1

Case 3: If D D b 2 y D Ae

.b=2a/t

e .1C/t e t lim y .t / D lim !0 !0  e tCh e t D t lim h h!0   d t Dt e D t et dt which is, along with e t , a solution of the CASE II DE y 00 2y 0 C y D 0.

cos.!t / C Be

.b=2a/t

sin.!t /

p 4ac b 2 . If t ! 1, then the amplitude of 2a .b=2a/t both terms Ae ! 0 and Be .b=2a/t ! 0. Thus, lim y.t / D 0. where ! D t!1

18. The auxiliary equation ar 2 C br C c D 0 has roots r1 D

16. The auxiliary equation r 2 .2 C /r C .1 C / factors to .r 1 /.r 1/ D 0 and so has roots r D 1 C  and r D 1. Thus the DE y 00 .2 C /y 0 C .1 C /y D 0 has general solution y D Ae .1C/t C Be t . The function e .1C/t e t is of this form with A D B D 1=. y .t / D  We have, substituting  D h=t ,

4ac < 0 then the general solution is

b

p

2a

D

;

r2 D

p bC D ; 2a

where D D p b 2 4ac. Note that a.r2 r1 / D D D .2ar1 C b/. If y D e r1 t u, then y 0 D e r1 t .u0 Cr1 u/, and y 00 D e r1 t .u00 C2r1 u0 Cr12 u/. Substituting these expressions into the DE ay 00 C by 0 C cy D 0, and simplifying, we obtain e r1 t .au00 C 2ar1 u0 C bu0 / D 0; or, more simply, u00 .r2 r1 /u0 D 0. Putting v D u0 reduces this equation to first order: v 0 D .r2

r1 /v;

which has general solution v D C e .r2 r1 /t : Hence Z u D C e .r2 r1 /t dt D Be .r2 r1 /t C A; and y D e r1 t u D Ae r1 t C Be r2 t .

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101

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ADAMS and ESSEX: CALCULUS 9

by the previous problem. Therefore ay 00 C by 0 C cy D 0 has general solution

19. If y D A cos !t C B sin !t then y 00 C ! 2 y D

A! 2 cos !t

B! 2 sin !t y D Ae k t cos.!t / C Be k t sin.!t /:

2

C ! .A cos !t C B sin !t / D 0

for all t . So y is a solution of (†). 20. If f .t / is any solution of .†/ then f 00 .t / D all t . Thus,

! 2 f .t / for

24.

2  2 i d h 2 ! f .t / C f 0 .t / dt D 2! 2 f .t /f 0 .t / C 2f 0 .t /f 00 .t / D 2! 2 f .t /f 0 .t /

y 0 .0/ D

If g.t / satisfies .†/ and also g.0/ D g 0 .0/ D 0, then by Exercise 20,  2  2 ! 2 g.t / C g 0 .t /  2  2 D ! 2 g.0/ C g 0 .0/ D 0:

25.

Since a sum of squares cannot vanish unless each term vanishes, g.t / D 0 for all t . 22. If f .t / is any solution of .†/, let g.t / D f .t / A cos !t B sin !t where A D f .0/ and B! D f 0 .0/. Then g is also solution of .†/. Also g.0/ D f .0/ A D 0 and g 0 .0/ D f 0 .0/ B! D 0. Thus, g.t / D 0 for all t by Exercise 24, and therefore f .x/ D A cos !t C B sin !t . Thus, it is proved that every solution of .†/ is of this form.

26.

4ac b 2 b and ! 2 D which is 2a 4a2 kt positive for Case III. If y D e u, then

8 00 < y C 100y D 0 y.0/ D 0 : 0 y .0/ D 3 y D A cos.10t / C B sin.10t / A D y.0/ D 0; 10B D y 0 .0/ D 3 3 yD sin.10t / 10     y D A cos !.t c/ C B sin !.t c/

D A cos !t C B sin !t where A D A cos.!c/ B sin.!c/ and B D A sin.!c/ C B cos.!c/ 27.

For y 00 C y D 0, we have y D A sin t C B cos t . Since, y.2/ D 3 D A sin 2 C B cos 2 y 0 .2/ D 4 D A cos 2 B sin 2;

Substituting into ay 00 C by 0 C cy D 0 leads to   0 D e k t au00 C .2ka C b/u0 C .ak 2 C bk C c/u   D e k t au00 C 0 C ..b 2 =.4a/ .b 2 =.2a/ C c/u   D a e k t u00 C ! 2 u : 00

therefore A D 3 sin 2 4 cos 2 B D 4 sin 2 C 3 cos 2: Thus,

2

Thus u satisfies u C ! u D 0, which has general solution u D A cos.!t / C B sin.!t /

102

5 2:

(easy tocalculate y 00 C ! 2 y D 0)  y D A cos.!t / cos.!c/ C sin.!t / sin.!c/   C B sin.!t / cos.!c/ cos.!t / sin.!c/   D A cos.!c/ B sin.!c/ cos !t   C A sin.!c/ C B cos.!c/ sin !t

23. We are given that k D

  y 0 D e k t u0 C ku   y 00 D e k t u00 C 2ku0 C k 2 u :

5)B D

Thus, y D 2 cos 2t 25 sin 2t . circular frequency = ! D 2, frequency = 1 ! D  0:318 2  2 period = D   3:14 !q amplitude = .2/2 C . 52 /2 ' 3:20

2! 2 f .t /f 0 .t / D 0

 2  2 for all t . Thus, ! 2 f .t / C f 0 .t / is constant. (This can be interpreted as a conservation of energy statement.) 21.

Because y 00 C 4y D 0, therefore y D A cos 2t C B sin 2t . Now y.0/ D 2 ) A D 2;

y D .3 sin 2 D 3 cos.t

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4 cos 2/ sin t C .4 sin 2 C 3 cos 2/ cos t 2/ 4 sin.t 2/:

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 3.7 (PAGE 212)

8 < y 00 C ! 2 y D 0 28. y.a/ D A : 0 y .a/ D B   B   y D A cos !.t a/ C sin !.t a/ ! 29. From Example 9, the spring constant is k D 9  104 gm=sec2 . For a frequency of 10 Hz (i.e., a circular frequency ! D 20 rad=sec.), a mass m satisfying p k=m D 20 should be used. So,

32.

y D e k t ŒA cosh !.t t0 /B sinh !.t  A !.t t0 / A !.t t0 / e C e D ek t 2 2  B !.t t0 / B !.t t0 / e C e 2 2 D A1 e .kC!/t C B1 e .k

9  104 k D D 22:8 gm: mD 400 2 400 2

therefore, y D A cos 20 t C B sin 20 t and 1)AD

1 2 1 y 0 .0/ D 2 ) B D D : 20 10

33.

t0 /B sin !.t

t0 /

D e k t ŒA cos !t cos !t0 C A sin !t sin !t0 C B sin !t cos !t0 B cos !t sin !t0  D e k t ŒA1 cos !t C B1 sin !t ;

where A1 D A cos !t0 B sin !t0 and B1 D A sin !t0 C B cos !t0 . Under the conditions of this problem we know that e k t cos !t and e k t sin !t are independent solutions of ay 00 C by 0 C cy D 0, so our function y must also be a solution, and, since it involves two arbitrary constants, it is a general solution.

!/t

8 00 < y C 2y 0 C 5y D 0 y.3/ D 2 : 0 y .3/ D 0

The DE has auxiliary equation r 2 C 2r C 5 D 0 with roots r D 1 ˙ 2i . By the second previous problem, a general solution can be expressed in the form y D e t ŒA cos 2.t 3/ C B sin 2.t 3/ for which

1 Thus, y D cos 20 t C sin 20 t , with y in cm and t 10 in r second, gives the displacement at time t . The amplitude 1 2 is . 1/2 C . /  1:0005 cm. 10 k ! , !2 D (k = spring const, m = mass) 30. Frequency D 2 m Since the spring does not change, ! 2 m D k (constant) For m D 400 gm, ! D 2.24/ (frequency = 24 Hz) 4 2 .24/2 .400/ If m D 900 gm, then ! 2 D 900 2  24  2 D 32. so ! D 3 32 Thus frequency = D 16 Hz 2 4 2 .24/2 400 For m D 100 gm, ! D 100 ! so ! D 96 and frequency = D 48 Hz. 2 31. Using the addition identities for cosine and sine, y D e k t ŒA cos !.t

t0 /

where A1 D .A=2/e !t0 C .B=2/e !t0 and B1 D .A=2/e !t0 .B=2/e !t0 . Under the conditions of this problem we know that Rr D k ˙ ! are the two real roots of the auxiliary equation ar 2 C br C c D 0, so e .k˙!/t are independent solutions of ay 00 C by 0 C cy D 0, and our function y must also be a solution. Since it involves two arbitrary constants, it is a general solution.

The motion is determined by 8 < y 00 C 400 2 y D 0 y.0/ D 1 : 0 y .0/ D 2 y.0/ D

Expanding the hyperbolic functions in terms of exponentials,

y0 D

e t ŒA cos 2.t 3/ C B sin 2.t 3/ C e t Œ 2A sin 2.t 3/ C 2B cos 2.t 3/:

The initial conditions give 2 D y.3/ D e 0

0 D y .3/ D

Thus A D 2e 3 and B D solution

e

A 3

.A C 2B/

A=2 D

y D e 3 t Œ2 cos 2.t

34.

3

3/

e 3 . The IVP has

sin 2.t

3/:

8 00 < y C 4y 0 C 3y D 0 y.3/ D 1 : 0 y .3/ D 0

The DE has auxiliary equation r 2 C 4r C 3 D 0 with roots r D 2 C 1 D 1 and r D 2 1 D 3 (i.e. k ˙ !, where k D 2 and ! D 1). By the second previous problem, a general solution can be expressed in the form y D e 2t ŒA cosh.t 3/ C B sinh.t 3/ for which y0 D

2e

2t

Ce

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ŒA cosh.t

2t

ŒA sinh.t

3/ C B sinh.t

3/ C B cosh.t

3/ 3/:

103

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SECTION 3.7 (PAGE 212)

ADAMS and ESSEX: CALCULUS 9

The initial conditions give 1 D y.3/ D e 0

0 D y .3/ D

6

e

The conditions for stopping the motion are met at t D 2; the mass remains at rest thereafter. Thus 84 1 < 5 cos t C 5 if 0  t   2 1 x.t / D 5 cos t 5 if  < t  2 :1 if t > 2 5

A 6

. 2A C B/

Thus A D e 6 and B D 2A D 2e 6 . The IVP has solution y D e6

2t

Œcosh.t

3/ C 2 sinh.t

3/:

Review Exercises 3 (page 213) 1.

35. Let u.x/ D c Also u0 .x/ D u00 .x/ D

k 2 y.x/. Then u.0/ D c k 2 a. k 2 y 0 .x/, so u0 .0/ D k 2 b. We have k 2 y 00 .x/ D

 k2 c

 k 2 y.x/ D

k 2 u.x/

This IVP for the equation of simple harmonic motion has solution u.x/ D .c

k 2 a/ cos.kx/

xD0

2.

kb sin.kx/

so that  1  y.x/ D 2 c u.x/ k   c D 2 c .c k 2 a/ cos.kx/ C kb sin.kx/ k b c D 2 .1 cos.kx/ C a cos.kx/ C sin.kx/: k k 36. Since x 0 .0/ D 0 and x.0/ D 1 > 1=5, the motion will be governed by x 00 D x C .1=5/ until such time t > 0 when x 0 .t / D 0 again. Let u D x .1=5/. Then u00 D x 00 D .x 1=5/ D u, u.0/ D 4=5, and u0 .0/ D x 0 .0/ D 0. This simple harmonic motion initial-value problem has solution u.t / D .4=5/ cos t . Thus x.t / D .4=5/ cos t C .1=4/ and x 0 .t / D u0 .t / D .4=5/ sin t . These formulas remain valid until t D  when x 0 .t / becomes 0 again. Note that x./ D .4=5/ C .1=5/ D .3=5/.

104

f .x/ D sec2 x tan x ) f 0 .x/ D 2 sec2 x tan2 x C sec4 x > 0 for x in . =2; =2/, so f is increasing and therefore one-to-one and invertible there. The domain of f 1 is . 1; 1/, the range of f . Since f .=4/ D 2, therefore f 1 .2/ D =4, and 1 0

/ .2/ D

.f

3.

lim f .x/ D

x!˙1

4.

5. 6.

lim

1 f 0 .f

x!˙1

x ex2

1 .2//

D

1 1 D : f 0 .=4/ 8

D 0:

2

Observe f 0 .x/ D e x .1 2x 2 / is positive if x 2 < 1=2 2 and ispnegative p if x > 1=2. Thus f is increasing p on 2; 1= 2/ and is decreasing on . 1; 1= 2/ and . 1= p on .1= 2; 1/. p p The maxpand min values p of f are 1= 2e (at x D 1= 2) and 1= 2e (at x D 1= 2). y D e where

x

sin x, .0  x  2/ has a horizontal tangent

dy D e x .cos x sin x/: dx This occurs if tan x D 1, p The pso x D =4 or x D 5=4. points are .=4; e =4 = 2/ and .5=4; e 5=4 = 2/. 0D

7.

Since x./ < .1=5/, the motion for t >  will be governed by x 00 D x .1=5/ until such time t >  when x 0 .t / D 0 again.

Let v D x C .1=5/. Then v 00 D x 00 D .x C 1=5/ D v, v./ D .3=5/ C .1=5/ D .2=5/, and v 0 ./ D x 0 ./ D 0. Thius initial-value problem has solution v.t / D .2=5/ cos.t / D .2=5/ cos t , so that x.t / D .2=5/ cos t .1=5/ and x 0 .t / D .2=5/ sin t . These formulas remain valid for t   until t D 2 when x 0 becomes 0 again. We have x.2/ D .2=5/ .1=5/ D 1=5 and x 0 .2/ D 0.

f .x/ D 3x C x 3 ) f 0 .x/ D 3.1 C x 2 / > 0 for all x, so f is increasing and therefore one-to-one and invertible. Since f .0/ D 0, therefore f 1 .0/ D 0, and ˇ ˇ 1 1 1 d ˇ 1 .f /.x/ˇ D 0 D : D 0 ˇ dx f .f 1 .0// f .0/ 3

If f 0 .x/ D x for all x, then d f .x/ f 0 .x/ xf .x/ D D 0: 2 =2 2 x dx e e x =2 2

Thus f .x/=e x =2 D C (constant) for all x. Since f .2/ D 3, we have C D 3=e 2 and 2 2 f .x/ D .3=e 2 /e x =2 D 3e .x =2/ 2 . 8.

Let the length, radius, and volume of the clay cylinder at time t be `, r, and V , respectively. Then V D  r 2 `, and dr d` dV D 2 r` C r2 : dt dt dt

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INSTRUCTOR’S SOLUTIONS MANUAL

REVIEW EXERCISES 3 (PAGE 213)

Since d V =dt D 0 and d `=dt D k` for some constant k > 0, we have 2 r`

dr D dt

k r 2 `;

)

dr D dt

13.

kr : 2

y D aa C aa .1 C ln a/.x

a) An investment of $P at r% compounded continuously grows to $P e rT =100 in T years. This will be $2P provided e rT =100 D 2, that is, rT D 100 ln 2. If T D 5, then r D 20 ln 2  13:86%.

14.

b) Since the doubling time is T D 100 ln 2=r, we have

If r D 13:863% and r D T 

0:5%, then

100 ln 2 . 0:5/  0:1803 years: 13:8632

The doubling time will increase by about 66 days. ˇ ah 1 a0Ch a0 d x ˇˇ 10. a) lim D lim D a ˇ D ln a. h h dx ˇ h!0 h!0 xD0   Putting h D 1=n, we get lim n a1=n 1 D ln a. n!1

11.

ln 2 ln x D is satisfied if x D 2 or x D 4 (because x 2 ln 4 D 2 ln 2).

1 ln b DmD : b b Thus ln b D 1, and b D e.

15.

b) Using the technique described in the exercise, we calculate   10 210 21=2 1  0:69338183   11 211 21=2 1  0:69326449

Thus ln 2  0:693. 2  2 d  f .x/ D f 0 .x/ dx  2 ) 2f .x/f 0 .x/ D f 0 .x/

a)

b) The line y D mx through the origin intersects the curve y D ln x at .b; ln b/ if m D .ln b/=b. The same line intersects y D ln x at a different point .x; ln x/ if .ln x/=x D m D .ln b/=b. This equation will have only one solution x D b if the line y D mx intersects the curve y D ln x only once, at x D b, that is, if the line is tangent to the curve at x D b. In this case m is the slope of y D ln x at x D b, so

100 ln 2 r: r2

dT T  r D dr

Let the rate be r%. The interest paid by account A is 1; 000.r=100/ D 10r. The interest paid by account B is 1; 000.e r=100 1/. This is $10 more than account A pays, so 1; 000.e r=100

If y D cos

1

x, then x D cos y and 0  y  . Thus

tan y D sgn x

0

Thus cos

sec2

x D tan

y

1

1 D sgn x

p .. 1

1  D x p 2

2

12. If f .x/ D .ln x/=x, then f .x/ D .1 ln x/=x . Thus f 0 .x/ > 0 if ln x < 1 (i.e., x < e) and f 0 .x/ < 0 if ln x > 1 (i.e., x > e). Since f is increasing to the left of e and decreasing to the right, it has a maximum value f .e/ D 1=e at x D e. Thus, if x > 0 and x ¤ e, then 17.

Putting x D  we obtain .ln /= < 1=e. Thus ln. e / D e ln  <  D  ln e D ln e  ; and  e < e  follows because ln is increasing.

1

p

Since cot x D 1= tan x, cot

ln x 1 < : x e

1/ D 10r C 10:

A TI-85 solve routine gives r  13:8165%. 16.

) f 0 .x/ D 0 or f 0 .x/ D 2f .x/: Since f .x/ is given to be nonconstant, we have f 0 .x/ D 2f .x/. Thus f .x/ D f .0/e 2x D e 2x .

a/:

This line passes through the origin if 0 D aa Œ1 a.1 C ln a/, that is, if .1 C ln a/a D 1. Observe that a D 1 solves this equation. Therefore the slope of the line is 11 .1 C ln 1/ D 1, and the line is y D x.

That is, r is decreasing at a rate proportional to itself. 9.

y D x x D e x ln x ) y 0 D x x .1 C ln x/. The tangent to y D x x at x D a has equation

r

1 x2

1D

p

x2

1 x

:

x 2 /=x/. 1

x D tan

1

.1=x/.

1 csc 1 x D sin 1 cos 1 x 1 .1=x/2  tan 1 D 2 1=x p  1 D x 2 1: sgn xtan 2  cos 1 x D sin 1 x. 2 If y D cot

1

x, then x D cot y and 0 < y < =2. Thus

p p csc y D sgn x 1 C cot2 y D sgn x 1 C x 2 sgn x : sin y D p 1 C x2

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105

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REVIEW EXERCISES 3 (PAGE 213)

Thus cot

1

x D sin

1

ADAMS and ESSEX: CALCULUS 9

sgn x p D sgn xsin 1 C x2

1

p

1 1 C x2

:

21.

1 . x 18. Let T .t / be the temperature of the milk t minutes after it is removed from the refrigerator. Let U.t / D T .t / 20. By Newton’s law, csc

1

x D sin

ex > 1 C x C

1

U 0 .t / D kU.t /

g.t / D e t

U.t / D U.0/e k t :

)

kD

If T .s/ D 18, then U.s/ D sk D ln.2=15/, and

1 12

2, so

ln.8=15/: 2D

1.

T .0/ D 96 ) U.0/ D 96

T .20/ D 40 ) U.20/ D 40

ln y D x ln x ln.ln y/ D ln x C ln.ln x/ g.y/ ln.ln y/ x.ln x C ln.ln x// D lim lim x!1 y!1 ln y x ln x   ln.ln x/ : D lim 1 C x!1 ln x

R R ) 60

R D .96

R ) 40

R D .96

R/e 10k R/e 20k :

p Now ln x

0, then c > 0, and f 0 .c/ > 0. If x < 0, then c < 0, and f 0 .c/ < 0. In either case f .x/ D xf 0 .c/ > 0, which is what we were asked to show.

106

g.0/ D g 0 .c/ 0

b) Being increasing on Œe 1 ; 1/, f .x/ D x x is invertible on that interval. Let g D f 1 . If y D x x , then x D g.y/. Note that y ! 1 if and only if x ! 1. We have

U.t / D U.0/e k t :

3600 120R C R2 D 3840 16R D 240 R D 15:

t kC1 .k C 1/Š

a) .d=dx/x x D x x .1 C ln x/ > 0 if ln x > 1, that is, if x > e 1 . Thus x x is increasing on Œe 1 ; 1/.

We have

T .10/ D 60 ) U.10/ D 60



Challenging Problems 3 (page 214)

19. Let R be the temperature of the room, Let T .t / be the temperature of the water t minutes after it is brought into the room. Let U.t / D T .t / R. Then )

t2 2Š

for some c in .0; x/. Since x and g 0 .c/ are both positive, so is g.x/. This completes the induction and shows the desired inequality holds for x > 0 for all positive integers k.

15e sk . Thus

12 D 26:46 min for the milk to

U 0 .t / D kU.t /

t

g.x/ g.x/ D x x

15e 12k

ln.2=15/ ln.2=15/ D 12  38:46: k ln.8=15/

It will take another 38:46 warm up to 18ı .

1

on the interval .0; x/ (where x > 0) to obtain

8 D U.12/ D U.0/e 12k D

e 12k D 8=15;

x2 xk C  C 2Š kŠ

holds for all x > 0. This is certainly true for k D 1, as shown in the previous exercise. Apply the MVT to

Now T .0/ D 5 ) U.0/ D 15 and T .12/ D 12 ) U.12/ D 8. Thus

sD

Suppose that for some positive integer k, the inequality

dv D dt

g

kv.

a) Let u.t / D

g

kv.t /. Then

and

du D dt

k

dv D dt

u.t / D u.0/e k t D .g C kv0 /e k t  1 1 g C u.t / D g .g C kv0 /e v.t / D k k b) lim t!1 v.t / D

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ku,

kt

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INSTRUCTOR’S SOLUTIONS MANUAL

c)

3.

CHALLENGING PROBLEMS 3 (PAGE 214)

dy g g C kv0 k t D v.t / D C e ; y.0/ D y0 dt k k g C kv0 k t gt e CC y.t / D k k2 g C kv0 g C kv0 y0 D 0 C C ) C D y0 C k2 k2  gt g C kv0  kt y.t / D y0 1 e C k k2

dv D dt

g C kv 2 (k > 0)

a) Let u D 2t

p gk. If v.t / D

kv

g 1 eu , then k 1 C eu

g .1 C e u /. e u / .1 k .1 C e u /2 u 4ge D .1 C e u /2   .1 e u /2 gDg 1 .1 C e u /2 4ge u dv D D : .1 C e u /2 dt

dv D dt

2

r

r

e u /e u p 2 gk

4.

  dy dp D e bt by . y, then  dt  dt dp p therefore transforms to The DE D kp 1 dt e bt M

If p D e

bt

  dy p D by C kpe bt 1 dt e bt M  2 ky y D .b C k/y D Ky 1 ; M L bCk M . This is a standard k Logistic equation with solution (as obtained in Section 3.4) given by Ly0 yD ; y0 C .L y0 /e Kt

where K D b C k and L D

where y0 D y.0/ D p.0/ D p0 . Converting this solution back in terms of the function p.t /, we obtain Lp0 e bt p0 C .L p0 /e .bCk/t .b C k/Mp0   D bt p0 ke C .b C k/M kp0 e

p.t / D

p g 1 e 2t gk p . Thus v.t / D k 1 C e 2t gk p r r g e 2t gk 1 g b) lim v.t / D lim p D t!1 t!1 k e 2t gk C 1 k p r g 1 1 C e 2t gk c) If y.t / D y0 C t ln , then k k 2 y.0/ D y0 and p p r 1 2 gke 2t gk dy g D p dt k k 1 C e 2t gk p r g 1 e 2t gk p D v.t /: D k 1 C e 2t gk r

Thus y.t / gives the height of the object at time t during its fall.

: kt

Since p represents a percentage, we must have .b C k/M=k < 100. If k D 10, b D 1, M D 90, and p0 D 1, then bCk M D 99 < 100. The numerator of the final exk pression for p.t / given above is a constant. Therefore p.t / will be largest when the derivative of the denominator,  f .t / D p0 ke bt C .b Ck/M

 kp0 e

kt

D 10e t C980e

10t

is zero. Since f 0 .t / D 10e t 9; 800e 10t , this will happen at t D ln.980/=11. The value of p at this t is approximately 48.1. Thus the maximum percentage of potential clients who will adopt the technology is about 48.1%.

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107

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SECTION 4.1 (PAGE 220)

ADAMS and ESSEX: CALCULUS 9

CHAPTER 4. MORE APPLICATIONS OF DIFFERENTIATION

7.

V D

dV dr 4 3  r , so D 4 r 2 . 3 dt dt

When r D 30 cm and d V =dt D 20 cm3 /s, we have

Section 4.1 Related Rates 1.

(page 220)

20 D 4.30/2

If the side and area of the square at time t are x and A, respectively, then A D x 2 , so dA dx D 2x : dt dt

20 1 dr D D : dt 3600 180 The radius is increasing at 1=.180/ cm/s. 8.

The volume V of the ball is given by

If x D 8 cm and dx=dt D 2 cm/min, then the area is increasing at rate dA=dt D 32 cm2 /min.

4 4 V D r3 D 3 3

2. As in Exercise 1, dA=dt D 2x dx=dt . If dA=dt D 2 ft2 /s and x D 8 ft, then dx=dt D 2=.16/. The side length is decreasing at 1/8 ft/s.

D

D

When D D 6 cm, dD=dt D

4 cm/s, then

A D r ) r D

9.

)

1 p 2 A



dA : dt

dr 1 p . The D dt 10  1 radius is decreasing at the rate p cm/min when the 10  area is 100 cm2 . When

dA D dt

dr D dt

2, and A D 100,

5. For A D  r 2 , we have dA=dt D 2 r dr=dt . If dA=dt D 1=3 km2 /h, p then (a) dr=dt p D 1=.6 r/ km/h, or (b) dr=dt D 1=.6 A=/ D 1=.6 A/ km/h 6. Let the length, width, and area be l, w, and A at time t . Thus A D lw. dw dl dA Dl Cw dt dt dt When l D 16, w D 12,

dl dl ) D dt dt

The length is decreasing at 4 m/s.

108

:5 cm/h. At that time 9 

28:3:

48 D 12

dS dx D 12x : dt dt

If V D 64 cm3 and d V =dt D 2 cm3 /s, then x D 4 cm and dx=dt D 2=.3  16/ D 1=24 cm/s. Therefore, dS=dt D 12.4/.1=24/ D 2. The surface area is increasing at 2 cm2 /s. 10. Let V , r and h denote the volume, radius and height of the cylinder at time t . Thus, V D  r 2 h and dV dr dh D 2 rh C r2 : dt dt dt If V D 60,

dV dr D 2, r D 5, D 1, then dt dt 60 12 V D D  r 2  25 5  dh 1 dr dV D 2 rh dt  r 2 dt dt   1 12 22 D : 2 10 D 25 5 25 hD

dA dw D 3, D 0, we have dt dt

0 D 16  3 C 12

 3 D ; 6

The volume V , surface area S, and edge length x of a cube are related by V D x 3 and S D 6x 2 , so that dx dV D 3x 2 ; dt dt

A 

D

The volume is decreasing at about 28.3 cm3 /h.

4. Let A and r denote the area and radius of the circle. Then r

3

dV  D .36/. 0:5/ D dt 2

dA D 40.4/ D 160. dt The area is increasing at 160 cm2 /s.

2

D 2

dV  dD D D2 : dt 2 dt

dr dA D 2 r : dt dt If r



where D D 2r is the diameter of the ball. We have

3. Let the radius and area of the ripple t seconds after impact be r and A respectively. Then A D  r 2 . We have

dr 20 cm and dt

dr dt

4

The height is decreasing at the rate

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INSTRUCTOR’S SOLUTIONS MANUAL

11.

SECTION 4.1 (PAGE 220)

Let the length, width, depth, and volume at time t be l, w, h and V respectively. Thus V D lwh, and dl dw dh dV D wh C lh C lw : dt dt dt dt If l D 6 cm, w =5cm, h= 4cm, dw D dt

The pdistance from the origin is increasing at a rate of 2= 5.

16.

From the figure, x 2 C k 2 D s 2 . Thus

dl dh D D 1m/s, and dt dt

x

2cm/s, then dV D 20 dt

p When angle P CA D 45ı , x D k and s D 2k. The radar gun indicates p that ds=dt D 100 km/h. Thus dx=dt D 100 2k=k  141. The car is travelling at about 141 km/h.

48 C 30 D 2:

The volume is increasing at a rate of 2 cm3 /s.

A

12. Let the length, width and area at time t be x, y and A respectively. Thus A D xy and k

dA dx D 5, D 10, x D 20, y D 16, then dt dt dy dy 5 D 20 C 16.10/ ) D dt dt

Thus, the width is decreasing at 13. y D x 2 . Thus then 14.

dy D dt

P

Fig. 4.1-16

2 and

dx D dt

3,

4. 3/ D 12. y is increasing at rate 12.

Since x 2 y 3 D 72, then 2xy 3

dx dy dy C 3x 2 y 2 D0) D dt dt dt

2y dx : 3x dt

dx dy 8 D 2, then D . Hence, the dt dt 9 8 vertical velocity is units/s. 9 We have dx dy Cy D1 xy D t ) x dt dt dy dx y D tx 2 ) D x 2 C 2xt dt dt If x D 3, y D 2,

15.

s

31 : 4

31 m/s. 4

dy dx D 2x . If x D dt dt

C x

dA dy dx Dx Cy : dt dt dt If

ds dx Ds : dt dt

17.

We continue the notation of Exercise 16. If dx=dt p D 90 km/h, and p angle P CA D 30ı , p then s D 2k, x D 3k, and ds=dt D . 3k=2k/.90/ D 45 3 D 77:94. The radar gun will read about 78 km/h.

18. Let the distances x and y be as shown at time t . Thus dx dy x 2 C y 2 D 25 and 2x C 2y D 0. dt dt dx 1 4 dy If D and y D 3, then x D 4 and C 3 D 0 so dt 3 3 dt dy 4 D . dt 9 4 m/s. The top of the ladder is slipping down at a rate of 9

At t D 2 we have xy D 2, y D 2x 2 ) 2x 3 D 2 ) x D 1, y D 2. dy dx dx dy Thus C2 D 1, and 1 C 4 D . dt dt dt dt dx dy dx D1) D0) D 1 ). So 1 C 6 dt dt dt p Distance D from origin satisfies D D x 2 C y 2 . So   1 dy dx dD D p C 2y 2x dt dt dt 2 x2 C y2  1  2 D p 1.0/ C 2.1/ D p : 5 5

5 m

y

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x

1/3 m/s

Fig. 4.1-18

109

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SECTION 4.1 (PAGE 220)

ADAMS and ESSEX: CALCULUS 9

We are given that dx=dt D 2 ft/s, so dy=dt D 24=13 ft/s when x D 12 ft. Now the similar triangles in the figure show that s sCy D ; 6 15 so that s D 2y=3. Hence ds=dt D 48=39. The woman’s shadow is changing at rate 48/39 ft/s when she is 12 ft from the point on the path nearest the lamppost.

19. Let x and y be the distances shown in the following figure. From similar triangles: x xCy 2y dx 2 dy D )xD ) D : 2 5 3 dt 3 dt Since

dy D dt

1 , then 2

dx D dt

1 d and .x C y/ D 3 dt

1 2

1 D 3

5 : 6

21.

Hence, the man’s shadow is decreasing at 31 m/s and the shadow of his head is moving towards the lamppost at a rate of 65 m/s.

If dC =dt D 600 when x D 12; 000, then dx=dt D 100. The production is increasing at a rate of 100 tonnes per day. 22.

5 m 2 m y

x2 C D 10; 000 C 3x C 8; 000   x dx dC D 3C : dt 4; 000 dt

Let x, y be distances travelled by A and B from their positions at 1:00 pm in t hours. dx dy Thus D 16 km/h, D 20 km/h. dt dt Let s be the distance between A and B at time t . Thus s 2 D x 2 C .25 C y/2

x

2s

Fig. 4.1-19

ds dx dy D 2x C 2.25 C y/ dt dt dt

 At 1:30 t D 21 we have x D 8, y D 10, p p s D 82 C 352 D 1289 so

20.

p

1289

ds D 8  16 C 35  20 D 828 dt

ds 828 D p  23:06. At 1:30, the ships are sepadt 1289 rating at about 23.06 km/h.

15

and 6

y 5

s

x

A

16 km/h

pos. of

A

at 1:00 p.m.

B

at 1:00 p.m.

x

25 km

s

pos. of

Fig. 4.1-20 y

Refer to the figure. s, y, and x are, respectively, the length of the woman’s shadow, the distances from the woman to the lamppost, and the distances from the woman to the point on the path nearest the lamppost. From one of triangles in the figure we have

If x D 12, then y D 13. Moreover, 2y

110

B

Fig. 4.1-22 23.

y 2 D x 2 C 25:

dy dx D 2x : dt dt

20 km/h

Let  and ! be the angles that the minute hand and hour hand made with the vertical t minutes after 3 o’clock. Then  d D rad=min dt 30 d!  D rad=min: dt 360

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INSTRUCTOR’S SOLUTIONS MANUAL

Since  D 0 and ! D D

 t 30

SECTION 4.1 (PAGE 220)

 at t D 0, therefore 2 and ! D

25.

  tC : 360 2

V D 13  r 2 h D 31 h3 dV dh dh 1 dV D h2 ) D : dt dt dt h2 dt

At the first time after 3 o’clock when the hands of the clock are together, i.e.,  D !,

1 dV 1 dV D and h D 3, then D . Hence, the dt 2 dt 18 1 m/min. height of the pile is increasing at 18 Let r, h, and V be the top radius, depth, and volume of 10 r and the water in the tank at time t . Then D h 8 1 2  25 3 V D r h D h . We have 3 3 16 If

  180  tD tC )t D : ) 30 360 2 11 4 Thus, the hands will be together at 16 11 minutes after 3 o’clock.

Let V , r and h be the volume, radius and height of the cone. Since h D r, therefore

26.

12  !

9

 25 2 dh dh 16 1 : D 3h ) D 10 3 16 dt dt 250h2

3

1 dh D . dt 250 1 m/min when The water level is rising at a rate of 250 depth is 4 m. When h D 4 m, we have

6 Fig. 4.1-23 24.

Let y be the height of balloon t seconds after release. Then y D 5t m. Let  be angle of elevation at B of balloon at time t . Then tan  D y=100. Thus

10 m

r

1 dy 5 1 d D D D sec  dt 100 dt 100 20  d 1 1 C tan2  D dt 20   y 2  d 1 D : 1C 100 dt 20 2

d 1 d 1 . D so D dt 20 dt 100 The angle of elevation of balloon at B is increasing at a 1 rad/s. rate of 100 When y D 200 we have 5

8 m h

Fig. 4.1-26 27.

Let r and h be the radius and height of the water in the tank at time t . By similar triangles, 10 5 r D ) r D h: h 8 4 The volume of water in the tank at time t is V D

1 2 25 3 r h D h : 3 48

Thus, y

dV 25 2 dh dh 16 d V D h ) D : dt 16 dt dt 25h2 dt If

 B

100 m

Fig. 4.1-24

A

h3 and h D 4, then 1000   16 43 9 1 dh D : D dt .25/.4/2 10 1000 6250

dV 1 D dt 10

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SECTION 4.1 (PAGE 220)

ADAMS and ESSEX: CALCULUS 9

9 m/min Hence, the depth of water is increasing at 6250 when the water is 4 m deep. The maximum depth occurs dh when D 0, i.e., dt 16 25h2



1 10

h3 1000



x

10 m/min 30 m

h3 D0 1000 p 3 ) h D 100:

D0)

1 10

Thus, the maximum depth the water in the tank can get is p 3 100  4:64 m.

Fig. 4.1-29 30.

28. Let r, h, and V be the top radius, depth, and volume of the water in the tank at time t . Then

Let P , x, and y be your position, height above centre, and horizontal distance from centre at time t . Let  be the angle shown. Then y D 10 sin  , and x D 10 cos  . We have dy d D 10 cos  ; dt dt

3 1 r D D h 9 3 1  3 V D  r 2h D h 3 27  dh dV D h2 : dt 9 dt If

s

d D 1 rpm D 2 rad/min: dt

6 dy 6 When x D 6, then cos  D , so D 10   12. 10 dt 10 You are rising or falling at a rate of 12 m/min at the time in question.

2 dh D 20 cm/h D m/h when h D 6 m, then dt 10

P

dV  2 4 D  36  D  2:51 m3 /h. dt 9 10 5

10 m

y



Since water is coming in at a rate of 10 m3 /h, it must be leaking out at a rate of 10 2:51  7:49 m3 /h.

C

x

3 m

r

Fig. 4.1-30

9 m

31.

h

Let x and y denote the distances of the two aircraft east and north of the airport respectively at time t as shown in the following diagram. Also let the distance between the two aircraft be s, then s 2 D x 2 C y 2 . Thus, 2s

Fig. 4.1-28 29. Let x and s be the distance as shown. Then s 2 D x 2 C302 and dx ds x dx ds D 2x ) D : 2s dt dt dt s dt When x D 40,

p dx D 10, s D 402 C 302 D 50, then dt

ds 40 D .10/ D 8. Hence, one must let out line at 8 dt 50 m/min.

112

dx dy ds D 2x C 2y : dt dt dt

dx dy D 200 and D 150 when x D 144 and dt p dt 2 y D 60, we have s D 144 C 602 D 156, and Since

1 ds D Œ144. 200/ C 60.150/  dt 156

126:9:

Thus, the distance between the aircraft is decreasing at about 126.9 km/h.

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 4.1 (PAGE 220)

150 km/h

34. s

Let x and y be the distances travelled from the intersection point by the boat and car respectively in t minutes. Then

y

1000 1000 dx D 20  D m/min dt 60 3 dy 1000 4000 D 80  D m/min dt 60 3 The distance s between the boat and car satisfy

x

airport

200 km/h

Fig. 4.1-31

s 2 D x 2 C y 2 C 202 ; 32.

1 0:6 0:4 x y 3 dP 0:6 0:4 0:4 dx 0:4 0:6 D x y C x y dt 3 dt 3 P D

0:6 dy

After one minute, x D Thus

:

dt

1374:5

If dP =dt D 0, x D 40, dx=dt D 1, and y D 10; 000, then dy D dt

6y 0:4 y 0:6 dx D x 0:4 4x 0:6 dt

6y dx D 4x dt

Hence 375:

s

ds dx dy Dx Cy : dt dt dt

4000 1000 ,yD so s  1374: m. 3 3

1000 1000 4000 4000 ds D C  1; 888; 889: dt 3 3 3 3

ds  1374:2 m/min  82:45 km/h after 1 minute. dt

The daily expenses are decreasing at $375 per day. y

20 m

33. Let the position of the ant be .x; y/ and the position of its shadow be .0; s/. By similar triangles,

Car

x s

s

y x

D

y 3

x

)sD

3y 3

:

x

Boat

Then, dy dx C 3y dt dt : .3 x/2

3.3 ds D dt If the ant is at .1; 2/ and 3.2/. ds D dt

x/

1 dy dx D , D dt 3 dt 1 4/

1 , then 4

C 3.2/. 31 / 1 D : 4 8

Hence, the ant’s shadow is moving at along the y-axis.

1 8

units/s upwards

y S

Fig. 4.1-34 35.

Let h and b (measured in metres) be the depth and the surface width of the water in the trough at time t . We have p 2 h D tan 60ı D 3 ) b D p h: 1 . 2 b/ 3 Thus, the volume of the water is   10 1 hb .10/ D p h2 ; V D 2 3 and

y

ant

p dV 20 dh dh 3 dV D p h ) D : dt dt dt 20h dt 3

dV 1 D and h D 0:2 metres, then dt 4 p p   3 3 1 dh D : D dt 20.0:2/ 4 16 p 3 m/min. Hence, the water level is rising at 16 If

x Fig. 4.1-33

3 lamp

x

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113

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SECTION 4.1 (PAGE 220)

ADAMS and ESSEX: CALCULUS 9

ı 60 b=2

10 m

b=2

30 cm

p

y

h ı 30

3 m

32 Cx 2

x s

Fig. 4.1-37

Fig. 4.1-35

a) By similar triangles,

Thus,

36. Let V and h be the volume and depth of water in the pool at time t . If h  2, then x 20 D D 10; h 2

so V D

1D

m/min.

If x D 4 and

2/.

  1 D 5

24 : 125

Hence, the free top end of the ladder is moving vertically downward at 24/125 m/s. 1 160

b) By similar triangles, p Then,

dh dh dV D 80h D 80 . dt dt dt 1 m/min. So surface of water is dropping at a rate of 80

b) If h D 1m, then

1 dx D , then dt 5

dy 30.4/ D dt .9 C 16/3=2

dV dh D 160 . dt dt So surface of water is dropping at a rate of

a) If h D 2:5m, then

dy dx dy dx 30x D D : dt dx dt .9 C x 2 /3=2 dt

1 xh8 D 40h2 : 2

If 2  h  3, then V D 160 C 160.h

y 3 30 D p )yD p : 2 2 10 3 Cx 9 C x2

1D

D

s 10x : )sD p 10 9 C x2

ds ds dx D dt dx dt   p 2x 2 . 9 C x /.10/ .10x/ p 2 9 C x 2 dx D .9 C x 2 / dt 90 dx D : .9 C x 2 /3=2 dt

20 8 3

1

x 32 C x 2

If x D 4 and

x h

1 dx D , then dt 5

ds 90 D dt .9 C 16/3=2

  1 18 : D 5 125

This is the rate of change of the length of the horizontal projection of the ladder. The free top end of the ladder is moving horizontally to the right at rate dx dt

Fig. 4.1-36 38.

37. Let the various distances be as shown in the figure.

114

ds 1 D dt 5

18 7 D m/s: 125 125

Let x, y, and s be distances shown at time t . Then s 2 D x 2 C 16; ds dx s Dx ; dt dt

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s/2 D y 2 C 16 ds dy .15 s/ Dy : dt dt

.15

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 4.1 (PAGE 220)

1 dx D , then s D 5 and When x D 3 and dt 2 p p 2 D y D 102 4 84.  3 1 3 ds D D so Also dt 5 2 10 dy D dt

10 3 p D 84 10

40.

Let y be height of ball t seconds after it drops. dy d 2y D 9:8, j tD0 D 0, yj tD0 D 20, and Thus dt 2 dt

3 p  0:327: 84

Crate B is moving toward Q at a rate of 0.327 m/s.

dy D dt

4:9t 2 C 20;

yD

9:8t:

Let s be distance of shadow of ball from base of pole. s 10 s By similar triangles, D . y 20 200 20s 200 D sy, s D 20 y ds ds dy 20 Dy Cs . dt dt dt

P

4

15 s B

y

a) At t D 1, we have

s x

A

Fig. 4.1-38 39. Let  be the angle of elevation, and x and y the horizontal and vertical distances from the launch site. We have dx dy y x d sec2  D dt 2 dt : dt x

)

At the instant in question

b) As the r ball hits the ground, y Dr0, s D 10, 20 20 dy t D , and D 9:8 , so 4:9 dt 4:9 dy ds D 0 C 10 . 20 dt dt r 20 Now y D 0 implies that t D . Thus 4:9

100 D 2, sec2  D 1 C tan2  D 5, and 50

p p d 1 2 3 1 50.2/ 100.2 3/ D D  dt 5 .50/2 125

r 1 20 .9:8/  2 4:9

ds D dt

9:90:

The shadow is moving at about 9.90 m/s when the ball hits the ground. 10 m

p dx dy D 4 cos 30ı D 2 3; D 4 sin 30ı D 2; dt dt x D 50 km; y D 100 km: Thus tan  D

9:8, y D 15:1,

ds 200 4:9 D . 9:8/. dt 4:9 The shadow is moving at a rate of 81.63 m/s after one second.

Q

y tan  D x

dy D dt

20 y

20 m y

0:0197: 10

s 10 s

Therefore, the angle of elevation is decreasing at about 0.0197 rad/s.

Fig. 4.1-40

4 km/s

ı 30

y

41. Let y.t / be the height of the rocket t seconds after it blasts off. We have



d 2y D 10; dt 2

x

Fig. 4.1-39

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dy DyD0 dt

115

lOMoARcPSD|6566483

SECTION 4.1 (PAGE 220)

ADAMS and ESSEX: CALCULUS 9

at t D 0. Hence y D 5t 2 , (y in metres, t in seconds). Now y d dy=dt tan  D , so sec2  D , and 2000 dt 2000   y 2  d 10t t 1C D D 2000 dt 2000 200 t 1 d D  dt 200 25t 4 1C 20002 t 800t 1 D D :  200 4002 C t 4 t4 1C 4002 At t D 10, we have

d 8000  0:047 rad/s. D dt 4002 C 1002

Starting with x0 D 1:5, get x4 D x5 D 1:73205080757.

9.

g.x/ D x

10. f .x/ D x 3 C 2x 2 2, f 0 .x/ D 3x 2 C 4x. Newton’s formula xnC1 D g.xn /, where

Starting with x0 D 1:5, get x5 D x6 D 0:839286755214. 11.

f .x/ D x 4 8x 2 x C 16, f 0 .x/ D 4x 3 Newton’s formula xnC1 D g.xn /, where g.x/ D x

Fig. 4.1-41

Section 4.2 Finding Roots of Equations (page 230)

x 4 8x 2 x C 16 3x 4 8x 2 16 D : 3 4x 16x 1 4x 3 16x 1

Because f . 3/ D 1, f . 2/ D 3, f . 1/ D 1, f .0/ D 1, f .1/ D 3, there are roots between 3 and 2, between 1 and 0, and between 0 and 1. Starting with x0 D 2:5, get x5 D x6 D 2:87938524157. Starting with x0 D 0:5, get x4 D x5 D 0:652703644666. Starting with x0 D 0:5, get x4 D x5 D 0:532088886328.

2. To solve 1 C 14 sin x D x, start with x0 D 1 and iterate xnC1 D 1 C 41 sin xn . x5 and x6 round to 1.23613. 3. To solve cos.x=3/ D x, start with x0 D 0:9 and iterate xnC1 D cos.xn =3/. x4 and x5 round to 0.95025.

4. To solve .x C 9/1=3 D x, start with x0 D 2 and iterate xnC1 D .xn C 9/1=3 . x4 and x5 round to 2.24004.

13.

f .x/ D sin x 1 C x, f 0 .x/ D cos x C 1. Newton’s formula is xnC1 D g.xn /, where

5. To solve 1=.2 C x 2 / D x, start with x0 D 0:5 and iterate xnC1 D 1=.2 C xn2 /. x6 and x7 round to 0.45340.

6. To solve x 3 C 10x 10 D 0, start with x0 D 1 and iterate 1 3 xn . x7 and x8 round to 0.92170. xnC1 D 1 10 f .x/ D x 2 2, f 0 .x/ D 2x. Newton’s formula xnC1 D g.xn /, where

2x 3 C 3x 2 C 1 x 3 C 3x 2 1 D : 2 3x C 6x 3x 2 C 6x

g.x/ D x

1 xn e starting with x C 0 D 0:3. Both x10 2 round to 0.35173.

g.x/ D x

yD1

8. f .x/ D x 2 3, f 0 .x/ D 2x. Newton’s formula xnC1 D g.xn /, where

116

x

2x

3

x y D sin x

Starting with x0 D 1:5, get x3 D x4 D 1:41421356237.

g.x/ D x

sin x 1 C x : cos x C 1

The graphs of sin x and 1 x suggest a root near x D 0:5. Starting with x0 D 0:5, get x3 D x4 D 0:510973429389. y

x2 2 x2 C 2 D : 2x 2x

2

0.5

1.0

2

D

1.

12. f .x/ D x 3 C 3x 2 1, f 0 .x/ D 3x 2 C 6x. Newton’s formula xnC1 D g.xn /, where

Iterate xnC1 D

g.x/ D x

16x

Starting with x0 D 1:5, get x4 D x5 D 1:64809536561. Starting with x0 D 2:5, get x5 D x6 D 2:35239264766.

2 km

7.

x 3 C 2x 2 2 2x 3 C 2x 2 C 2 D : 2 3x C 4x 3x 2 C 4x

g.x/ D x



and x11

2x 3 C 1 x 3 C 2x 1 D : 2 3x C 2 3x 2 C 2

Starting with x0 D 0:5, get x3 D x4 D 0:45339765152.

y

1.

f .x/ D x 3 C 2x 1, f 0 .x/ D 3x 2 C 2. Newton’s formula xnC1 D g.xn /, where

x C3 : 2x

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Fig. 4.2-13

1.5x

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INSTRUCTOR’S SOLUTIONS MANUAL

14.

SECTION 4.2 (PAGE 230)

f .x/ D x 2 cos x, f 0 .x/ D 2x C sin x. Newton’s formula is xnC1 D g.xn /, where g.x/ D x

has a root near x D 0:6. Use of a solve routine or Newton’s Method gives x D 0:56984029099806.

x 2 cos x : 2x C sin x

sin x . Since jf .x/j  1=.1 C x 2 / ! 0 1 C x2 as x ! ˙1 and f .0/ D 0, the maximum and minimum values of f will occur at the two critical points of f that are closest to the origin on the right and left, respectively. For CP:

18. Let f .x/ D

The graphs of cos x and x 2 , suggest a root near x D ˙0:8. Starting with x0 D 0:8, get x3 D x4 D 0:824132312303. The other root is the negative of this one, because cos x and x 2 are both even functions. y

.1 C x 2 / cos x 2x sin x .1 C x 2 /2 2 0 D .1 C x / cos x 2x sin x

0 D f 0 .x/ D

y D x2

y D cos x 19. -1.5 -1.0 -0.5 0.5 1.0 1.5x Fig. 4.2-14 15.

Since tan x takes all real values between any two consecutive odd multiples of =2, its graph intersects y D x infinitely often. Thus, tan x D x has infinitely many solutions. The one between =2 and 3=2 is close to 3=2, so start with x0 D 4:5. Newton’s formula here is xnC1 D xn

with 0 < x <  for the maximum and  < x < 0 for the minimum. Solving this equation using a solve routine or Newton’s Method starting, say, with x0 D 1:5, we get x D ˙0:79801699184239: The corresponding max and min values of f are ˙0:437414158279. cos x Let f .x/ D . Note that f is an even function, and 1 C x2 that f has maximum value 1 at x D 0. (Clearly f .0/ D 1 and jf .x/j < 1 if x ¤ 0.) The minimum value will occur at the critical points closest to but not equal to 0. For CP: .1 C x 2 /. sin x/ 2x cos x .1 C x 2 /2 2 0 D .1 C x / sin x C 2x cos x: 0 D f 0 .x/ D

The first CP to the right of zero is between =2 and 3=2, so start with x D 2:5, say, and get x D 2:5437321475261. The minimum value is f .x/ D 0:110639672192.

tan xn xn : sec2 xn 1

We get x3 D x4 D 4:49340945791. y

20.

For x 2 D 0 we have xnC1 D xn .xn2 =.2xn // D xn =2. If x0 D 1, then x1 D 1=2, x2 D 1=4, x3 D 1=8. a) xn D 1=2n , by induction.

b) xn approximates the root x D 0 to within 0.0001 provided 2n > 10; 000. We need n  14 to ensure this.

yDx

c) To ensure that xn2 is within 0.0001 of 0 we need .1=2n /2 < 0:0001, that is, 22n > 10; 000. We need n  7.



x y D tan x

21. Fig. 4.2-15

d) Convergence of Newton approximations to the root x D 0 of x 2 D 0 is slower than usual because the derivative 2x of x 2 is zero at the root. p x if x  0 , f .x/ D p x if x < 0  p x/ if x > 0 1=.2 p f 0 .x/ D . 1=.2 x/ if x < 0 The Newton’s Method formula says that

16. A graphing calculator shows that the equation p .1 C x 2 / x

1D0

xnC1 D xn

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f .xn / D xn f 0 .xn /

2xn D

xn :

117

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SECTION 4.2 (PAGE 230)

ADAMS and ESSEX: CALCULUS 9

If x0 D a, then x1 D a, x2 D a, and, in general, xn D . 1/n a. The approximations oscillate back and forth between two numbers. If one observed that successive approximations were oscillating back and forth between two values a and b, one should try their average, .aCb/=2, as a new starting guess. It may even turn out to be the root! 22. Newton’s Method formula for f .x/ D x 1=3 is

Hence

Since the values of xn are assumed to neither converge nor diverge, the exponential factor 2n will dominate for large n 26.

1=3

xn

xnC1 D xn

.1=3/xn

2=3

D xn

3xn D

2xn :

If x0 D 1, then x1 D 2, x2 D 4, x3 D 8, x4 D 16, and, in general, xn D . 2/n . The successive “approximations” oscillate ever more widely, diverging from the root at x D 0.

23. Newton’s Method formula for f .x/ D x 2=3 is xnC1 D xn

.2=3/xn

1=3

3 2 xn

D xn

D

1 2 xn :

27.

If x0 D 1, then x1 D 1=2, x2 D 1=4, x3 D 1=8, x4 D 1=16, and, in general, xn D . 1=2/n . The successive approximations oscillate around the root x D 0, but still converge to it (though more slowly than is usual for Newton’s Method). 24.

Since xnC1 D



xn2 1 2xn

2

D



xn2 C 1 2xn

2

f .v/j  Kju

vj

holds whenever u and v are in Œa; b. Pick any x0 in Œa; b, and let x1 D f .x0 /, x2 D f .x1 /, and, in general, xnC1 D f .xn /. Let r be the fixed point of f in Œa; b found in Exercise 24. Thus f .r/ D r. We have jx1

jx2

:

rj D jf .x0 /

rj D jf .x1 /

f .r/j  Kjx0 f .r/j  Kjx1

rj rj  K 2 jx0

rj;

and, in general, by induction

It follows that ynC1

2 2xn D xn2 C 1 1 yn D 4yn2 D 4yn .1 yn 

jxn

a) Since sin2 .unC1 / D 4 sin2 .un /.1 sin2 .un // D 4 sin2 .un / cos2 .un / D sin2 .2un /; we have unC1 D 2un . Thus unC1 D 2n u0 . It follows that

1 , we have 1 C xn2 dyn D

1.

2.

2xn dxn : .1 C xn2 /2

rj:

Section 4.3 Indeterminate Forms (page 235)

dyn D 2 sin.un / cos.un / 2n du0 : b) Since yn D

rj  K n jx0

Since K < 1, limn!1 K n D 0, so limn!1 xn D r. The iterates converge to the fixed point as claimed in Theorem 6.

yn /:

25. Let yj D sin2 .uj /.

118

We are given that there is a constant K satisfying 0 < K < 1, such that jf .u/

xn2 1 , we have 2xn

2 1 C xnC1 D1C

Let g.x/ D f .x/ x for a  x  b. g is continuous (because f is), and since a  f .x/  b whenever a  x  b (by condition (i)), we know that g.a/  0 and g.b/  0. By the Intermediate-Value Theorem there exists r in Œa; b such that g.r/ D 0, that is, such that f .r/ D r. The fixed point r is unique because if there were two such fixed points, say r1 and r2 , then condition (ii) would imply that jr1 r2 j D jf .r1 / f .r2 /j  Kjr1 r2 j; which is impossible if r1 ¤ r2 and K < 1.

2=3

xn

.1 C xn2 /2 2 sin.un / cos.un / 2n du0 : 2xn

dxn D

  0 0 3 3 D D lim x!0 4 sec2 4x 4   0 ln.2x 3/ lim x!2 x 2 4 0   2 1 2x 3 D : D 2x 2

3x lim x!0 tan 4x

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INSTRUCTOR’S SOLUTIONS MANUAL

  0 sin ax x!0 sin bx 0 a cos ax a D D lim x!0 b cos bx b   1 cos ax 0 4. lim x!0 1 cos bx 0   0 a sin ax D lim x! 0 b sin bx 0 a2 cos ax a2 D lim 2 D 2: x!0 b cos bx b   sin 1 x 0 5. lim x!0 tan 1 x 0 1 C x2 D lim p D1 x!0 1 x2   x 1=3 1 0 lim 2=3 6. x!1 x 0 1 . 13 /x 2=3 1 D lim 2 D : x!1 . /x 1=3 2 3 3.

7.

lim

lim x cot x Œ0  1  x  cos x D lim x!0 sin x   0 x D 1  lim x!0 sin x 0 1 D1 D lim x!0 cos x   0 1 cos x lim x!0 ln.1 C x 2 / 0 sin x  D lim  2x x!0 1 C x2 sin x D lim .1 C x 2 / lim x!0 x!0 2x 1 cos x D : D lim x!0 2 2   sin2 t 0 lim t! t  0 2 sin t cos t D0 D lim t! 1   0 10x e x lim x!0 x 0 10x ln 10 e x D lim D ln 10 1: x!0 1   0 cos 3x lim 2x 0 x!=2  3 sin 3x 3 3 D lim D . 1/ D 2 2 2 x!=2

SECTION 4.3 (PAGE 235)

12.

13.

9.

10.

11.

lim x sin

x!1

1 x

sin D lim

D lim

x!1

14.

15.

16.

17.

Œ1  0 1 x

  0 0

1 x 1 1 cos 2 x x D lim cos 1 D 1: 1 x!1 x x2

x!1

x!0

8.

  0 ln.ex/ 1 x!1 sin x 0 1 1 x D lim D : x!1  cos.x/  lim

  0 sin x x!0 x3 0   0 1 cos x D lim x!0 3x 2 0   sin x 0 D lim x!0 6x 0 1 cos x D : D lim x!0 6 6 lim

x

  sin x 0 tan x 0   0 1 cos x D lim 2 x!0 1 sec x 0 1 cos x 2 D lim .cos x/ 2 x!0 cos x 1 cos x 1 D 1  lim x!0 .cos x 1/.cos x C 1/ 1 D 2

x x!0 x lim

  0 x!0 x4 0   0 2x C 2 sin x D lim 3 x!0 4x 0 1 x sin x D lim 3 2 x!0   x 1 1 1 D (by Exercise 14): D 2 6 12 lim

2

x2

2 cos x

  0 sin2 x lim x!0C tan x x 0   2 sin x cos x 0 D lim x!0C sec2 x 1 0 cos x D1 D 2  1  lim x!0C 2 sec2 x tan x

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119

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SECTION 4.3 (PAGE 235)

18.

19.

20.

21.

  0 ln sin r 0 r!=2 cos r  cos r  sin r D 0: D lim sin r r!=2

25.

lim

2 sin t D  t!=2 t lim

  0 cos 1 x lim x!1 x 1 0   1 p 1 x2 D D lim x!1 1 1

lim x.2 tan

x!1

2 tan

x

/

1

x  1 x!1 x 1 2 . D lim x!1 1 C x 2 x2 2x 2 D 2 D lim x!1 1 C x 2 D lim

lim

22.

t!.=2/

23.

24.

ADAMS and ESSEX: CALCULUS 9

tan t /

.sec t 1

D

t!.=2/

D

t!.=2/

lim

lim



Since

hence

Œ0  1   0 0

1 t



p

lim x

p

x

x!0C

x!0C

p

x ln x

 1 Œ1 1 x!1C x 1 ln x   x ln x x C 1 0 D lim x!1C .x 1/.ln x/ 0   0 ln x D lim 1 x!1C 0 ln x C 1 x 1 x D lim 1 x!1C 1 C 2 x x x 1 D lim D D : x!1C xC1 2 lim



x

1/

ln x x ln x D lim x!0C x 1=2 x!0C   1 x D 0; D lim   1 x!0C x 3=2 2 lim

26.

sin t cos t cos t D 0: sin t

D lim e

120

1:

Œ1   0 0

 1 .1 t!0 t e at   e at 1 0 D lim t!0 t e at 0 ae at D lim at Da t!0 e C at e at lim

2

Let y D .csc x/sin x . Then ln y D sin2 x ln.csc x/ h1i ln.csc x/ lim ln y D lim x!0C x!0C csc2 x 1 csc x cot x csc x D lim x!0C 2 csc2 x cot x 1 D lim D 0: x!0C 2 csc2 x 2 Thus limx!0C .csc x/sin x D e 0 D 1.

D e 0 D 1:

  0 0

27.

  0 3 sin t sin 3t t!0 3 tan t tan 3t 0   3.cos t cos 3t / 0 D lim 2 t!0 3.sec2 t sec 3t / 0 cos t cos 3t D lim t!0 cos2 3t cos2 t 2 cos t cos2 3t cos 3t cos t D lim t!0 cos2 3t cos2 t 1 1 D D lim t!0 cos 3t C cos t 2 lim

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INSTRUCTOR’S SOLUTIONS MANUAL

28.

Let y D



sin x x

1=x 2

SECTION 4.3 (PAGE 235)

32.

:

 sin x   0 x lim ln y D lim x!0 x!0 x2 0  x   x cos x sin x  sin x x2 D lim x!0 2x   0 x cos x sin x D lim x!0 2x 2 sin x 0 x sin x D lim x!0 4x sin x C 2x 2 cos x   0 sin x D lim x!0 4 sin x C 2x cos x 0 cos x 1 D lim D : x!0 6 cos x 2x sin x 6   2 sin x 1=x Thus; lim D e 1=6 : x!0 x ln



x!0

33.

34.

2

29. Let y D .cos 2t /1=t . ln.cos 2t / . We have Then ln y D t2   ln.cos 2t / 0 t!0 t2 0   0 2 tan 2t D lim t!0 2t 0 2 2 sec 2t D lim D 2: t!0 1

lim ln y D lim

t!0

2

Therefore lim t!0 .cos 2t /1=t D e 30.

31.

2

.

h 1i 1 csc x cot x h 1 i D lim 1 x!0C 1 x   x cos x 0 D lim x!0C sin2 x 0   1 D lim cos x lim x!0C x!0C 2 sin x cos x D 1:

csc x lim x!0C ln x

h1i ln sin x lim x!1 csc x 1  cos x sin x D lim x!1  csc x cot x  D lim tan x D 0  x!1

Let y D .1 C tan x/1=x :   0 ln.1 C tan x/ lim ln y D lim x!0 x!0 x 0 sec2 x D lim D 1: x!0 1 C tan x Thus; lim .1 C tan x/1=x D e:

35.

  0 2f .x/ C f .x h/ 2 h 0 h!0   f 0 .x C h/ f 0 .x h/ 0 D lim 2h 0 h!0 f 00 .x C h/ C f 00 .x h/ D lim 2 h!0 2f .x/ 00 D f .x/ D 2 lim

f .x C h/

3f .x C h/ C 3f .x h/ f .x 3h/ h3 h!0 3f 0 .x C 3h/ 3f 0 .x C h/ 3f 0 .x h/ C 3f 0 .x 3h/ D lim 3h2 h!0 3f 00 .x C 3h/ f 00 .x C h/ C f 00 .x h/ 3f 00 .x 3h/ D lim 2h h!0 9f 000 .x C 3h/ f 000 .x C h/ f 000 .x h/ C 9f 000 .x 3h/ D lim 2 h!0 D8f 000 .x/: lim

f .x C 3h/

Suppose that f and g are continuous on Œa; b and differentiable on .a; b/ and g.x/ 6D 0 there. Let a < x < t < b, and apply the Generalized Mean-Value Theorem; there exists c in .x; t / such that

) ) ) ) )

f .x/ f .t / f 0 .c/ D 0 g.x/ g.t / g .c/    f .x/ f .t / g.x/ f 0 .c/ D 0 g.x/ g.x/ g.t / g .c/   f .x/ f .t / f 0 .c/ g.x/ g.t / D 0 g.x/ g.x/ g .c/ g.x/ f 0 .c/ g.t / f 0 .c/ f .t / f .x/ D 0 C g.x/ g .c/ g.x/ g 0 .c/ g.x/ " # f 0 .c/ 1 f .x/ f 0 .c/ D 0 C f .t / g.t / 0 g.x/ g .c/ g.x/ g .c/ " # f .x/ f 0 .c/ 1 f 0 .c/ LD 0 LC f .t / g.t / 0 : g.x/ g .c/ g.x/ g .c/

Since jm C nj  jmj C jnj, therefore, " ˇ ˇ 0 ˇ ˇ 0 ˇ# ˇ ˇ ˇ f .c/ ˇ ˇ f .c/ ˇ ˇ f .x/ 1 ˇ ˇ ˇ ˇ ˇ ˇ ˇ g.x/ Lˇ  ˇ g 0 .c/ Lˇ C jg.x/j jf .t /jCjg.t /jˇ g 0 .c/ ˇ : Copyright © 2018 Pearson Canada Inc. Downloaded by ted cage ([email protected])

121

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SECTION 4.3 (PAGE 235)

ADAMS and ESSEX: CALCULUS 9

Now suppose that  is an arbitrary small positive number. Since limc!aC f 0 .c/=g 0 .c/ D L, and since a < x < c < t , we can choose t sufficiently close to a to ensure that ˇ 0 ˇ f .c/ ˇ ˇ g 0 .c/

In particular,

ˇ ˇ  Lˇˇ < : 2

ˇ 0 ˇ ˇ f .c/ ˇ  ˇ ˇ ˇ g 0 .c/ ˇ < jLj C 2 :

f .x/ D x 5 C x 3 C 2x on .a; b f 0 .x/ D 5x 4 C 3x 2 C 2 > 0 for all x. f has no min value, but has abs max value b 5 C b 3 C 2b at x D b. 1 1 10. f .x/ D . Since f 0 .x/ D < 0 for all x in x 1 .x 1/2 the domain of f , therefore f has no max or min values. 9.

x

12. f .x/ D

x

Since limx!aC jg.x/j D 1, we can choose x between a and t sufficiently close to a to ensure that  1 h  i  jf .t /j C jg.t /j jLj C < : jg.x/j 2 2 It follows that

Thus limx!aC

ˇ ˇ f .x/ ˇ ˇ g.x/

ˇ ˇ   Lˇˇ < C D : 2 2

1.

f .x/ D x C 2 on Œ 1; 1 f 0 .x/ D 1 so f is increasing. f has absolute minimum 1 at x D mum 3 at x D 1.

3. f .x/ D x C 2 on Œ 1; 1/ f has absolute minimum 1 at x D maximum. 4. f .x/ D x 2 1 no max, abs min

1 1 2

on Œ2; 3 1 at x D 3, abs max 1 at x D 2.

Let f .x/ D jx 1j on Œ 2; 2: f . 2/ D 3, f .2/ D 1. f 0 .x/ D sgn .x 1/. No CP; SP x D 1, f .1/ D 0. Max value of f is 3 at x D 2; min value is 0 at x D 1.

14.

Let f .x/ D jx 2 x 2j D j.x 2/.x C 1/j on Œ 3; 3: f . 3/ D 10, f .3/ D 4. f 0 .x/ D .2x 1/sgn .x 2 x 2/. CP x D 1=2; SP x D 1, and x D 2. f .1=2/ D 9=4, f . 1/ D 0, f .2/ D 0. Max value of f is 10 at x D 3; min value is 0 at x D 1 or x D 2. 1 2x f .x/ D 2 , f 0 .x/ D x C1 .x 2 C 1/2 f has abs max value 1 at x D 0; f has no min values.

15. 1 and absolute maxi16.

17. 1 and has no absolute

1

13.

(page 242)

2. f .x/ D x C 2 on . 1; 0 abs max 2 at x D 0, no min.

on .0; 1/ 1 < 0 on .0; 1/ f 0 .x/ D .x 1/2 f has no max or min values.

abs min

f .x/ D L: g.x/

Section 4.4 Extreme Values

1

f .x/ D

11.

f .x/ D .x C 2/.2=3/ no max, abs min 0 at x D f .x/ D .x

2/1=3 , f 0 .x/ D

f has no max or min values.

2/

2=3

>0

1 at x D 0. 2

y D .x

6. f .x/ D x 2 1 on .2; 3/ no max or min values. f .x/ D x 3 C x 4 on Œa; b f 0 .x/ D 3x 2 C 1 > 0 for all x. Therefore f has abs min a3 C a b 3 C b 4 at x D b.

x

2/1=3

Fig. 4.4-17

4 at x D a and abs max

18. f .x/ D x 2 C 2x, f 0 .x/ D 2x C 2 D 2.x C 1/ Critical point: x D 1. f .x/ ! 1 as x ! ˙1.

8. f .x/ D x 3 C x 4 on .a; b/ Since f 0 .x/ D 3x 2 C 1 > 0 for all x, therefore f is increasing. Since .a; b/ is open, f has no max or min values.

122

1 .x 3

y

5. f .x/ D x 2 1 on Œ 2; 3 f has abs min 1 at x D 0, abs max 8 at x D 3, and local max 3 at x D 2.

7.

2.

f0 f

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&

CP 1 j abs min

C %

!x

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 4.4 (PAGE 242)

Hence, f .x/ has no max value, and the abs min is x D 1.

y

1 at

y D .x 2

y

4/2 16

y D x 2 C 2x

x

2

2

x

Fig. 4.4-20 . 1; 1/

21.

Fig. 4.4-18 19. f .x/ D x 3 3x 2 f 0 .x/ D 3x 2 3 D 3.x f0

C %

f

D x 2 .x 1/.5x 3 CP x D 0; ; 1 5

1/.x C 1/

CP 1 j loc max

CP 1 j loc min

&

f .x/ D x 3 .x 1/2 f 0 .x/ D 3x 2 .x 1/2 C 2x 3 .x

C %

f0 !x

f

f has no absolute extrema.

C %

CP 0 j

1/

3/

CP

CP 1 j loc min

3 5

C

j loc max

&





%

C %

!x

f has no absolute extrema. y

y

1 x

3 108 5 ; 55

x

1

y D x3

3x

2

y D x 3 .x

.1; 4/

Fig. 4.4-19

Fig. 4.4-21 22.

20. f .x/ D .x 2 4/2 , f 0 .x/ D 4x.x 2 Critical points: x D 0; ˙2. f .x/ ! 1 as x ! ˙1. f0 f

&

CP 2 j abs min

C %

CP 0 j loc max

1/2

4/ D 4x.x C 2/.x

&

CP C2 j abs min

C %

2/

!x

Hence, f .x/ has abs min 0 at x D ˙2 and loc max 16 at x D 0.

f .x/ D x 2 .x 1/2 , f 0 .x/ D 2x.x 1/2 C 2x 2 .x 1/ D 2x.2x Critical points: x D 0; 21 and 1. f .x/ ! 1 as x ! ˙1. f0 f

&

CP 0 j abs min

CP C %

Hence, f .x/ has loc max x D 0 and x D 1.

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CP 1 j abs min

1 2

j loc max 1 16

&

at x D

1 2

1/.x

C %

1/

!x

and abs min 0 at

123

lOMoARcPSD|6566483

SECTION 4.4 (PAGE 242)

ADAMS and ESSEX: CALCULUS 9

y

y .1;0:5/

yD

. 1; 0:5/

y D x 2 .x

1/2



x2 D1 C1 2x f 0 .x/ D 2 .x C 1/2 f .x/ D

f .x/ D x.x 2 0

f .x/ D .x

D .x

D .x 2

D .x

1/2 C 2x.x 2

2

1/.x

2

1/2x

1/ p 1/.x C 1/. 5x

CP 1 j loc & f % max

CP

p 1/. 5x C 1/

yD

C

x

Fig. 4.4-25 26.

p f .˙1/ D 0, f .˙1= 5/ D ˙16=25 5

x

f .x/ D p

CP 1 j abs min

f0

p

1= 5 p 1= 5

x4 .x 4 C 1/3=2 1

, f 0 .x/ D

x4 C 1 Critical points: x D ˙1. f .x/ ! 0 as x ! ˙1.

y

x

1

&

f

Hence, f has abs max x D 1.

1/2

p1 2

1 x2 x , f 0 .x/ D 2 f .x/ D 2 x C1 .x C 1/2 Critical point: x D ˙1. f .x/ ! 0 as x ! ˙1. f0 f

&

Hence, f has abs max x D 1.

124

1 2

C %



%

27.

CP C1 j abs max

&

at x D 1 and abs min

!x

p

f .x/ D x 2 p f 0 .x/ D 2 x 2 f0

1 2

x2

at f

SP p

2

j loc & max

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&

!x

at x D 1 and abs min y

1 1; p 2

CP C1 j abs max

C

Fig. 4.4-23

CP 1 j abs min

x2 x2 C 1

p1 5

p

24.

!x

yD1

CP 1 C j j j !x loc % loc & loc % max min min

y D x.x 2

%

CP

p1 5

f0 C

C

y

2

1 C 4x /

1/.5x 2

1

&

f

1/2

2

CP 0 j abs min

f0

Fig. 4.4-22 23.

1 0/ x x ln x 1 ln x f 0 .x/ D x 2 D x x2 f .x/ ! 1 as x ! 0C (vertical asymptote), f .x/ ! 0 as x ! 1 (horizontal asymptote). ASY CP f0 0 C e j j !x abs & f % max   1 e; e

x

CP 1= ln 2 j abs max 

yD &

ln x x

!x

Fig. 4.4-35

1 1 ln 2 ; e ln 2

36.

Since f .x/ D jx C 1j,

x

y Dx2

x

Fig. 4.4-33

126

x

f .x/ D

y

x

0

x2

Fig. 4.4-34

Hence,f has abs max 1 at x D 0 and no min value.

33.

.1;1=e/

f 0 .x/ D sgn .x C 1/ D



1; 1;

if x > 1; if x < 1.

1 is a singular point; f has no max but has abs min 0 at x D 1. f .x/ ! 1 as x ! ˙1.

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lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 4.4 (PAGE 242)

y

y

1 

 x

y D jx C 1j

y D sin jxj

1

Fig. 4.4-38

x

39. Fig. 4.4-36 f .x/ D jx 2

37.

1j

f .x/ D 2xsgn .x 2 CP: x D 0 SP: x D ˙1

f f

0

0

&

SP 1 C j abs min %

1/

y D j sin xj

y



CP 0 j loc & max

SP 1 C j !x abs % min



40.

f .x/ D .x 1/2=3 .x C 1/2=3 f 0 .x/ D 32 .x 1/ 1=3 32 .x C 1/ 1=3 Singular point at x D ˙1. For critical points: .x 1/ 1=3 D .x C 1/ 1=3 ) x 1 D x C 1 ) 2 D 0, so there are no critical points.

1j

1

f0

C

f

%

SP 1 j abs max

SP C1 j abs min

&

Hence, f has abs max 22=3 at x D at x D 1. . 1;22=3 /

1

C %

!x

1 and abs min

22=3

y

y D .x

x

1

x

2

Fig. 4.4-39

y

y D jx 2

f .x/ D j sin xj .2n C 1/ CP: x D ˙ , SP D ˙n 2 f has abs max 1 at all CP. f has abs min 0 at all SP.

1/2=3

.x C 1/2=3 x

.1; 22=3 /

Fig. 4.4-37

Fig. 4.4-40

38. f .x/ D sin jxj

3 5  f 0 .x/ D sgn .x/ cos jxj D 0 at x D ˙ ; ˙ ; ˙ ; ::: 2 2 2 0 is a singular point. Since f .x/ is an even function, its graph is symmetric about the origin.

f f

0

&

CP 3 C 2 j abs min %

CP  2 j abs max &

SP 0 C j loc min %

CP  2 j abs & max

CP 3 C 2 j !x abs % min

 Hence, f has abs max 1 at x D ˙.4k C 1/ and abs min 2  1 at x D ˙.4k C 3/ where k D 0, 1, 2, : : : and loc 2 min 0 at x D 0.

p

41. f .x/ D x= x 2 C 1. Since p 0

f .x/ D

42.

2x x p 1 2 x2 C 1 D 2 > 0; x2 C 1 .x C 1/3=2

x2 C 1

for all x, f cannot have any maximum or minimum value. p f .x/ D x= x 4 C 1. f is continuous on R, and limx!˙1 f .x/ D 0. Since f .1/ > 0 and f . 1/ < 0, f must have both maximum and minimum values. p f 0 .x/ D

4x 3 x p 1 x4 2 x4 C 1 D : x4 C 1 .x 4 C 1/3=2

x4 C 1

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127

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SECTION 4.4 (PAGE 242)

ADAMS and ESSEX: CALCULUS 9

p p CP x D ˙1. f .˙1/ p D ˙1= 2. f has max value 1= 2 and min value 1= 2.   y 1 1; p 2

 p

43. f .x/ D x 4 f .˙2/ D 0. f 0 .x/ D

1 1; p 2



yD p

x x4

48.

49.

x

C1

Fig. 4.4-42

x 2 is continuous on Œ 2; 2, and p

4

2.2 x 2 / 2x D p : x2 C x p 2 4 x2 4 x2

p p maximum value 2 CP x Dp˙ 2. f .˙ 2/ D ˙2. f hasp at x D 2 and min value 2 at x D 2. p 2 2 44. f .x/ D x = 4 x is continuous on . 2; 2/, and limx! 2C f .x/ D limx!2 f .x/ D 1. Thus f can have no maximum value, but will have a minimum value. p

2x 4 f 0 .x/ D

x2 4

x2 p 2 4 x2

x2 D

8x x 3 : .4 x 2 /3=2

p p CP x D 0, x D ˙ 8. f .0/ D 0, and ˙ 8 is not in the domain of f . f has minimum value 0 at x D 0. 45. f .x/ D 1=Œx sin x is continuous on .0; /, and limx!0C f .x/ D 1 D limx! f .x/. Thus f can have no maximum value, but will have a minimum value. Since f is differentiable on .0; /, the minimum value must occur at a CP in that interval. 46. f .x/ D .sin x/=x is continuous and differentiable on R except at x D 0 where it is undefined. Since limx!0 f .x/ D 1 (Theorem 8 of Section 2.5), and jf .x/j < 1 for all x ¤ 0 (because j sin xj < jxj), f cannot have a maximum value. Since limx!˙1 f .x/ D 0 and since f .x/ < 0 at some points, f must have a minimum value occurring at a critical point. In fact, since jf .x/j  1=jxj for x ¤ 0 and f is even, the minimum value will occur at the two critical points closest to x D 0. (See Figure 2.20 In Section 2.5 of the text.) 47.

If it exists, an absolute max value is the maximum of the set of all the local max values. Hence, if a function has an absolute max value, it must have one or more local max values. On the other hand, if a function has a local max value, it may or may not have an absolute max value. Since a local max value, say f .x0 / at the point x0 , is defined such that it is the max within some interval jx x0 j < h where h > 0, the function may have greater values, and may even approach 1 outside this interval. There is no absolute max value in this latter case.

128

Section 4.5 Concavity and Inflections (page 246) 1.

2x

No. f .x/ D x 2 has abs max value 0, but g.x/ D jf .x/j D x 2 has no abs max value. ( 1 if x > 0 f .x/ D x sin x 0 if x < 0 jf .x/j  jxj if x > 0 so limx!0C f .x/ D 0 D f .0/. 1 Therefore f is continuous at x D 0. Clearly x sin is x continuous at x > 0. Therefore f is continuous on Œ0; 1/. Given any h > 0 there exists x1 in .0; h/ and x2 in .0; h/ such that f .x1 / > 0 D f .0/ and f .x2 / < 0 D f .0/. Therefore f cannot be a local max or min value at 0. 1 Specifically, let positive integer n satisfy 2n > h 1 1 . and let x1 D  , x2 D 3 2n C 2n C 2 2 Then f .x1 / D x1 > 0 and f .x2 / < 0.

2. 3. 4.

5.

p

1 1 3=2 x x, f 0 .x/ D p , f 00 .x/ D 4 2 x 00 f .x/ < 0 for all x > 0. f is concave down on .0; 1/. f .x/ D

f .x/ D 2x x 2 , f 0 .x/ D 2 2x, f 00 .x/ D Thus, f is concave down on . 1; 1/.

f .x/ D x 2 C 2x C 3, f 0 .x/ D 2x C 2, f 00 .x/ D 2 > 0. f is concave up on . 1; 1/. f .x/ D x x 3 , f 0 .x/ D 1 f 00 .x/ D 6x. f 00

C

f

^

f .x/ D 10x 3

x 3 / D 60x.1

f .x/ D 60.x C

f

^

0 j infl

_

!x

15x 4 ;

00

f 00

3x 2 ,

3x 5 ;

f 0 .x/ D 30x 2

6.

2 < 0.

1 j infl

_

0 j infl

x/.1 C x/: C ^

1 j infl

f .x/ D 10x 3 C 3x 5 , f 0 .x/ D 30x 2 C 15x 4 , f 00 .x/ D 60x C 60x 3 D 60x.1 C x 2 /. f 00 f

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_

0 j infl

C ^

!x

_

!x

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

7.

f .x/ D

13. 2

3

x /D

4x.3

f 00 .x/ D

8.

x 2 /2 ;

f .x/ D .3 0

12x C 4x ;

12 C 12x 2 D 12.x

f 00

C

f

^

f .x/ D .2 C 2x 00

1 j infl

1/.x C 1/:

_

x 2 /2 ;

00

2

C

f 9.

f .x/ D .x 2

f 00 .x/ D 6.x 2 D 6.x C

f

^

_

  .2n 1/ ; n , and conf is concave up on intervals 2   .2n C 1/ n cave down on intervals n; are . Points 2 2 inflection points.

!x

^

x 2 /.2

14.

f .x/ D x 2 sin x, f 0 .x/ D 1 2 cos x, f 00 .x/ D 2 sin x. Inflection points: x D n  for n D 0; ˙1; ˙2;  :::. f is concave down on .2nC1/; .2nC2/ and concave   up on .2n/; .2n C 1/ .

15.

f .x/ D tan

2x/;

2

x /. 2/

C

2 j infl

^

f .x/ D x C sin 2x; f 0 .x/ D 1 C 2 cos 2x; f 00 .x/ D 4 sin 2x:

f 00 .x/ D

!x

1

2

x; f 0 .x/ D

2x . .1 C x 2 /2

4/3 ;

f 0 .x/ D 6x.x 2

f 00

0 j infl

^

C

1 j infl

f 0 .x/ D 2.2 C 2x

f .x/ D 2.2 2x/ C 2.2 C 2x D 12x.x 2/: f

SECTION 4.5 (PAGE 246)

f 00

C

f

^

4/2 ; 4/2 C 24x 2 .x 2 4/.5x

2 j infl _

2

4/ 16.

4/:

p2 5

j infl

C ^

p2 5

j infl _

f 00 f 17.

x 3 x 10. f .x/ D 2 , , f 0 .x/ D 2 x C3 .x C 3/2 2x.x 2 9/ . f 00 .x/ D .x 2 C 3/3

f

11.

_

3 j infl

C ^

0 j infl

_

_

2

f 00

3 j infl

C ^

!x

f .x/ D sin x; f 0 .x/ D cos x; f 00 .x/ D sin x. f is concave down on intervals .2n; .2n C 1// and concave up on intervals ..2n 1/; 2n/, where n ranges over the integers. Points x D n are inflection points.

12. f .x/ D cos 3x, f 0 .x/ D 3 sin 3x, f 00 .x/ D 9 cos 3x.  Inflection points: x D n C 12 for n D 0; ˙1; ˙2; :::. 3   4n C 1 4n C 3 f is concave up on ;  and concave 6  6  4n C 3 4n C 5 ;  . down on 6 6

_

C ^

C

2 j infl

f .x/ D e x ; f 0 .x/ D 2xe 2 f 00 .x/ D e x .4x 2 2/.

f f 00

0 j infl

!x

f .x/ D xe x , f 0 .x/ D e x .1 C x/, f 00 .x/ D e x .2 C x/.

2 C j !x infl ^

2

1 ; 1 C x2

x2

p1 2

j infl

^ ;

p1 2

_

!x

j infl

C ^

!x

2 ln.x 2 / ln.x 2 / , f 0 .x/ D , x x2 2 6 C 2 ln.x / f 00 .x/ D . x3 f has inflection point at x D ˙e 3=2 and f is undefined at x D 0. f is concave up on . e 3=2 ; 0/ and .e 3=2 ; 1/; and concave down on . 1; e 3=2 / and .0; e 3=2 /.

18. f .x/ D

19.

2x ; 1 C x2 2.1 x 2 / .1 C x 2 /.2/ 2x.2x/ D : f 00 .x/ D 2 2 .1 C x / .1 C x 2 /2 f .x/ D ln.1 C x 2 /;

f 00 f

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_

f 0 .x/ D

1 j infl

C ^

1 j infl

_

!x

129

lOMoARcPSD|6566483

SECTION 4.5 (PAGE 246)

20. f .x/ D .ln x/2 , f 0 .x/ D f 00 .x/ D

2.1

2 ln x, x

2 f 00 .x/ D 6x C 3 : x     1 1 00 > 0; f < 0: p f 00 p 4 4 3 3 1 1 Therefore f has a loc min at p and a loc max at p . 4 4 3 3

ln x/ for all x > 0. x2

f 00

x3 3 f 0 .x/ D x 2 f 00 .x/ D 2x

C

0 j

f

21.

ADAMS and ESSEX: CALCULUS 9

e j infl

^

8x C 12; 8 D 2.x 4/: f 00 f

_

29. C

4 j infl

^

!x

22. f .x/ D .x 1/1=3 C .x C 1/1=3 , f 0 .x/ D 31 Œ.x 1/ 2=3 C .x C 1/ 2=3 , f 00 .x/ D 29 Œ.x 1/ 5=3 C .x C 1/ 5=3 . f .x/ D 0 , x 1 D .x C 1/ , x D 0. Thus, f has inflection point at x D 0. f 00 .x/ is undefined at x D ˙1. f is defined at ˙1 and x D ˙1 are also inflection points. f is concave up on . 1; 1/ and .0; 1/; and down on . 1; 0/ and .1; 1/. 23. According to Definition 4.3.1 and the subsequent discussion, f .x/ D ax C b has no concavity and therefore no inflections. 24.

25.

f .x/ D 3x 3 36x 3, f 0 .x/ D 9.x 2 4/, f 00 .x/ D 18x. The critical points are x D 2; f 00 .2/ > 0 ) local min; x D 2; f 00 . 2/ < 0 ) local max: f .x/ D x.x

f 0 .x/ D 3x 2

2/2 C 1 D x 3

8x C 4 D .x 2 CP: x D 2, x D 3

4x 2 C 4x C 1

2/.3x

27.

f .x/ D x 3 C f 0 .x/ D 3x 2

130

8;

f 00 .2/ D 4 > 0;

31.

1 CP: x D ˙ p : 4 3

x 1 x ln 2 , f 0 .x/ D , 2x 2x ln 2.x ln 2 2/ f 00 .x/ D . 2x The critical point is   1 1 ; f 00 < 0 ) local max: xD ln 2 ln 2 x f .x/ D 1 C x2 .1 C x 2 / x2x 1 x2 f 0 .x/ D D .1 C x 2 /2 .1 C x 2 /2 CP: x D ˙1 .1 C x/2 . 2x/ .1 x 2 /2.1 C x 2 /2x f 00 .x/ D .1 C x 2 /4 3 6x C 2x 3 2x 2x 4x C 4x 3 D D 2 3 .1 C x / .1 C x 2 /3 1 1 , f 00 . 1/ D . f 00 .1/ D 2 2 f has a loc max at 1 and a loc min at 1. f .x/ D

f .x/ D xe x , f 0 .x/ D e x .1 C x/, f 00 .x/ D e x .2 C x/. The critical point is x D 1. f 00 . 1/ > 0; ) local min: f .x/ D x ln x; f 0 .x/ D 1 C ln x;

CP: x D

1 e

1 1 ; f 00 . / D e > 0: x e 1 f has a loc min at . e f 00 .x/ D

32.

f 00

1 x

1 3x 4 1 D ; x2 x2

30.

2/

  2 D 4 < 0. 3 Therefore, f has a loc min at x D 2 and a loc max at 2 xD . 3 4 4 , f 00 .x/ D 8x 3 . 26. f .x/ D x C , f 0 .x/ D 1 x x2 The critical points are x D 2; f 00 .2/ > 0 ) local min; x D 2; f 00 . 2/ < 0 ) local max: f 00 .x/ D 6x

28.

25 ; 3

4x 2 C 12x

f .x/ D

!x

_

33.

f .x/ D .x 2 4/2 , f 0 .x/ D 4x 3 16x, f 00 .x/ D 12x 2 16. The critical points are x D 0; f 00 .0/ < 0 ) local max; x D 2; f 00 .2/ > 0 ) local min; x D 2; f 00 . 2/ > 0 ) local min: f .x/ D .x 2 0

4/3 2

f .x/ D 6x.x 4/2 CP: x D 0, x D ˙2 f 00 .x/ D 6.x 2 4/2 C 24x 2 .x 2 2

2

4/

D 6.x 4/.5x 4/ f 00 .0/ > 0; f 00 .˙2/ D 0: f has a loc min at x D 0. Second derivative test yields no direct information about ˙2. However, since f 00 has opposite signs on opposite sides of the points 2 and 2, each of these points is an inflection point of f , and therefore f cannot have a local maximum or minimum value at either.

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lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

34.

f .x/ D .x 2 0

SECTION 4.5 (PAGE 246)

3/e x ;

2

f .x/ D .x C 2x

38. x

3/e D .x C 3/.x

x

1/e ;

f 00 .x/ D .x 2 C 4x 1/e x : The critical points are x D 3; f 00 . 3/ < 0 ) local max; x D 1; f 00 .1/ > 0 ) local min. 35.

2

f .x/ D x e

f 0 .x/ D e

Suppose that f has an inflection point at x0 . To be specific, suppose that f 00 .x/ < 0 on .a; x0 / and f 00 .x/ > 0 on .x0 ; b/ for some numbers a and b satisfying a < x0 < b. If the graph of f has a non-vertical tangent line at x0 , then f 0 .x0 / exists. Let F .x/ D f .x/

2x 2

2x 2

.2x

4x 3 / D 2.x

2x 3 /e

f .x/ D



x2 x2

if x  0 if x < 0,

we have n

2x if x  0 D 2jxj 2x if x < 0 n 2 if x > 0 f 00 .x/ D D 2sgn x: 2 if x < 0 f 0 .x/ D

f 0 .x/ D 0 if x D 0. Thus, x D 0 is a critical point of f . It is also an inflection point since the conditions of Definition 3 are satisfied. f 00 .0/ does not exist. If a the graph of a function has a tangent line, vertical or not, at x0 , and has opposite concavity on opposite sides of x0 , the x0 is an inflection point of f , whether or not f 00 .x0 / even exists. 00

37. Suppose f is concave up (i.e., f .x/ > 0) on an open interval containing x0 . Let h.x/ D f .x/ f .x0 / f 0 .x0 /.x x0 /. Since h0 .x/ D f 0 .x/ f 0 .x0 / D 0 at x D x0 , x D x0 is a CP of h. Now h00 .x/ D f 00 .x/. Since h00 .x0 / > 0, therefore h has a min value at x0 , so h.x/  h.x0 / D 0 for x near x0 . Since h.x/ measures the distance y D f .x/ lies above the tangent line y D f .x0 / C f 0 .x0 /.x x0 / at x, therefore y D f .x/ lies above that tangent line near x0 . Note: we must have h.x/ > 0 for x near x0 , x ¤ x0 , for otherwise there would exist x1 ¤ x0 , x1 near x0 , such that h.x1 / D 0 D h.x0 /. If x1 > x0 , there would therefore exist x2 such that x0 < x2 < x1 and f 0 .x2 / D f 0 .x0 /. Therefore there would exist x3 such that x0 < x3 < x2 and f 0 .x3 / D 0, a contradiction. The same contradiction can be obtained if x1 < x0 .

x0 /:

F .x/ represents the signed vertical distance between the graph of f and its tangent line at x0 . To show that the graph of f crosses its tangent line at x0 , it is sufficient to show that F .x/ has opposite signs on opposite sides of x0 . Observe that F .x0 / D 0, and F 0 .x/ D f 0 .x/ f 0 .x0 /, so that F 0 .x0 / D 0 also. Since F 00 .x/ D f 00 .x/, the assumptions above show that F 0 has a local minimum value at x0 (by the First Derivative Test). Hence F .x/ > 0 if a < x < x0 or x0 < x < b. It follows (by Theorem 6) that F .x/ < 0 if a < x < x0 , and F .x/ > 0 if x0 < x < b. This completes the proof for the case of a nonvertical tangent. If f has a vertical tangent at x0 , then its graph necessarily crosses the tangent (the line x D x0 ) at x0 , since the graph of a function must cross any vertical line through a point of its domain that is not an endpoint.

2x 2

1 CP: x D 0, x D ˙ p 2 2 f 00 .x/ D e 2x .2 20x 2 C 16x 4 /   1 4 < 0: f 00 .0/ > 0; f 00 ˙ p D e 2 Therefore, f has a loc (and abs) min value at 0, and loc 1 (and abs) max values at ˙ p . 2 36. Since

f 0 .x0 /.x

f .x0 /

39.

f .x/ D x n g.x/ D x n D

f .x/;

n D 2; 3; 4; : : :

fn0 .x/ D nx n 1 D 0 at x D 0 If n is even, fn has a loc min, gn has a loc max at x D 0. If n is odd, fn has an inflection at x D 0, and so does gn . 40.

Let there be a function f such that f 0 .x0 / D f 00 .x0 / D ::: D f .k

f

.k/

.x0 / ¤ 0

1/

.x0 / D 0;

for some k  2:

If k is even, then f has a local min value at x D x0 when f .k/ .x0 / > 0, and f has a local max value at x D x0 when f .k/ .x0 / < 0. If k is odd, then f has an inflection point at x D x0 .  1=x 2 if x ¤ 0 41. f .x/ D e 0 if x D 0 a)

lim x

n

x!0C

f .x/ D lim

e

x!0C

D lim y n e y!1

y2

1=x 2

xn

.put y D 1=x/

D 0 by Theorem 5 of Sec. 4.4

Similarly, limx!0 x n f .x/ D 0, and limx!0 x n f .x/ D 0. P b) If P .x/ D jnD0 aj x j then by (a) lim P

x!0

  n X 1 f .x/ D aj lim x x!0 x

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j D0

j

f .x/ D 0:

131

lOMoARcPSD|6566483

SECTION 4.5 (PAGE 246)

ADAMS and ESSEX: CALCULUS 9

c) If x ¤ 0 and P1 .t / D 2t 3 , then f 0 .x/ D

2 e x3

1=x 2

D P1

If x D 0, then

  1 f .x/: x

f .x/ D lim

  1 Assume that f .k/ .x/ D Pk f .x/ for some x k  1, where Pk is a polynomial. Then

      1 1 1 0 1 P f .x/ C P P1 f .x/ k x2 k x x x   1 D PkC1 f .x/; x

where PkC1 .t / D t 2 Pk0 .t / C P1 .t /Pk .t / is a polynomial.   1 f .x/ for n ¤ 0, where By induction, f .n/ D Pn n Pn is a polynomial. f .h/

f .0/ D lim h 1 f .h/ D 0 by h h!0 (a). Suppose that f .k/ .0/ D 0 for some k  1. Then f .kC1/ .0/ D lim

f .k/ .h/

f .k/ .0/

h D lim h 1 f .k/ .h/ h!0   1 f .h/ D 0 D lim h 1 Pk h h!0

1.

by (b). Thus f .n/ .0/ D 0 for n D 1; 2; : : : by induction.

e) Since f 0 .x/ < 0 if x < 0 and f 0 .x/ > 0 if x > 0, therefore f has a local min value at 0 and f has a loc max value there.

Function (d) appears to be the derivative of function (c), and function (b) appears to be the derivative of function (d). Thus graph (c) is the graph of f , (d) is the graph of f 0 , (b) is the graph of f 00 , and (a) must be the graph of the other function g. y y (a) (b)

5 4

3 2 1 1 2 3 4 5

1 x 2 sin ; if x ¤ 0; x 0; if x D 0.

5 4

If x ¤ 0, then 1 1 f 0 .x/ D 2x sin cos x x 2 1 1 cos f 00 .x/ D 2 sin x x x

132

1 2 3

4

x

y

(c)

3 2 11 2 3 4 5

5

4 3 2

(d)

4 3 2 1

42. We are given that f .x/ D

4 3 2 1

4 3 2 1

0

f) If g.x/ D xf .x/ then g .x/ D f .x/ C xf .x/, g 00 .x/ D 2f 0 .x/ C xf 00 .x/. In general, g .n/ .x/ D nf .n 1/ .x/ C xf .n/ .x/ (by induction). Then g .n/ .0/ D 0 for all n (by (d)). Since g.x/ < 0 if x < 0 and g.x/ > 0 if x > 0, g cannot have a max or min value at 0. It must have an inflection point there. (

1 2 3

4

x

5

4 3 2

Fig. 4.6-1

1 1 sin : x2 x

D 0:

Section 4.6 Sketching the Graph of a Function (page 255)

h!0

0

h!0

0

Thus 0 is a critical point of f . There are points x arbitrarily close to 0 where f .x/ > 0, for example 2 x D , and other such points where f .x/ < 0, .4n C 1/ 2 for example x D . Therefore f does not have .4n C 3/ a local max or min at x D 0. Also, there are points arbitrarily close to 0 where f 00 .x/ > 0, for example 1 , and other such points where f 00 .x/ < 0, xD .2n C 1/ 1 for instance x D . Therefore f does not have con2n stant concavity on any interval .0; a/ where a > 0, so 0 is not an inflection point of f either.

f .kC1/ .x/ D

d) f 0 .0/ D limh!0

1 h h

h2 sin

0

2.

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1 1 2 3 4 5

1 2

3 4

x

1 2

3 4

x

y

4 3 2 1

11 2 3 4 5

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

(a)

5 4

(c)

5 4

y

3 2 1 1 2 3 4 5

1 2 3

4

x

y

5

1 2 3

4

x

5

has inflections at 0 and ˙1:7 (approximately).

4 3 2 1

4 3 2

1 1 2 3 4 5

3. 1 2

3 4

x

1 2

3 4

x

y

(d)

4 3 2 1

3 2 11 2 3 4 5

y

(b)

4 3 2 1

SECTION 4.6 (PAGE 255)

4 3 2 1

4 3 2

11 2 3 4 5

f .x/ D x=.1 x 2 / has slope 1 at the origin, so its graph must be (c). g.x/ D x 3 =.1 x 4 / has slope 0 at the origin, but has the same sign at all points as does f .x/, so its graph must be (b). p h.x/ D .x 3 x/= 1 C x 6 has no vertical asymptotes, so its graph must p be (d). k.x/ D x 3 = jx 4 1j is positive for all positive x ¤ 1, so its graph must be (a).

4. (a)

Fig. 4.6-2 The function graphed in Fig. 4.2(a): is odd, is asymptotic to y D 0 at ˙1, is increasing on . 1; 1/ and .1; 1/, is decreasing on . 1; 1/, has CPs at x D 1 (max) and 1 (min), is concave up on . 1; 2/ and .0; 2/ (approximately), is concave down on . 2; 0/ and .2; 1/ (approximately), has inflections at x D ˙2 (approximately). The function graphed in Fig. 4.2(b): is even, is asymptotic to y D 0 at ˙1, is increasing on . 1:7; 0/ and .1:7; 1/ (approximately), is decreasing on . 1; 1:7/ and .0; 1:7/ (approximately), has CPs at x D 0 (max) and ˙1:7 (min) (approximately), is concave up on . 2:5; 1/ and .1; 2:5/ (approximately), is concave down on . 1; 2:5/, . 1; 1/, and .2:5; 1/ (approximately), has inflections at ˙2:5 and ˙1 (approximately). The function graphed in Fig. 4.2(c): is even, is asymptotic to y D 2 at ˙1, is increasing on .0; 1/, is decreasing on . 1; 0/, has a CP at x D 0 (min), is concave up on . 1; 1/ (approximately), is concave down on . 1; 1/ and .1; 1/ (approximately), has inflections at x D ˙1 (approximately). The function graphed in Fig. 4.2(d): is odd, is asymptotic to y D 0 at ˙1, is increasing on . 1; 1/, is decreasing on . 1; 1/ and .1; 1/, has CPs at x D 1 (min) and 1 (max), is concave down on . 1; 1:7/ and .0; 1:7/ (approximately), is concave up on . 1:7; 0/ and .1:7; 1/ (approximately),

5 4

(b)

y

3

2

2

1

1

3 2 1 1

1 2 3

4

x

5

4 3 2

5 4

1 1

2

2

3

3

y

(d)

3

3 4

x

1 2

3 4

x

y 3

2

2

1

1

3 2 1 1

1 2

4

4

(c)

y

3

1 2 3

4

x

5

4 3 2

1 1

2

2

3

3

4

4

Fig. 4.6-4 The function graphed in Fig. 4.4(a): is odd, is asymptotic to x D ˙1 and y D x, is increasing on . 1; 1:5/, . 1; 1/, and .1:5; 1/ (approximately), is decreasing on . 1:5; 1/ and .1; 1:5/ (approximately), has CPs at x D 1:5, x D 0, and x D 1:5, is concave up on .0; 1/ and .1; 1/, is concave down on . 1; 1/ and . 1; 0/, has an inflection at x D 0. The function graphed in Fig. 4.4(b): is odd, is asymptotic to x D ˙1 and y D 0, is increasing on . 1; 1/, . 1; 1/, and .1; 1/, has a CP at x D 0, is concave up on . 1; 1/ and .0; 1/, is concave down on . 1; 0/ and .1; 1/, has an inflection at x D 0. The function graphed in Fig. 4.4(c): is odd, is asymptotic to x D ˙1 and y D 0, is increasing on . 1; 1/, . 1; 1/, and .1; 1/, has no CP, is concave up on . 1; 1/ and .0; 1/, is concave down on . 1; 0/ and .1; 1/, has an inflection at x D 0.

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133

lOMoARcPSD|6566483

SECTION 4.6 (PAGE 255)

ADAMS and ESSEX: CALCULUS 9

y

The function graphed in Fig. 4.4(d): is odd, is asymptotic to y D ˙2, is increasing on . 1; 0:7/ and .0:7; 1/ (approximately), is decreasing on . 0:7; 0:7/ (approximately), has CPs at x D ˙0:7 (approximately), is concave up on . 1; 1/ and .0; 1/ (approximately), is concave down on . 1; 0/ and .1; 1/ (approximately), has an inflection at x D 0 and x D ˙1 (approximately). 5. f .0/ D 1 f .˙1/ D 0 f .2/ D 1 limx!1 f .x/ D 2, limx! 1 f .x/ D f0

SP 0 j loc max

C %

f

CP 1 j loc min

&

y D f .x/

2 .1;1/

.3;1/ 1 2

x

1

C %

yDx 1

!x

Fig. 4.6-6 00

f f

C

C

0 j

^

2 j infl

^

_

!x

0 must be a SP because f 00 > 0 on both sides and it is a loc max. 1 must be a CP because f 00 is defined there so f 0 must be too. y yD2

y D f .x/

1 .2;1/ 1

7. x

1

y D .x 2

y D 6x.x

yD 1 00

f

%

SP 1 j

C %

CP 0 j loc max

CP 2 j loc min

&

C %

C

f

^

Since

lim

x!˙1

1 j infl

 f .x/ C 1

oblique asymptote.

134

_

1 j infl

1/2 1/2 .x C 1/2

1/2 C 4x 2 .x 2

1/

2

D 6.x 1/.5x 1/ p p D 6.x 1/.x C 1/. 5x 1/. 5x C 1/ From y: Asymptotes: none. Symmetry: even. Intercepts: x D ˙1. From y 0 : CP: x D 0, x D ˙1. SP: none.

y0 !x

Inflection points: x D 1; 1; 3. f0

2

2

6. According to the given properties: Oblique asymptote: y D x 1. Critical points: x D 0; 2. Singular point: x D 1. Local max 2 at x D 0; local min 0 at x D 2. C

2

D 6x.x

y D 6Œ.x

Fig. 4.6-5

f0

1/3

0

y &

CP 1 j

CP CP 0 C 1 C j j !x abs % & min %

1 From y 00 : y 00 D 0 at x D ˙1, x D ˙ p . 5 C ^

3 j infl

_

 x D 0, the line y D x

!x 1 is an

y 00 C

1 j y ^ infl _

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p1 5

j infl

C

p1 5

1 C j j !x ^ infl _ infl ^

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 4.6 (PAGE 255)

y

9. y D .x 2

1/3

4 2 2 2 x ; y 00 D 3 : D 1; y 0 D yD x x x2 x From y: Asymptotes: x D 0, y D 1. Symmetry: none obvious. Intercept: .2; 0/. Points: . 1; 3/. From y 0 : CP: none. SP: none.

1

x

1

&

y

Fig. 4.6-7 y 00 2

0

2

2

00

2

8. y D x.x 1/ , y D .x 1/.5x 1/, y D 4x.5x 3/. From y: Intercepts: .0; 0/, .1; 0/. Symmetry: odd (i.e., about the origin). 1 From y 0 : Critical point: x D ˙1; ˙ p . 5 CP y0

C

CP 1 C p 5 j loc % min

1 j loc & max

y %

CP 1 p 5 j loc max &

y

y 00 y

_

3 5

j infl

C

^ yD

!x 2

x x

C

1

.2;0/ x

j !x loc % min

1

. 1; 3/

0 j infl

^

C

CP

3 . 5

q

_

ASY 0 j

y

From y 00 : q Inflection points at

x D 0; ˙

!x

&

From y 00 : y 00 D 0 nowhere.

1

2

ASY 0 j

y0

p 1= 5

p 1= 5

_

q

3 5

j infl

C ^

Fig. 4.6-9 !x 4 2 2 x 1 , y 00 D . D1 , y0 D xC1 xC1 .x C 1/2 .x C 1/3 From y: Intercepts: .0; 1/, .1; 0/. Asymptotes: y D 1 (horizontal), x D 1 (vertical). No obvious symmetry. Other points: . 2; 3/. From y 0 : No critical point.

10. y D

y

p1 5

q

3 1 5

y0

C

y

%

x

ASY 1 j

C %

!x

From y 00 : No inflection point. y D x.x

2

2

1/

Fig. 4.6-8

y 00

C

y

^

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ASY 1 j

_

!x

135

lOMoARcPSD|6566483

SECTION 4.6 (PAGE 255)

ADAMS and ESSEX: CALCULUS 9

y

yD

y

x3 1Cx

yD

x 1 xC1



. 2;3/ yD1



xD 1

x

1 xD 1

3 27 2; 4

x

1

Fig. 4.6-11 1 2x 6x 2 8 , y0 D , y 00 D . 2 2 2 4Cx .4 C x / .4 C x 2 /3 From y: Intercept: .0; 14 /. Asymptotes: y D 0 (horizontal). Symmetry: even (about y-axis). From y 0 : Critical point: x D 0.

12. y D

Fig. 4.6-10

CP 0 j abs y % max 2 00 00 From y : y D 0 at x D ˙ p . 3 y0

3

11.

x 1Cx 3x 2 C 2x 3 .1 C x/3x 2 x 3 D y0 D 2 .1 C x/ .1 C x/2 2 2 .1 C x/ .6x C 6x / .3x 2 C 2x 3 /2.1 C x/ y 00 D .1 C x/4 2 2 6x.1 C x/ 6x 4x 3 6x C 6x 2 C 2x 3 D D .1 C x/3 .1 C x/3 2x.3 C 3x C x 2 / D .1 C x/3 From y: Asymptotes: x D 1. Symmetry: none. Intercepts .0; 0/. Points . 3=2; 27=4/. 3 . From y 0 CP: x D 0, x D 2 yD

CP 3 2

y0 y

j loc min

&

C %

ASY 1 j

C %

CP 0 j

%

!x

From y 00 : y 00 D 0 only at x D 0.

y

00

y

136

C ^

ASY 1 j

_

0 j infl

C ^

y 00

C

y

^

_

2 p 3 j infl

C ^

1=4

yD p2 3

!x

1 4 C x2

p2 3

x

Fig. 4.6-12 2x ; y0 D x2 .2 x 2 /2 2 8x 2 4 C 6x 2 y 00 D C D 2 2 2 3 .2 x / .2 x / .2 px 2 /3 From y: Asymptotes: y D 0, x D ˙ 2. Symmetry: even. Intercepts .0; 12 /. Points .˙2; 21 /. From y 0 : CP x D 0. yD

1

2

y 00 !x

2 p 3 j infl

&

!x

y

13. C

C

y

&

ASY p 2 j

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&

CP 0 C j loc min %

ASY p 2 j

C !x

%

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 4.6 (PAGE 255)

y

y 00 W y 00 D 0 nowhere. ASY p 2 j

y 00 y

_

C ^

_

p

x2



xD 1

!x

2 2; 3



y

xD

x

yD

ASY p 2 j

2 2; 3



1  x

xD1

p xD 2

2 1=2

x



1 2; 2





1 2; 2

yD

Fig. 4.6-14



15.

1 x2

2

Fig. 4.6-13

x2

1 D1C 2 1 x 1 2x 0 y D 2 .x 1/2 2 2.3x 2 C 1/ .x 1/2 x2.x 2 1/2x D y 00 D 2 2 4 .x 1/ .x 2 1/3 From y: Asymptotes: y D 1, x  D ˙1. Symmetry: even. 4 Intercepts .0; 0/. Points ˙2; . 3 0 From y : CP x D 0. yD

x2

y0 y 14.

2x.x 2 C 3/ x2 C 1 , y 00 D . 2 2 1 .x 1/ .x 2 1/3 From y: Intercept: .0; 0/. Asymptotes: y D 0 (horizontal), x D ˙1 (vertical). Symmetry: odd. Other points: .2; 23 /, . 2; 23 /. From y 0 : No critical or singular points. yD

x

x2

, y0 D

00

C %

ASY 1 j

CP 0 j loc & max

C %

y0 y

&

&

ASY 1 j

&

&

!x

00

From y : y D 0 nowhere. y 00

C

y

^

ASY 1 j

_

ASY 1 j

y

ASY 1 j

ASY 1 j

!x



4 2; 3



C ^

yD 

!x x2

x2

4 2; 3

1



yD1

From y 00 : y 00 D 0 at x D 0.

y 00 y

_

ASY 1 j

C ^

x xD 1

0 j infl _

ASY 1 j

C ^

!x

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xD1

Fig. 4.6-15

137

lOMoARcPSD|6566483

SECTION 4.6 (PAGE 255)

x3

ADAMS and ESSEX: CALCULUS 9

x 2 .x 2 3/ 00 2x.x 2 C 3/ ,y D . 2 2 1 .x 1/ .x 2 1/3 From y: Intercept: .0; 0/. Asymptotes: x D ˙1 (vertical), y D p x (oblique). Symmetry: odd. Other points:   p 3 3 . ˙ 3; ˙ 2 p From y 0 : Critical point: x D 0; ˙ 3.

16. y D

x2

, y0 D

CP ASY CP ASY CP p p 3 1 0 1 3 C j j j j j !x loc loc y % max & & & & min %

From y 0 : CP: x D 0. C

y

%

CP 0 j

y 00 y

p

C

j infl

^

_

00

y

_

ASY 1 j

C ^

!x

%

0 C j infl ^

3

From y : y D 0 at x D 0. y 00

C

p From y 00 : y 00 D 0 at x D 0, x D ˙ 3.

y0 C

00

y0

p

3 j !x infl _

y

0 j infl

ASY 1 j

_

C ^

!x

yD p

3;

y



yDx

p

3;

p  3 3 4

x3 C1

x2

p  3 3 4

x

xD 1 yDx p

3 p 3

x

Fig. 4.6-17 xD1

yD

x2 2x 2.1 3x 2 / , y0 D 2 , y 00 D . 2 C1 .x C 1/ .x 2 C 1/3 From y: Intercept: .0; 0/. Asymptotes: y D 1 (horizontal). Symmetry: even. From y 0 : Critical point: x D 0.

x3 x2

18. y D

1 Fig. 4.6-16

17.

x3 C x x x x3 D Dx 2 2 C1 x C1 x C1 x 4 C 3x 2 x 2 .x 2 C 3/ .x 2 C 1/3x 2 x 3 2x 0 D 2 D y D 2 2 2 .x C 1/ .x C 1/ .x 2 C 1/2 2 2 3 4 2 2 .x C 1/ .4x C 6x/ .x C 3x /2.x C 1/2x y 00 D .x 2 C 1/4 5 3 4x C 10x C 6x 4x 5 12x 3 D .x 2 C 1/3 2x.3 x 2 / D .x 2 C 1/3 From y: Asymptotes: y D x (oblique). Symmetry: odd. Intercepts p .0; 0/. p Points .˙ 3; ˙ 34 3/. yD

138

x2

x2

CP 0 j abs min

y0 &

y

C %

!x

1 From y 00 : y 00 D 0 at x D ˙ p . 3

y 00 y

_

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1 p 3 j infl

C ^

1 p 3 j infl

_

!x

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 4.6 (PAGE 255)

y

20.

yD1

x2 C1

yD p1 3

x2

p1 3

x

x2 2 0 2x 2.3x 2 C 1/ ,y D 2 , y 00 D . 2 2 x 1 .x 1/ p .x 2 1/3 From y: Intercept: .0; 2/, .˙ 2; 0/. Asymptotes: y D 1 (horizontal), x D ˙1 (vertical). Symmetry: even. From y 0 : Critical point: x D 0.

yD

Fig. 4.6-18

f0 &

f

x 4 3 Dx 1 xC1 xC1 .x C 1/2 C 3 3 D y0 D 1 C 2 .x C 1/ .x C 1/2 6 y 00 D .x C 1/3 From y: Asymptotes: y D x 1 (oblique), x D Symmetry: none. Intercepts .0; 4/, .˙2; 0/. From y 0 : CP: none.

&

CP 0 C j loc min %

yD

y0 y

_

ASY 1 j

C ^

C

y

%

ASY 1 j

ASY 1 j

%

!x

p

C

y

^

_

!x

x

2

yD ASY 1 j

_

yD1 p

2

From y 00 : y 00 D 0 nowhere. y 00

%

!x

xD1

2

C

C

y

1.

xD 1

y0

ASY 1 j

From y 00 : y 00 D 0 nowhere.

2

19.

ASY 1 j

x2 x2

2 1

!x Fig. 4.6-20

y

21.

2

1

yDx 1

Fig. 4.6-19

2

4

x2 4 yD xC1

x

x 3 4x x.x 2/.x C 2/ D x2 1 x2 1 2 2 .x 1/.3x 4/ .x 3 4x/2x y0 D 2 2 .x 1/ 3x 4 7x 2 C 4 2x 4 C 8x 2 D .x 2 1/2 x4 C x2 C 4 D .x 2 1/2 .x 2 1/2 .4x 3 C 2x/ .x 4 C x 2 C 4/2.x 2 y 00 D .x 2 1/4 5 3 4x 2x 2x 4x 5 4x 3 16x D .x 2 1/3 6x 3 18x x2 C 3 D D 6x 2 2 3 .x 1/ .x 1/3 From y: Asymptotes: y D x (oblique), x D ˙1. Symmetry: odd. Intercepts .0; 0/, .˙2; 0/. yD

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1/2x

139

lOMoARcPSD|6566483

SECTION 4.6 (PAGE 255)

ADAMS and ESSEX: CALCULUS 9

y

From y 0 : CP: none.

y0

C

y

%

yD1

ASY 1 j

C %

ASY 1 j

C %

1

y

^

ASY 1 j

0 C j _ infl ^

ASY 1 j

x

!x yD

From y 00 : y 00 D 0 at x D 0.

y 00 C

1

x2 1 x2

!x _ Fig. 4.6-22

y xD1 xD 1

2

x

2

23.

yDx

yD

x 3 4x x2 1

Fig. 4.6-21

1 2 6 x2 1 D1 , y 0 D 3 , y 00 D . x2 x2 x x4 From y: Intercepts: .˙1; 0/. Asymptotes: y D 1 (horizontal), x D 0 (vertical). Symmetry: even. From y 0 : No critical points.

22. y D

y0 C y %

y0 y

&

ASY 0 j

From y 00 : y 00 is negative for all x.

140

C %

x5

2x 3 x .x 2 1/2 2 2 4 5 .x 1/ 5x x 2.x 2 1/2x y0 D 2 .x 1/4 6 4 6 5x 5x 4x x 4 .x 2 5/ D D .x 2 1/3 .x 2 1/3 2 3 5 3 .x 1/ .6x 20x / .x 6 5x 4 /3.x 2 1/2 2x y 00 D .x 2 1/6 7 5 3 6x 26x C 20x 6x 7 C 30x 5 D 2 4 .x 1/ 4x 3 .x 2 C 5/ D .x 2 1/4 From y: Asymptotes: y D x, x D ˙1. Symmetry: odd.  p 25 p 5 . Intercepts .0; 0/. Points ˙ 5; ˙ 16 p From y 0 : CP x D 0, x D ˙ 5. yD

.x 2

DxC

1/2

CP ASY CP ASY CP p p 5 1 C 0 C 1 5 C j j j j j loc loc % % & max & min From y 00 : y 00 D 0 if x D 0.

!x y 00 y

_

ASY 1 j

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_

0 C j infl ^

ASY 1 j

C ^

!x

!x

%

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 4.6 (PAGE 255)

y

yDx

p

5

1

p 5

1

x

x5

yD

.x 2

1/2

Fig. 4.6-23 24.

yD 00

x/2

.2

x3 2

y D

2.x

2/.x 6/ , x4 p 2.x 6 C 2 3/.x 12x C 24/ D x5 x5

, y0 D

.x

6

p 2 3/

From y: Intercept: .2; 0/. Asymptotes: y D 0 (horizontal), x D 0 (vertical). Symmetry: none obvious. Other points: . 2; 2/, . 10; 0:144/. From y 0 : Critical points: x D 2; 6. ASY 0 j

CP 2 C j loc % y & & min p From y 00 : y 00 D 0 at x D 6 ˙ 2 3. y0

y 00 y

_

0 j

C ^

p 6C2 3 j infl _

CP 6 j loc max

6

.

1

1 D 4x x.x 2/.x C 2/ 3x 2 4 3x 2 4 D y0 D .x 3 4x/2 x 2 .x 2 4/2 3 2 .x 4x/ .6x/ .3x 2 4/2.x 3 4x/.3x 2 4/ y 00 D .x 3 4x/4 4 2 4 6x 24x 18x C 48x 2 32 D 3 .x 4x/3 2 2 12.x 1/ C 20 D x 3 .x 2 4/3 From y: Asymptotes: y D 0, x D 0; 2; 2. Symmetry:    odd. No intercepts.  16 1 2 Points: ˙ p ; ˙ p , ˙3; ˙ 15 3 3 3 2 0 From y : CP: x D ˙ p . 3 ASY CP ASY CP ASY p2 y0 2 C 0 C p2 2 3 3 j j j j j !x loc % loc & y & & min % max & From y 00 : y 00 D 0 nowhere. 25.

yD

x3

ASY ASY ASY 2 C 0 2 C j j j !x y _ ^ _ ^

y 00

y

&

!x yD

p 2 3 C j !x infl ^

1 x3

4x

3

xD2 p2 3 3

p2 3 xD 2

x

y

yD

x/2

.2

x3

.6;2=27/

2 . 10; 0:144/

p 6C2 3 p 6 2 3

Fig. 4.6-25 x

26.

x x yD 2 D , x Cx 2 .2 C x/.x 1/ 2 .x C 2/ 2.x 3 C 6x C 2/ 00 y0 D , y D . .x C 2/2 .x 1/2 .x C 2/3 .x 1/3 From y: Intercepts: .0; 0/. Asymptotes: y D 0 (horizontal), x D 1, x D 2 (vertical). Other points: . 3; 34 /, .2; 12 /. From y 0 : No critical point. y0

Fig. 4.6-24

y

&

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ASY 2 j

&

ASY 1 j

&

!x

141

lOMoARcPSD|6566483

SECTION 4.6 (PAGE 255)

ADAMS and ESSEX: CALCULUS 9

y

From y 00 : y 00 D 0 if f .x/ D x 3 C 6x C 2 D 0. Since f 0 .x/ D 3x 2 C 6  6, f is increasing and can only have one root. Since f .0/ D 2 and f . 1/ D 5, that root must be between 1 and 0. Let the root be r.

y 00 y

_

ASY 2 j

C ^

r j infl _

ASY 1 j

yD

. 1;3/

x3

3x 2 C 1 x3

yD1

C ^

!x

x .1; 1/

y

yD

xD 2

x x2 C x

Fig. 4.6-27 2 28.

.2;1=2/ x

r . 3; 3=4/

xD1

y D x C sin x, y 0 D 1 C cos x, y 00 D sin x. From y: Intercept: .0; 0/. Other points: .k; k/, where k is an integer. Symmetry: odd. From y 0 : Critical point: x D .2k C 1/, where k is an integer.

f0

C

f

%

Fig. 4.6-26

CP  j

CP  j

C %

%

CP 3 j

C %

!x

From y 00 : y 00 D 0 at x D k, where k is an integer. 27.

3x 2 C 1 1 3 C 3 D1 x3 x x 3 3 3.x 2 1/ y0 D 2 D 4 x x x4 12 2 x2 6 C 5 D6 y 00 D 3 5 x x x From y W Asymptotes: y D 1, x D 0. Symmetry: none. Intercepts: since limx!0C y D 1, and limx!0 y D 1, there are intercepts between 1 and 0, between 0 and 1, and between 2 and 3. 1 Points: . 1; 3/, .1; 1/, .2; 38 /, .3; /. 27 From y 0 : CP: x D ˙1. yD

x3

CP ASY y0 C 1 0 j j loc y % max & & p From y 00 : y 00 D 0 at x D ˙ 2. y 00 C y ^

142

p

2

j infl

y 00 C y ^

2  C 0  C 2 j j j j j !x infl _ infl ^ infl _ infl ^ infl _ y

2

ASY p 0 C 2 j j !x _ ^ infl _

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y D x C sin x



CP 1 C j !x loc % min



Fig. 4.6-28

2

x

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

29. y D x C 2 sin x; y D 0 if x D 0

y 0 D 1 C 2 cos x;

SECTION 4.6 (PAGE 255)

y 00 D

1 From y 00 : y 00 D 0 at x D ˙ p . 2

2 sin x:

1 2 , i.e., x D ˙ ˙ 2n 2 3 y 00 D 0 if x D ˙n From y:Asymptotes: (none). odd.  Symmetry:   p p 2 8 2 8 Points: ˙ ; ˙ C 3 , ˙ ;˙ C 3 , 3 3 3 3  4 p 4 ˙ ;˙ 3 . 3 3 2 ˙ 2n. From y 0 : CP: x D ˙ 3 y 0 D 0 if x D

CP y0 y &

CP

8 3

4 3

C

j loc % min 00

CP 2 3

C

j loc & max

C

j loc % min

CP

CP

2 3

4 3

j loc & max

y

^

1 p 2 j infl

31.

CP 1 j abs min 2.

y

&

From y 00 : y 00 D 0 at x D y 00 y 4 3

2

x2

x

y D xe x ; y 0 D e x .1 C x/; y 00 D e x .2 C x/: From y: Asymptotes: y D 0 (at x D 1). Symmetry: .0;0/.  none.Intercept  1 2 Points: 1; , 2; , e e2 0 From y : CP: x D 1.

y



!x

Fig. 4.6-30

y0

1 3

^

p1 2

p1 2

00

yDx

_

C

yDe

C !x

j loc % min

1 p 2 j infl

1

2  C 0  C 2 j j j j j !x infl _ infl ^ infl _ infl ^ infl _

y ^

C

y

From y : y D 0 at x D ˙n. y 00 C

y 00

C %

C

2 j infl

_

^

x

!x

!x y

y D x ex

y D x C 2 sin x

x



Fig. 4.6-29

2

2

30. y D e x , y 0 D 2xe x , y 00 D .4x 2 2/e x . From y: Intercept: .0; 1/. Asymptotes: y D 0 (horizontal). Symmetry: even. From y 0 : Critical point: x D 0. y

0

y

C %

CP 0 j abs max

2 e2



1;

Fig. 4.6-31 32.

2

2;

&



y D e x sin x .x  0/, y 0 D e x .cos x sin x/, y 00 D 2e x cos x. From y: Intercept: .k; 0/, where k is an integer. Asymptotes: y D 0 as x ! 1.  C k, where k is an From y 0 : Critical points: x D 4 integer. y

!x

1 e

0

y

0 j

C %

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CP  4 j abs max

&

CP 5 C 4 j abs min %

CP 9 4 j loc max

&

!x

143

lOMoARcPSD|6566483

SECTION 4.6 (PAGE 255)

ADAMS and ESSEX: CALCULUS 9

From y 00 : y 00 D 0 at x D .k C integer.

1 2 /,

y

where k is an . 1;1=e/

y 00

0 j

y

 2 j infl

_

3 2 j infl

C ^

5 2 j infl

_

C ^

a

!x

p  =4 = 2

 4 ;e

x

yDe

y0



%

C

Fig. 4.6-32 y

y 00 D e

x2

x2

p

2



C %

!x

2. p 2C 2 j infl

2

j infl

^

p

CP 0 j abs min

_

C ^

!x

y

.2x

2x 3 / D 2x.1

6x 2

.2

2x.2x

x 2 /e

. 2;4e

x2

2/

2 x

yDx e

2x 3 //

2

D .2 10x 2 C 4x 4 /e x From y: Asymptotes: y D 0. Intercept:  Symmetry: even.  .0; 0/. 1 Points ˙1; e From y 0 : CP x D 0, x D ˙1. y0 C y %

CP 1 j abs max &

CP 0 C j abs min %

2

y 00

C

y

^

a j infl _

p

p 2C 2

2

Fig. 4.6-34 35. CP 1 j !x abs & max

From y 00 : y 00 D 0 if 2x 4 5x 2 C 1 D 0 p 5 ˙ 25 8 x2 D p4 5 ˙ 17 : D 4 s s p 5 C 17 5 so x D ˙a D ˙ , x D ˙b D ˙ 4

144

x

x2

y D x2e

y0 D e

&

From y 00 : y 00 D 0 at x D

x

y 00

33.

CP 2 j loc max

C

y 3 2

 2

a

b

y D x 2 e x , y 0 D .2x C x 2 /e x D x.2pC x/e x , p 2/.x C 2 C 2/e x . y 00 D .x 2 C 4x C 2/e x D .x C 2 From y: Intercept: .0; 0/. Asymptotes: y D 0 as x ! 1. From y 0 : Critical point: x D 0, x D 2.

sin x

5 4

b

x2

y D x2e

Fig. 4.6-33 34.

y

.1;1=e/

b C b j j infl ^ infl _

ln x ; x

1 ln x y0 D x2  1 x2 .1 ln x/2x 2 ln x 3 x y 00 D D x4 x3 From y: Asymptotes: x D 0, y D 0. Symmetry:  0/.   Intercept: .1;  none. 3 1 , e 3=2 ; 3=2 . Points: e; e 2e From y 0 : CP: x D e. yD

y0 p

y 17

4

.

ASY 0 j

C %

CP e j abs max

&

!x

From y 00 : y 00 D 0 at x D e 3=2 .

a C j !x infl ^

y 00 y

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ASY 0 j

_

e 3=2 j infl

C ^

!x

x

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 4.6 (PAGE 255)

y

37.

.e;1=e/ e 3=2

1

yD

x

ln x x

ln x .x > 0/, x2 6 ln x 5 1 2 ln x , y 00 D . y0 D 3 x x4 From y: Intercepts: .1; 0/. Asymptotes: y D 0, since ln x ln x D 0, and x D 0, since lim D 1. lim x!1 x 2 x!0C x 2 From y 0 : Critical point: x D e 1=2 .

y

C %

CP p e j abs max

&

y

yD p

y

y

0 j

1=2 2

x

Fig. 4.6-37 5=6

j infl

38. C ^

!x

y p . e;.2e/

x

, y 0 D .x 2 C 1/ 3=2 , y 00 D 3x.x 2 C 1/ 5=2 . C1 From y: Intercept: .0; 0/. Asymptotes: y D 1 as x ! 1, and y D 1 as x ! 1. Symmetry: odd. From y 0 : No critical point. y 0 > 0 and y is increasing for all x. From y 00 : y 00 D 0 at x D 0. yD p

x2

1/

e 5=6

1

x2

2

e _

1 4

!x

From y 00 : y 00 D 0 at x D e 5=6 . 00

ASY 2 j

y0

36. y D

0 j

D .4 x 2 / 1=2 4 x2 x 1 .4 x 2 / 3=2 . 2x/ D y0 D 2 .4 x 2 /3=2 3 .4 x 2 /3=2 x .4 x 2 /1=2 . 2x/ 00 2 y D .4 x 2 /3 4 C 2x 2 D .4 x 2 /5=2 From y: Asymptotes: x D ˙2. Domain 2 < x < 2. Symmetry: even. Intercept: .0; 21 /. From y 0 : CP: x D 0. CP ASY 0 C 2 j j !x abs y & % min 00 00 00 From y : y D 0 nowhere, y > 0 on . 2; 2/. Therefore, y is concave up.

Fig. 4.6-35

y0

1

yD p

x

y 00

C

y

^

0 j infl

_

!x

y yD1

ln x yD 2 x

yD 1

Fig. 4.6-36

yD p

x x2

x

C1

Fig. 4.6-38

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145

lOMoARcPSD|6566483

SECTION 4.6 (PAGE 255)

39.

ADAMS and ESSEX: CALCULUS 9

y D .x 2 1/1=3 2 y 0 D x.x 2 1/ 2=3 3 2 2 y 00 D Œ.x 2 1/ 2=3 x.x 2 1/ 5=3 2x 3 3   x2 2 2 .x 1/ 5=3 1 C D 3 3 From y: Asymptotes: none. Symmetry: even. Intercepts: .˙1; 0/, .0; 1/. From y 0 : CP: x D 0. SP: x D ˙1. SP 1 j

y0 y

&

&

CP 0 j abs min

SP 1 j

C %

C %

From f : Intercept: .0; 0/, .˙1; 0/. Asymptotes: none. Symmetry: odd. 1 From f 0 : CP: x D ˙ . SP: x D 0. e

f f

0

C %

y

C

1 j infl

_

!x

&

CP 1 e j loc min

&

C

0 j infl

_

_

%

!x

^

!x

!x 1 1 ; e e

1/1=3

 1 1 e; e

1

C

y

y

y D .x 2

0 j

f 00 f

1 j infl

^

SP

From f 00 : f 00 is undefined at x D 0.

From y 00 : y 00 D 0 nowhere. y 00

CP 1 e j loc max



x

y D x ln jxj

1 x

Fig. 4.6-40 1

sin x . 1 C x2 Curve crosses asymptote at infinitely many points: x D n .n D 0; ˙1; ˙2; : : :/. y sin x yD 1 C x2

41. y D 0 is an asymptote of y D

Fig. 4.6-39

40. According to Theorem 5 of Section 4.4,

yD

1 1Cx 2

lim x ln x D 0:

x!0C

Thus, x

lim x ln jxj D lim x ln x D 0:

x!0

x!0C

If f .x/ D x ln jxj for x ¤ 0, we may define f .0/ such that f .0/ D lim x ln jxj D 0. Then f is continuous on x!0

yD

the whole real line and

f 0 .x/ D ln jxj C 1;

146

f 00 .x/ D

1 sgn .x/: jxj

Copyright © 2018 Pearson Canada Inc. Downloaded by ted cage ([email protected])

Fig. 4.6-41

1 1Cx 2

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 4.8 (PAGE 267)

Section 4.7 Graphing with Computers (page 261) 1.

> plot([exp(x)*ln(1+1/exp(x)), > 0.71*exp(x-35.7)], x=33..38, > y =0..2, style=point, symbol=[circle, point], > color = [red, black], numpoints = 1500);

(b) The problem is with g.x/. When x grows large enough, the argument of the square root is evaluated as 22x , as the computer discards the 1. When this happens, the argument of the logarithm vanishes and the computer could be expected to return 1. However we now arrive at the case of the previous exercise. The computer will return a variety of complex numbers, infinite values, and finite real values, produced by the computer evaluation of the logarithm of the expression in question 2. The computer only plots the finite real values, but all of them are completely spurious.

will produce the curve as shown in the given figure (in red), and also the exponential curve (black) conforming to the rightmost stripe as shown in this figure:

(c) The argument of the square root is 22x .1 2 2x /. The computer will begin to encounter serious difficulties for values of x beginning where 2 2x  , that is, 2x D 52 or x D 26. This is evident in the figure.

The longest (rightmost) of the exponential stripes in the given figure seems to begin at about .0:71; 35:7/. Accordingly, the plot command

2 1.8 1.6 1.4 1.2 y 1 0.8 0.6 0.4 0.2

4.

1111111111 D

2 34

35

x

36

37

38

5.

Fig. 4.7-1 (The red curves appear gray here.) Other exponential stripes can be handled similarly

52

2

1023

D2

D 10

52 1023 1075 log10 2

 10

324

:

As in the previous exercise, there are 10 bits available for the exponent, so the largest possible exponent is 1111111111 in base 2, or 1023 in base 10. The largest possible mantissa is 0:111    111 (52 digits) 1 1 1 D C 2 C    C 52 2 2 2 1 D1  1: 252

2. The square of any number will tend to require an increased number of digits to represent it—especially for squares of numbers with large numbers of digits to begin with. However on a computer the number of digits is fixed so the least significant digits are discarded. The resulting number is different from the square of the original number. Consequently the square root will not be quite the same and the expression cannot be expected to vanish exactly.

Thus the largest positive floating-point number is approximately 21023 D 101023 log10 2  10308 .

Section 4.8 Extreme-Value Problems (page 267)

3. (a) We have  g.x/ D ln 2x  D ln

D

 1 C 2 C 22 C    C 29 ;

that is, 1023 in base 10. The smallest positive mantissa is 0:000    001 D 2 52 , so the smallest positive binary floating-point number is

0 33

D

Since there are 64 52 2 D 10 bits left to represent the exponent the absolute value of the exponent, the smallest possible exponent is

p

22x

 1

1. 

1 p 22x 1 p 2x C 22x 1 p p ln .2x 22x 1/.2x C 22x   p ln 2x C 22x 1 D f .x/: 2x

1/

!

Let the numbers be x and 7 x. Then 0  x  7. The product is P .x/ D x.7 x/ D 7x x 2 . P .0/ D P .7/ D 0 and P .x/ > 0 if 0 < x < 7. Thus maximum P occurs at a CP: 0D

dP D7 dx

2x ) x D

7 : 2

The maximum product is P .7=2/ D 49=4.

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147

lOMoARcPSD|6566483

SECTION 4.8 (PAGE 267)

ADAMS and ESSEX: CALCULUS 9

8 where x > 0. Their sum is 2. Let the numbers be x and x 8 S D x C . Since S ! 1 as x ! 1 or x ! 0C, the x minimum sum must occur at a critical point:

7.

P D P .x/ D 2x C

p 8 ) x D 2 2: x2

dS 0D D1 dx

0D

3. Let the numbers be x and 60 x. Then 0  x  60. Let P .x/ D x 2 .60 x/ D 60x 2 x 3 . Clearly, P .0/ D P .60/ D 0 amd P .x/ > 0 if 0 < x < 60. Thus maximum P occurs at a CP: dP D 120x dx

3x 2 D 3x.40

8.

x/:

3

D x .16

x/5

5x 3 .16

4

x/ .48

0D

x/4

8x/:

0  x  10:

S.0/ D 100 and S.10/ D 1; 000. For CP: 0 D S 0 .x/ D 3x 2

2.10

x/ D 3x 2 C 2x

20:

p The only positive CP is x D . 2 C 4 C 240/=6  2:270. Since S.2:270/  71:450, the minimum value of S is about 71.45. 6. If the numbers are x and n sum of their squares is

x, then 0  x  n and the

S.x/ D x 2 C .n

p

A D xh D x y 2

2.n

x2 D x

s 

x/2 :

x/ D 2.2x

P 2

P 2

x

2

x2:

P P2 2P x P x D 0, or x D . Thus y D P =3 and 2 6 the triangle is equilateral since all three sides are P =3.

i.e.,

y

y

h

n/ ) x D n=2:

Since S.n=2/ D n2 =2, this is the smallest value of the sum of squares.

148

2x ) x D

Evidently, y  x so 0  x  P =4. If x D 0 or x D P =4, then A D 0. Thus the maximum of A must occur at a CP. For max A: s Px dA P2 D Px r 0D ; dx 4 P2 Px 2 4

Observe that S.0/ D S.n/ D n2 . For critical points: 0 D S 0 .x/ D 2x

dA DP dx

Let the dimensions of the isosceles triangle be as shown. Then 2x C 2y D P (given constant). The area is

x. We want to minimize x/2 ;

x 2 D A D xy ) x D y:

)

P Hence, the width and the length are and 2 P P / D . Since the width equals the length, it .P 2 2 is a square. 9.

S.x/ D x 3 C .10

2A x2

Let the width and the length of a rectangle of given perimeter 2P be x and P x. Then the area of the rectangle is A.x/ D x.P x/ D P x x 2 :

5

The critical points are 0, 6 and 16. Clearly, P .0/ D P .16/ D 0, and P .6/ D 216  105 . Thus, P .x/ is maximum if the numbers are 6 and 10. 5. Let the numbers be x and 10

dP D2 dx

Since A.x/ ! 1 as x ! ˙1 the maximum must occur at a critical point:

4. Let the numbers be x and 16 x. Let P .x/ D x .16 x/ . Since P .x/ ! 1 as x ! ˙1, so the maximum must occur at a critical point:

2

.0 < x < 1/:

Thus min P occurs for x D y, i.e., for a square.

Therefore, x D 0 or 40. Max must correspond to x D 40. The numbers are 40 and 20.

0 D P 0 .x/ D 3x 2 .16

2A ; x

Evidently, minimum P occurs at a CP. For CP:

p p 8 Thus, the smallest possible sum is 2 2 C p D 4 2. 2 2

0D

Let the dimensions of a rectangle be x and y. Then the area is A D xy and the perimeter is P D 2x C 2y. Given A we can express

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x

x

Fig. 4.8-9

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 4.8 (PAGE 267)

10. Let the various dimensions be as shown in the figure. Since h D 10 sin  and b D 20 cos  , the area of the triangle is A. / D 21 bh D 100 sin  cos  D 50 sin 2

for 0 < 
0 for 0 < x < 10. Thus A will be maximum at a critical point. For a critical point

x 0

0 D A .x/ D

p

100

100 D p

x2 100

x x2

x2



1

p 2 100

x2

 . 2x/

:

2 Thus the p critical point is given by 2x D 100, so 50. The maximum area of the triangle is x p D A. 50/ D 50 cm2 .

Fig. 4.8-13 14.

x2

See the diagrams below. a) The area of the rectangle is A D xy. Since y a

x

D

b b.a x/ )yD : a a

16.

Thus, the area is A D A.x/ D

bx .a a

x/

.0  x  a/:

A. / D

For critical points: 0 D A0 .x/ D

b .a a

a : 2

2x/ ) x D

NEED FIGURE If the equal sides of the isosceles triangle are 10 cm long and the angles opposite these sides are  , then the area of the triangle is

2b < 0, A must have a maximum Since A00 .x/ D a a value at x D . Thus, the largest area for the rectan2 gle is   ab a b a square units; D a a 2 2 4 that is, half the area of the triangle ABC . A C

1 .10/.10 sin  / D 50 sin  cm2 ; 2

which is evidently has maximum value 50 cm2 when  D =2, that is, when the triangle is right-angled. This solution requires no calculus, and so is easier than the one given for the previous problem.

17.

Let the width and the height of the billboard be w and h m respectively. The area of the board is A D wh. The printed area is .w 8/.h 4/ D 100. 100w 100 and A D 4w C ; .w > 8/. Thus h D 4 C w 8 w 8 Clearly, A ! 1 if w ! 1 or w ! 8C. Thus minimum A occurs at a critical point:

b

x C

dA 100 100w D4C dw w 8 .w 8/2 100w D 4.w 2 16w C 64/ C 100w 0D

y a x a

B

A

D

B

w Fig. 4.8.14(a)

Fig. 4.8.14(b)

(b) This part has the same answer as part (a). To see this, let CD ? AB, and solve separate problems for the largest rectangles in triangles ACD and BCD as shown. By part (a), both maximizing rectangles have the same height, namely half the length of CD. Thus, their union is a rectangle of area half of that of triangle ABC .

150

2

wD

16w

16 ˙

800

136 D 0 p p 800 D 8 ˙ 10 2: 2

p Since w > 0 we must have w D 8 C 10 2. p 100 Thus h D 4 C p D 4 C 5 2. 10 2 p p The billboard should be 8 C 10 2 m wide and 4 C 5 2 m high.

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lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 4.8 (PAGE 267)

For maximum profit: w 2

0D (Since

h

4

w 8

20.

2

Fig. 4.8-17 18. Let x be the side of the cut-out squares. Then the volume of the box is V .x/ D x.70

2x/.150

2x/

If the manager charges $.40 C x/ per room, then .80 2x/ rooms will be rented. The total income will be $.80 2x/.40 C x/ and the total cost will be $.80 2x/.10/ C .2x/.2/. Therefore, the profit is P .x/ D .80

0 D V 0 .x/ D 4.2625 220x C 3x 2 / D 4.3x 175/.x 15/ 175 : ) x D 15 or 3

21.

T D

p

0D

70

dT 1 1 x p D dx 15 122 C x 2 39 p ) 13x D 5 122 C x 2 ) .132

Fig. 4.8-18

D 4.500; 000 C 500x

 13 5 T .0/ C D 0:9949 < T .10/: 15 39 (Or note that

2

1 d T D dt 2 15

x, so the total monthly profit

D x/ D 4.500 C x/.1000 x 2 /:

52 /x 2 D 52  122 ) x D 5

T .5/ D

19. Let the rebate be $x. Then number of cars sold per month is x 2000 C 200 D 2000 C 4x: 50

P D .2000 C 4x/.1000

10 x 122 C x 2 C : 15 39

T .0/ D

150 2x

The profit per car is 1000 is

for x > 0:

10 12 C D 1:0564 hrs 15 39 p 244 D 1:0414 hrs T .10/ D 15 For critical points:

150

70 2x

2x/.10/ C .2x/.2/

Head for point C on road x km east of A. Travel time is

We have

30/ D 72; 000 cm3 :

x x

2x

Œ.80

2

If P 0 .x/ D 16 4x D 0, then x D 4. Since P 00 .x/ D 4 < 0, P must have a maximum value at x D 4. Therefore, the manager should charge $44 per room.

The only critical point in Œ0; 35 is x D 15. Thus, the largest possible volume for the box is 30/.150

2x/.40 C x/

D 2400 C 16x

.0  x  35/:

Since V .0/ D V .35/ D 0, the maximum value will occur at a critical point:

V .15/ D 15.70

2x/ ) x D 250:

d 2P D 8 < 0 any critical point gives a local dx 2 max.) The manufacturer should offer a rebate of $250 to maximize profit.

4 h 4

dP D 4.500 dx

x/

p

122 C x 2

p

x2

122 C x 2 122 C x 2

122 >0 15.122 C x 2 /3=2

so any critical point is a local minimum.) To minimize travel time, head for point 5 km east of A.

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151

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SECTION 4.8 (PAGE 267)

A

ADAMS and ESSEX: CALCULUS 9

C

x

(b) Since E t0 D a`w 2 .2w C 3u/=.w C u/2 > 0 for all w > 0, E t is an increasing function of w. Thus its smallest value occurs for the smallest value of w that permits flight, namely w D s. The minimum energy for the tailwind trip is E t D k`s 3 =.s C u/.

B

10 x

39 km/h

12 15 km/h

p

(c) The minimum energy for the tailwind part of the round trip in part (b) is independent of u. However, for the headwind part, the minimum Eh D v D 3u=2 only applies as long as v  s. Otherwise the plane cannot fly. If u > 2s=3, then v D 3u=2 and the least total energy for the trip is k`.s 3 =.s C u/ C 27u2 =4/. If u < 2s=3, then the minimum value for Eh at v D 3u=2 implies a speed too slow to stay airborne. As Eh0 > 0 when v > 3u=2 the the least value for Eh that is admissible happens for v D s. Thus the total energy becomes 2k`s 4 =.s 2 u2 /.

122 Cx 2

P

Fig. 4.8-21 22. This problem is similar to the previous one except that the 10 in the numerator of the second fraction in the expression for T is replaced with a 4. This has no effect on the critical point of T , namely x D 5, which now lies outside the appropriate interval 0  x  4. Minimum T must occur at an endpoint. Note that

25.

Use x m for the circle and 1 of areas is

x 2 C 4 2 x/2

A D  r 2 C s2 D 2

D

4 12 C D 0:9026 T .0/ D 15 39 1p 2 T .4/ D 12 C 42 D 0:8433: 15

E D 3000k

x .1 C 4 42



1

x 4

2

.0  x  1/

1 1 , A.1/ D > A.0/. For CP: 16 4   1 x 1 x 1  1 dA D )x C : D )xD 0D dx 2 8 2 8 8 4C

Now A.0/ D

The minimum travel time corresponds to x D 4, that is, to driving in a straight line to B. 23. The time for the trip is 3000=.v needed for the trip is

x m for square. The sum

Since

100/, so the total energy

for A.

v3 ; v 100

d 2A 1 1 D C > 0, the CP gives local minimum dx 2 2 8

a) For max total area use none of wire for the square, i.e., x D 1. 4  D m b) For minimum total area use 1 4C 4C for square.

where k is a constant. Evidently we must have v > 100 or the trip would be impossible. The minimum value of E will occur at a critical point where

1 metre 3

0D

dE 2v D dv .v

2

1 x

x

300v : 100/2

s

The minimum thus occurs at v D 150 knots, and the time for the flight at this speed would be 3000=50 D 60 hours, or 2.5 days. This is much slower than commercial airliners can travel; the time for the flight at that speed is not much shorter than a fast ship could cross the Atlantic ocean.

r s xDC D2 r

1 xDP D4s

Fig. 4.8-25

24. (a) As shown in the previous exercise, the energy for a flight with airspeed v into the headwind is Eh D k`v 3 =.v u/. Similarly, the energy for a flight of the same distance with airspeed w and a tailwind of speed u is E t D k`w 3 =.w C u/.

152

26.

Let the dimensions of the rectangle be as shown in the figure. Clearly,

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x D a sin  C b cos ; y D a cos  C b sin :

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 4.8 (PAGE 267)

y

Therefore, the area is A. / D xy D .a sin  C b cos  /.a cos  C b sin  / D ab C .a2 C b 2 / sin  cos  1 D ab C .a2 C b 2 / sin 2 2

for 0   

Y

 : 2

 . Since 4  A00 . / D 2.a2 C b 2 / sin 2 < 0 when 0    , 2  therefore A. / must have a maximum value at  D . 4 Hence, the area of the largest rectangle is

9

If A0 . / D .a2 C b 2 / cos 2 D 0, then  D

A

  4

  1 D ab C .a2 C b 2 / sin 2 2 1 1 D ab C .a2 C b 2 / D .a C b/2 2 2

sq. units.

b a (Note: x D y D p C p indicates that the rectangle 2 2 containing the given rectangle with sides a and b, has largest area when it is a square.)

p .9; 3/

 p

3

 X

x

Fig. 4.8-27 28.

The longest beam will have length equal to the minimum of L D x C y, where x and y are as shown in the figure below: b a ; yD : xD cos  sin  Thus,   a b  L D L. / D C 0 2/ x x2 4 dx D 2 sec  tan  d Z 2 sec  tan  d D 2 sec  2 tan  Z  1 x 1 d D C C D sec 1 C C: D 2 2 2 2

4x 2 C4xC5

2xC1

 2

Fig. 6.3-19 p x2 4

x 

20.

Z

21.

Z

2

Fig. 6.3-15 16.

Z

dx p Let x D a sec  .a > 0/ x 2 x 2 a2 dx D a sec  tan  d Z a sec  tan  d D aZ2 sec2  a tan  1 1 cos  d D 2 sin  C C D 2 a a p 1 x 2 a2 C C: D 2 a x p x 2 a2

x  a

Fig. 6.3-16

226

Z x dx .x 1/ C 1 D dx Let u D x x 2 2x C 3 .x 1/2 C 2 du D dx Z Z du u du C D u2 C 2 u2 C 2   1 1 u D ln.u2 C 2/ C p tan 1 p CC 2 2 2  1 1 1 2 1 x 2x C 3/ C p tan p C C: D ln.x 2 2 2

x dx p 2ax x2 Z x dx Let x a D a sin  p D a2 .x a/2 dx D a cos  d Z .a C a sin  /a cos  d D a cos  D a. cos  / C C x a p D a sin 1 2ax x 2 C C: a

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1

1 2

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 6.3 (PAGE 355)

24. a x a



p 2ax x 2

Fig. 6.3-21

22.

Z

p

dx .4x x 2 /3=2 Z dx Let 2 x D 2 sin u D Œ4 .2 x/2 3=2 Z Z dx D 2 cos u du 2 cos u du 1 D sec2 u du D 8 cos3 u 4 1 1 x 2 D tan u C C D p C C: 4 4 4x x 2 2 u

Z D D D D D D

.3 Z Z



x dx 2x x 2 /3=2 x dx 4

.x C 1/2

.2 sin 

Let x C 1 D 2 sin  dx D 2 cos  d

3=2

1/2 cos  d 3 8 cos Z Z 1 1 sec  tan  d sec2  d 2 4 1 1 sec  tan  C C 2 4 xC1 1 1 CC p p 2 4 3 2x x 2 3 2x x 3 x 1 p C C: 4 3 2x x 2

xC1

1

Fig. 6.3-24

25.

p 4x x 2

x 2 C2xC2 u

2 x

Fig. 6.3-22

23.

Z dx dx D Let x C 1 D tan u .x 2 C 2x C 2/2 Œ.x C 1/2 C 12 dx D sec2 u du Z Z 2 sec u du D cos2 u du D sec4 u Z 1 u sin 2u D .1 C cos 2u/ du D C CC 2 2 4 1 1 D tan 1 .x C 1/ C sin u cos u C C 2 2 1 xC1 1 C C: D tan 1 .x C 1/ C 2 2 x 2 C 2x C 2

Z

Z

dx Let x D tan  .1 C x 2 /3 dx D sec2 d Z Z 2 sec  D d D cos4  d sec6   Z  1 C cos 2 2 D d 2  Z  1 1 C cos 4 D d 1 C 2 cos 2 C 4 2 3 sin 2 sin 4 D C C CC 8 4 32 sin  cos  sin 2 cos 2 3 C C CC D 8 2 16 3 sin  cos  1 D C C sin  cos .2 cos2  1/ C C 8 2 8   3 1 1 x x 2 D tan 1 x C  C 1 CC  8 2 1 C x2 8 1 C x2 1 C x2 3 1 3 x x D tan 1 x C  C  CC 8 8 1 C x2 4 .1 C x 2 /2 3x 3 C 5x 3 C C: D tan 1 x C 8 8.1 C x 2 /2 p

2

1Cx 2

xC1



p

x

 1

3 2x x 2

Fig. 6.3-23

Fig. 6.3-25

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227

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SECTION 6.3 (PAGE 355)

26.

ADAMS and ESSEX: CALCULUS 9

Z

x 2 dx Let x D tan u .1 C x 2 /2 dx D sec2 u du Z Z 2 tan u sec2 u du tan2 u du D D 4 sec u Z sec2 u Z 1 .1 cos 2u/ du D sin2 u du D 2 u sin u cos u D CC 2 2 1 1 x D tan 1 x C C: 2 2 1 C x2 p

1Cx 2

28.

x

Fig. 6.3-26

29.

30.

Z p 1 x2 dx Let x D sin  x3 dx D cos  d Z cos2  d D I; where D 3 Z sin  I D cot2  csc  d

D D

csc  cot 

d V D cot  csc  d V D csc 

csc3  d

csc  cot 

Z

csc  d

I:

Therefore 1 1 I D csc  cot  C ln j csc  C cot  j C C 2p 2 ˇ ˇ p 1 ˇˇ 1 1 1 x2 1 x 2 ˇˇ C ln ˇ C D ˇCC ˇ 2 x2 2 ˇx x p p 1 1 x2 1 1 C C: ln jxj D ln.1 C 1 x 2 / 2 2 2 x2

228

Z

U D sec  d V D sec2  d d U D sec  tanZ d V D tan  D 9 sec  tan  9 sec  tan2  d Z D 9 sec  tan  9 sec .sec2  1/ d Z Z D 9 sec  tan  C 9 sec  d 9 sec3  d

1

U D cot  d U D csc2 Z d

Let x D 3 tan  dx D 3 sec2  d

3 sec  3 sec2  d Z D 9 sec3  d

D

u

27.

Z p I D 9 C x 2 dx

31.

D 9 sec  tan  C 9 ln j sec  C tan  j I ˇp ˇ " p ! # x ˇˇ 9 C x2  x  9 ˇˇ 9 C x 2 9 C ˇCC C ln ˇ I D 2 3 3 2 ˇ 3 3ˇ   p p 9 1 D x 9 C x 2 C ln 9 C x 2 C x C C1 : 2 2 9 ln 3) (where C1 D C 2 Z dx p Let x D u2 2C x dx   2u du Z D Z 2 2u du D2 du 1 D 2Cu uC2 p p D 2u 4 ln ju C 2j C C D 2 x 4 ln.2 C x/ C C: Z dx Let x D u3 1 C x 1=3 dx D 3u2 du Z 2 u du D3 Let v D 1 C u 1Cu dv D du  Z  Z 2 1 v 2v C 1 dv D 3 dv v 2C D3 v v   2 v 2v C ln jvj C C D3 2 3 D .1 C x 1=3 /2 6.1 C x 1=3 / C 3 ln j1 C x 1=3 j C C: 2 Z 1 C x 1=2 . dx Let x D u6 I D 1 C x 1=3 5 dx D 6u du Z 8 Z u C u5 1 C u3 5 6u du D 6 du: D 1 C u2 1 C u2 Division is required to render the last integrand as a polynomial with a remainder fraction of simpler form: observe that u8 D u8 C u6

6

u5 D u5 C u3

3

2

u6

D .u C 1/.u 2

D .u C 1/.u

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u3

u4 C u4 C u2

4

2

u Cu

uCu

u/ C u:

1/ C 1

u2

1C1

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 6.3 (PAGE 355)

Thus

35. 8

5

u Cu D u6 u2 C 1 Therefore Z  I D6 u6 u7 D6 7

u4 C u3 C u2

4

3

u Cu Cu

u5 u4 u3 C C 5 4 3

1 C ln.u2 C 1/ C tan 2 D

32.

2

1

u u2 2 !

1C

u

uC1 : u2 C 1

uC1 1C 2 u C1



du

u 36.

u CC

6 7=6 6 5=6 3 2=3 x x C x C 2x 1=2 3x 1=3 7 5 2 C 3 ln.1 C x 1=3 / C 6 tan 1 x 1=6 C C:

6x 1=6

p x 2 x2 p dx Let u2 D x 2 C 1 x2 C 1 2u du D 2x dx Z p u 3 u2 du D u Z p p D 3 u2 du Let u D 3 sin v p du D 3 cosZv dv Z p p D . 3 cos v/ 3 cos v dv D 3 cos2 v dv

Z

3 .v C sin v cos v/ C C 2 p   3 u 3 u2 u 3 C CC D sin 1 p 2 2 3 3 0s 1 x2 C 1 3 1p 2 AC .x C 1/.2 D sin 1 @ 2 3 2

34.

Z

0

p ex 1

e 2x dx

1

dx x 2 C 2x C 2

p 3 1

D

Z

p 3

D

Z

Z

1

0

dx .x C 1/2 C 1

Let u D x C 1 du D dx ˇp3 ˇ  du ˇ D tan 1 uˇ D : ˇ u2 C 1 3 0

2

dx p 9 x2

Let x D 3 sin u dx D 3 cos u du Z xD2 Z 3 cos u du 1 xD2 2 D D csc u du 2 9 xD1 xD1 9 sin u.3 cos u/ ˇxD2 ! ˇxD2 p ˇ 1 1 9 x 2 ˇˇ ˇ D D . cot u/ˇ ˇ ˇ ˇ 9 9 x xD1 xD1 p ! p p p 5 8 5 1 2 2 : D D 9 2 1 9 18 x2

3 u

x

p 9 x2

Fig. 6.3-36

37.

x 2 / C C:

Let e x D sin  e x dx D cos  d Z =2 ˇ=2 1 ˇ cos2  d D . C sin  cos  /ˇ D =6 2 =6 p ! p  1  3 3 : D D 2 3 4 6 8 Z =2 cos x p dx Let u D sin x 0 1 C sin2 x du D cos x dx Z 1 du p Let u D tan w D 1 C u2 0 du D sec2 w dw Z =4 Z =4 2 sec w dw D D sec w dw sec w 0 0 ˇ=4 ˇ ˇ D ln j sec w C tan wjˇ ˇ 0 p p D ln j 2 C 1j ln j1 C 0j D ln. 2 C 1/: ln 2

p 3 1

1

D

33.

Z

A Bt C C Dt C E t D C 2 C 2 2 2 .t C 1/.t C 1/ t C1 t C1 .t C 1/2  1 D A.t 4 C 2t 2 C 1/ C B.t 4 C t 3 C t 2 C t / .t C 1/.t 2 C 1/2  C C.t 3 C t 2 C t C 1/ C D.t 2 C t / C E.t C 1/ 8 8 ACB D0 BD A ˆ ˆ ˆ ˆ ˆ ˆ 1=2, then Z  Z  p dx dx > p D : I1 ./ D p x C x2 0 2 x 0

x2

U Dx d V D xe dx 2 d U D dx V D 12 e x ˇR # " Z ˇ 1 R x2 1 x2 ˇ e xe dx D lim ˇ C ˇ R!1 2 2 0 0 Z 1 1 1 x2 2 D lim Re R C e dx 2 R!1 2 0 1p 1p D : D0C 4 4

Z

Z

1

Thus I1 ./ D O. 1=2 / as  ! 0C, and I2 ./ D O./ as  ! 0C. Since  <  1=2 (for 0 <  < 1), both I1 ./ and I2 ./ are O. 1=2 / as  ! 0C, and so, therefore, is E./.

a) First we calculate Z

Z

dx C x C x2 0 Z  p dx jI1 ./j < p D2  x 0 Z 1 dx jI2 ./j < D : 2 1= x D

Thus the given integral must diverge to infinity.

42. We are given that

We have

46.

€.x/ D

Z

1

c

f .x/ dx D

a

tx

1

e

t

Z

b

f .x/ dx.

a

dt .

0

a) Since lim t!1 t x 1 e t=2 D 0, there exists T > 0 such that t x 1 e t=2  1 if t  T . Thus Z 1 Z 1 0 t x 1 e t dt  e t dt D 2e T =2 T

and

Z

1

tx

T

1

e

t

dt converges by the comparison

T

theorem.

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241

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SECTION 6.5 (PAGE 370)

ADAMS and ESSEX: CALCULUS 9

The approximations are

If x > 0, then Z

0

T

t

x 1

e

t

dt
> jI 4

jI

Tn j:

This is because the second derivative of f .x/ D x is f 00 .x/ D 1=.4x 3=2 /, which is not bounded on Œ0; 1.

8. Let

D

Z

x2

e

Let x D

dx

1

0

e

.1=t/2

1



1 t dt t2

dx D  Z 1 1=t 2 1 e dt D dt: 2 t t2 0

Observe that

lim

t!0C

e

1=t 2

t2

D lim

t!0C

D lim

t

2

e 1=t 2 2t 2

h1i 1

3

e 1=t . 2t 3 / 1 D 0: D lim t!0C e 1=t 2 t!0C

9.

Referring to Example 5, we have ex D 1 C x C

p

1

Hence, I  0:14, accurate to 2 decimal places. These approximations do not converge very quickly, because the 2 fourth derivative of e 1=t has very large values for some values of t near 0. In fact, higher and higher derivatives behave more and more badly near 0, so higher order methods cannot be expected to work well either.

 0:0631  0:0234  0:0085  0:0031:

Observe that, although these errors are decreasing, they are not decreasing like 1=n2 ; that is,

Z

/

 0:1430237  "  64 64 1 1 0 C 4 64e 64 C e 64=9 C e 64=25 C S8 D 3 8 9 25 #    64 64=49 16 16=9 16 4 1 e C 2 16e C 4e C e Ce 49 9

The errors are

I D

4

where Rn .f I 0; x/ D x. Now

xn x2 C  C C Rn .f I 0; x/; 2Š nŠ e X x nC1 , for some X between 0 and .n C 1/Š

jRn .f I 0; x 2 /j 

x 2nC2 .n C 1/Š

if 0  x  1 for any x, since x 2  X  0. Therefore ˇZ 1 ˇ Z 1 ˇ ˇ 1 2 ˇ ˇ x 2nC2 dx R .f I 0; x / dx n ˇ ˇ .n C 1/Š 0 0 1 : D .2n C 3/.n C 1/Š This error will be less than 10 4 if .2n C 3/.n C 1/Š > 10; 000. Since 15  7Š > 10; 000, n D 6 will do. Thus we use seven terms of the series (0  n  6): Z 1 2 e x dx 0  Z 1 x4 x6 x 8 x 10 x 12 1 x2 C  C C dx 2Š 3Š 4Š 5Š 6Š 0 1 1 1 1 1 1 C C C D1 3 5  2Š 7  3Š 9  4Š 11  5Š 13  6Š  0:74684 with error less than 10 4 .

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249

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SECTION 6.8 (PAGE 388)

10. We are given that previous exercise

Z

Z

1

x2

e

0 1

x2

e

0

Z

1

e

x2

1

11.

Z

dx D

1

ADAMS and ESSEX: CALCULUS 9

dx D

1 2

p

2 Dividing p the first two equations gives u D 3=5, so u D 3=5. Then 3A=5 D 1=3, so A D 5=9, and finally, B D 8=9.

 and from the

dx D 0:74684. Therefore, e

x2

dx

0

Z

14. 1

e

x2

dx

Z

0

1p D  2 D 0:139

0:74684 (to 3 decimal places).

Z

1 1

f .x/ dx D 2

1 0

.bx 2 C d / dx D 2

Af . u/ C Af .u/ D 2A.bu2 C d /:



b Cd 3

1



1

Error D

12. For any function f we use the approximation 1 1

p

Z

p

f .x/ dx  f . 1= 3/ C f .1= 3/:

We have 

1

x 4 dx 

1 p 3

4



 1 4 2 D p 9 3 1 Z 1 2 2 2 D  0:17778 x 4 dx Error D 9 5 9 1     Z 1 1 1 C cos p  1:67582 cos x dx  cos p 3 3 1 Z 1 cos x dx 1:67582  0:00712 Error D 1 Z 1 p p e x dx  e 1= 3 C e 1= 3  2:34270 1 Z 1 Error D e x dx 2:34270  0:00771: Z

C

15.

1

1



d b C Cf .bx C dx C f / dx D 2 F .x/ dx D 2 5 3 0 1 AF . u/ C BF .0/ C AF .u/ D 2A.bu4 C du2 C f / C Bf: 4

2

These two expressions are identical provided Au4 D

250

1 ; 5

Au2 D

1 ; 3

AC

B D 1: 2

 1:68300

e x dx  e 1 Z Error D

I D

Z

1

e

x2

1

cos x dx 1

p 1

3=5

Ce

e x dx

1

p

1:68300  0:00006 3=5

 2:35034

2:35034  0:00006:

dx

0

T11 D S2 D R1 D

13. If F .x/ D ax 5 C bx 4 C cx 3 C dx 2 C ex C f , then, by symmetry, Z

1

Z

  1 0 1 1 T00 D T1 D R0 D .1/ e C e  0:6839397 2 2   1 1 1 0 e C e 1=4 C e 1  0:7313703 T10 D T2 D 2 2 2  1 T20 D T4 D 2T2 C e 1=16 C e 9=16  0:7429841 4 1 0 4T4 C e 1=64 C e 9=64 C e 25=64 C e T3 D T8 D 8  0:7458656

1

Z

f .x/ dx 

2 r ! r !6 3 6 5 3 3 5 C 0 D 0:24000 x 6 dx  4 C 9 5 5 1 Z 1 Error D x 6 dx 0:24000  0:04571 1 " r !# r ! Z 1 3 3 5 8 cos x dx  cos C cos C 9 5 5 9 1 Z

These two expressionspare identical provided A D 1 and u2 D 1=3, so u D 1= 3. Z

i 8 p p 5h f. 3=5/ C f . 3=5/ C f .0/: 9 9

1

We have

If f .x/ D ax 3 C bx 2 C cx C d , then, by symmetry, Z

For any function f we use the approximation

T21 D S4 D 

T31 D S8 D

4T20

4T10

3 T10

3 4T30

T20 3

T00

 0:7471805

 0:7468554  0:7468261

16T21 T11  0:7468337 15 16T31 T21  0:7468242 T32 D 15 2 64T3 T22 T33 D R3 D  0:7468241 63 I  0:746824 to 6 decimal places. T22 D R2 D

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49=64



lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

16. From Exercise 9 in Section 7.6, for I D

Z

SECTION 6.8 (PAGE 388)

1:6

Thetransformation is not   suitable because the derivative of 1 1 1 cos sin is , which has very large values at t t2 t some points close to 0. In order to approximate the integral I to an desired degree of accuracy, say with error less than  in absolute value, we have to divide the integral into two parts: Z 1 sin x I D dx 1 C x2  Z 1 Z t sin x sin x dx C dx D 2 1 C x2 t  1Cx D I1 C I2 :

f .x/ dx, 0

T00 D T1 D 1:9196

T10 D T2 D 2:00188

T20 D T4 D 2:02622

T30 D T8 D 2:02929:

Hence, R1 D T11 D T21 D R2 D

T22

D

T31 D T32 D R3 D T33 D

4T10

T00 3

4T20

T10

D 2:0346684

If t  tan

D 2:0343333 D S4

3 16T21 T11 D 2:0346684 15 4T30 T20 D 2:0303133 D S8 3 1 1 16T3 T2 D 2:0300453 15 2 2 64T3 T2 D 2:0299719: 63



Z



2

, then

Z 1 sin x dx dx < 1 C x2 1 C x2 t t ˇ1 ˇ   ˇ 1 tan 1 .t /  : D tan .x/ˇ D ˇ 2 2 1

t

Now let ZA be a numerical approximation to the proper t sin x dx, having error less than =2 in absointegral 2  1Cx lute value. Then jI

17.

 2h  y0 C 4y2 C y4 3  h 1 T2 D S4 D y0 C 4y1 C 2y2 C 4y3 C y4 3 16T21 T11 R2 D T22 D 15 2h 16h .y C 4y 0 1 C 2y2 C 4y3 C y4 / 3 .y0 C 4y2 C y4 / D 3 15  h D 14y0 C 64y1 C 24y2 C 64y3 C 14y4 45  2h  7y0 C 32y1 C 12y2 C 32y3 C 7y4 D 45 T11 D S2 D

18. Let I D

Z

Aj D jI1 C I2 Aj  jI1 Aj C jI2 j    C D : 2 2

Hence, A is an approximation to the integral I with the desired accuracy. 19.

sin x ; x 2 x .cos x

x cos c sin x ; x2 x sin x cos x/ .x cos x f 00 .x/ D x4 2 x sin x 2x cos x C 2 sin x D : x3 Now use l’H^opital’s Rule to get f .x/ D

f 0 .x/ D

lim f 00 .x/

x!0

D lim

2x sin x

x 2 cos x

cos x D 3

1 : 3

x!0

1 

sin x dx 1 C x2

Let x D

1 t dt t2

dx D   1   Z 0 sin 1 t   dt D 1 t2 1= 1C 2 t   1 Z 1= sin t dt: D 1 C t2 0

sin x/2x

D lim

x!0

20.

2 cos x C 2x sin x C 2 cos x 3x 2

If t is time and E is error, then for the trapezoid rule, t 2 E is approximately constant. Since E D 6  10 16 when t D 175:777 seconds, the time we would expect our computer to achieve an error of 10 32 is about s 10 16 175:7772  6  seconds; 10 32 which is about 1,365 years.

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21.

ADAMS and ESSEX: CALCULUS 9

If t is time and E is error, then t 4 E is approximately constant for the Simpson’s Rule case. Since E D 3:15  10 30 when t D 175:777 seconds, we would expect our computer to achieve quadruple precision in time  10 175:7774  3:15  10

30 1=4

32

5.

seconds;

3 A B D C 4x 2 1 2x 1 2x C 1 2Ax C A C 2Bx B D 4x 2 1 n 3 2A C 2B D 0 ) )AD B D A BD3 2 Z 3 dx 3 dx D 2 4x 1 2 2x 1 ˇ ˇ 3 ˇˇ 2x 1 ˇˇ D ln ˇ C C: 4 2x C 1 ˇ

or about 12 minutes if it were using Simpson’s Rule. Since our computer did the calculation more than 5,000 times faster than that, it must have been using an even higher-order method.

Review Exercises on Techniques of Integration (page 390) 1.

6.

A B x D C 2 2x C 5x C 2 2x C 1 xC2 Ax C 2A C 2Bx C B D 2x 2 C 5x C 2 n A C 2B D 1 ) 2A C B D 0

Thus A D

D

x

Let u D x 1 du  dx  Z D uC1 1 1 du D C du u3 u2 u3 1 1 1 1 CC D C C: 2 u 2u x 1 2.x 1/2

.x Z

D 3.

1/3

sin3 x cos3 x dx Z D sin3 x.1 sin2 x/ cos x dx Z

.u3

U D x2 C x 2 d U D .2x C 1/ dx 1 .x 2 3

Cx

d V D sin 3x V D 13 cos 3x Z 1 2/ cos 3x C 3 .2x C 1/ cos 3x dx

U D 2x C 1 d V D cos 3x dx d U D 2 dx V D 31 sin 3x 2 1 3 .x

D

2 1 3 .x

D

u5 / du D

u4 4

Let u D sin x du D cos x dx

u6 CC 6

7.

Z p D

Z

C x 2/ cos 3x C 91 .2x C 1/ sin 3x Z 2 sin 3x dx 9

C x 2/ cos 3x C 91 .2x C 1/ sin 3x 2 C cos 3x C C: 27

1 x2 dx x4 cos2 

Let x D sin  dx D cos  d

d 4 Z sin  D csc2  cot2  d D D

Z

Let v D cot  dv D csc2  d

v3 CC 3 !3 p cot3  1 1 x2 CC D C C: 3 3 x v 2 dv D

1 4 1 6 sin x sin x C C: 4 6 p Z p .1 C x/1=3 dx Let u D 1 C x p x dx du D p 2 x Z D 2 u1=3 du D 2. 43 /u4=3 C C p D 32 .1 C x/4=3 C C:

252



2/ sin 3x dx

D

4.

dx 2x C 1

dx

Z

D

.x 2 C x

1=3 and B D 2=3. We have

Z Z 1 2 x dx dx dx D C 2x 2 C 5x C 2 3 2x C 1 3 xC2 1 2 ln j2x C 1j C C: D ln jx C 2j 3 6

Z

Z

D

Z

2.

Z

Z

1 x



p 1 x2

Fig. RT-7

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INSTRUCTOR’S SOLUTIONS MANUAL

8.

Z

x 3 cos.x 2 / dx

D

1 2

Z

REVIEW EXERCISES ON TECHNIQUES OF INTEGRATION (PAGE 390)

Let w D x 2 dw D 2x dx

13.

9.

10.

11.

Z

cos.x 2 / C C:

p 1C4x

2

x dx Let u D 5x 3 2 .5x 3 2/2=3 du D 15x 2 dx Z 1 1 u 2=3 du D u1=3 C C D 15 5 1 D .5x 3 2/1=3 C C: 5

1

Fig. RT-13 14.

Z

15.

Z

dx Let x D 2 tan  .4 C x 2 /2 dx D 2 sec2  d Z Z 1 2 sec2  d D cos2  d D 16 sec4  8 1 D . C sin  cos  / C C 16   1 x 1 x D tan 1 C C C: 16 2 8 4 C x2

cos x dx Let u D sin x 1 C sin2 x du D cos x dx Z du D D tan 1 u C C 1 C u2 D tan 1 .sin x/ C C:

D

Z

p

D D 16.

sin3 x dx D 7 Zcos x

Z

D 

D

Fig. RT-11

12.

.sin x C cos x/ dx D

Z

Dx

D

.1 C sin 2x/ dx 1 2

cos 2x C C:

.u3 C u5 / du D

Let u D tan x du D sec2 x dx

u6 u4 C CC 4 6

We have

D

2

tan3 x sec4 x dx

1 1 tan4 x C tan6 x C C: 4 6

Z

4Cx 2

Z

tan3 x.1 C tan2 x/ sec2 x dx

x

2

2x



1 A B .A C B/x C .5A 3B/ D C D x 2 C 2x 15 x 3 xC5 x 2 C 2x 15 n 1 1 ACB D0 ) )AD ; B D : 5A 3B D 1 8 Z Z 8 Z dx dx 1 1 dx D x 2 Cˇ 2x 15 8 x 3 8 x C5 ˇ 1 ˇˇ x 3 ˇˇ D ln ˇ C C: 8 x C 5ˇ

Z

Let 2x D tan  2x ln 2 dx D sec2  d

D

U Dw d V D cos w dw d U D dw Z V D sin w D 21 w sin w 12 sin w dw 1 2

p 2x 1 C 4x dx

Z 1 sec3  d ln 2  1  sec  tan  C ln j sec  C tan  j C C D 2 ln 2  p 1  xp D 2 1 C 4x C ln.2x C 1 C 4x / C C: 2 ln 2

w cos w dw

D 21 x 2 sin.x 2 / C

Z

D

q Let x D 35 tan u q dx D 35 sec2 u du q Z . 3 tan2 u/. 3 sec2 u/ du 5 5 x 2 dx .3 C 5x 2 /3=2

.3/3=2 sec3 u Z 1 .sec u cos u/ du p 5 5 1 p .ln j sec u C tan uj sin u/ C C 5 5 ˇp ! p p ˇˇ ˇ 5x 2 C 3 5x ˇ 5x 1 ˇ p CC p ln ˇ C p ˇ p ˇ 5 5 3 3 ˇ 5x 2 C 3 p p  1 x p C C0 ; p ln 5x 2 C 3 C 5x 5 5 5 5x 2 C 3 p 1 where C0 D C p ln 3: 5 5

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p

20. p 5x

5x 2 C3

u

p 3

Fig. RT-16 17.

I D

Z

e

sin 2x dx

U De x d U D e x dx 1 e 2

D

x

x

cos 2x

1 2

d V D sin 2x dx 1 V D cos 2x 2 Z e

x

21.

cos 2x dx

1 e 2

I D

19.

cos 2x

d V D cos 2x dx 1 V D sin 2x 2 ! 1 1 x 1 e sin 2x C I 2 2 2

Z

2x 2 C 4x 3 dx D x 2 C 5x # " Z 6x C 3 dx D 2 x.x C 5/

I D

Z

2x 2 C 10x 6x x 2 C 5x

6x C 3 A B .A C B/x C 5A D C D x.x C 5/ x xC5 x.x C 5/ n 27 3 ACB D6 : ) )AD ; B D 5A D 3 5 Z Z Z 5 3 dx 27 dx I D 2 dx 5 x 5 xC5 3 27 D 2x ln jxj ln jx C 5j C C: 5 5 Z I D cos.3 ln x/ dx U D cos.3 ln x/ 3 sin.3 ln x/ dx dU D Zx

D x cos.3 ln x/ C 3

d V D dx V Dx

Z

x ln.1 C x 2 / dx 1 C x2

3

22.

Z

23.

Z

dx

sin2 x cos4 x dx Z 1 D .1 cos 2x/Œ 12 .1 C cos 2x/2 dx 2 Z 1 D .1 C cos 2x cos2 2x cos3 2x/ dx 8 Z 1 1 1 .1 C cos 4x/ dx sin 2x D xC 8 Z 16 16 1 .1 sin2 2x/ cos 2x dx 8 1 x 1 1 x sin 2x sin 4x sin 2x D C 8 16 16 64 16 1 C sin3 2x C C 48 sin 4x sin3 2x x C C C: D 16 64 48 p x 2 dx p Let x D 2 sin  p 2 x2 dx D 2 cos  d Z D 2 sin2  d D  sin  cos  C C p x 2 x2 x C C: D sin 1 p 2 2

sin.3 ln x/ dx p

d V D dx U D sin.3 ln x/ 3 cos.3 ln x/ dx V Dx dU D x  D x cos.3 ln x/ C 3 x sin.3 ln x/ 3I

I D

254

Let u D ln.1 C x 2 / 2x dx du D 1 C x2

D

1 x 1 1 x e cos 2x e sin 2x I 2  4  4 2 1 e x cos 2x C sin 2x C C: 5 5

D

18.

x

1 A Bx C C D C 4x 3 C x x 4x 2 C 1 A.4x 2 C 1/ C Bx 2 C C x D 4x 3 C x  4A C B D 0 ) ) B D 4: C D 0; A D 1 Z Z Z 1 dx x dx dx D 4 4x 3 C x x 4x 2 C 1 1 ln.4x 2 C 1/ C C: D ln jxj 2

Z u2 1 u du D CC 2 4   2 1 ln.1 C x 2 / C C: D 4

U De x d U D e x dx D

ADAMS and ESSEX: CALCULUS 9

2 x



1 3 x cos.3 ln x/ C x sin.3 ln x/ C C: 10 10

p 2 x2

Fig. RT-23

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INSTRUCTOR’S SOLUTIONS MANUAL

24.

We have Z I D tan4 x sec x dx

27.

3

U D tan x d U D 3 tan2 x Zsec2 x dx

D tan3 x sec x

3

D tan3 x sec x

3

3 D tan Z x sec x

3I

REVIEW EXERCISES ON TECHNIQUES OF INTEGRATION (PAGE 390)

d V D tan x sec x dx V D sec x

tan2 x sec3 x dx

Z

tan2 x.tan2 x C 1/ sec x dx

I D

25.

Z D D D D

D

3J where

D

U D tan x d V D tan x sec x dx d U D sec2 xZ dx V D sec x 3 D tan x sec x sec x dx Z D tan x sec x .tan2 x C 1/ sec x dx

D tan x sec x J J D 21 tan x sec x 1 4

C

1 2

tan3 x sec x 3 8

28.

tan x sec x

ln j sec x C tan xj C C:

1

x  2

U D sin dU D p

dx x

1

2

dx

29.

Z

30.

Let

d V D x dx x2 V D 2

4 x2 Z  x 2 dx x 1 x sin 1 Let x D 2 sin u D p 2 2 2 4 x2 dx D 2 cos u du Z   x2 1 x 2 sin 2 sin u du D 2 2 Z   x x2 D sin 1 .1 cos 2u/ du 2 2 x x2 D sin 1 u C sin u cos u C C 2 2 2  x 1 p x 1 sin 1 C x 4 x 2 C C: D 2 2 4

Z 1 .1 2u2 C u4 / du 4   2 3 1 5 1 u C u CC u 4 3 5 1 1 1 cos 4x C cos3 4x cos5 4x C C: 4 6 20

Z

dx D 2x 3 C x

Z

x dx Let u D x 2 x 6 2x 4 C x 2 du D 2x dx Z 1 1 du du D D 2 u3 2u2 C u 2 u.u 1/2 1 A B C D C C u.u 1/2 u u 1 .u 1/2 A.u2 2u C 1/ C B.u2 u/ C C u D u3 2u2 C u ( ACB D0 ) 2A B C C D 0 ) A D 1; B D 1; C D 1: A D1 Z Z Z du du 1 du 1 1 D 2 u3 2u2 C u 2 u 2 u 1 Z du 1 C 2 .u 1/2 1 1 1 1 ln ju 1j CK D ln juj 2 2 2u 1 2 1 x 1 D ln 2 C K: 2 jx 1j 2.x 2 1/

ln j sec x C tan xj C C ln j sec x C tan xj C C:

3 8

Let u D cos 4x du D 4 sin 4x dx

We have I D

x 2 dx Let u D 4x C 1 .4x C 1/10 du D 4 dx  Z  u 1 2 1 1 du 4 4 u10 Z 1 .u 8 2u 9 C u 10 / du 64 1 1 1 u 7C u 8 u 9CC 448 256 576   1 1 1 1 C C C: 64 7.4x C 1/7 4.4x C 1/8 9.4x C 1/9

26. We have Z x sin

sin5 .4x/ dx Z D .1 cos2 4x/2 sin 4x dx

D

tan2 x sec x dx

J D

Z

2

x5 Z

dx 2 C ex Z e x dx D Let u D 2e x C 1 2e x C 1 du D 2e x dx Z du 1 1 D ln.2e x C 1/ C C: D 2 u 2

In D

D I0 D

Z

x n 3x dx U D xn d U D nx n

x n 3x Zln 3

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1

dx

d V D 3x dx 3x V D ln 3

n In 1 : ln 3 3x 3x dx D C C: ln 3

255

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REVIEW EXERCISES ON TECHNIQUES OF INTEGRATION (PAGE 390)

Hence, I3 D

34. Z

We have Z

3 x

x 3 dx !#

"

31.

Z

sin2 x cos x dx Let u D sin x 2 sin x du D cos x dx Z 2 u du D Let 2 u D v 2 u du D dv  Z Z  4 4v C v 2 4 D dv D C 4 v dv v v v2 CC D 4 ln jvj C 4v 2 1 D 4 ln j2 uj C 4.2 u/ .2 u/2 C C 2 1 2 sin x C C1 : D 4 ln.2 sin x/ 2 sin x 2

35.

32. We have ! Z x2 C 1 2x C 1 dx D dx 1 x 2 C 2x C 2 x 2 C 2x C 2 Z 2x C 1 dx Let u D x C 1 Dx .x C 1/2 C 1 du D dx Z 2u 1 Dx du u2 C 1 D x ln ju2 C 1j C tan 1 u C C D x ln.x 2 C 2x C 2/ C tan 1 .x C 1/ C C:

Z

33.

Z

dx p Let x D sin  x2 1 x2 dx D Z cos  d Z cos  d D csc2  d D sin2  cos  p 1 x2 D cot  C C D C C: x

Fig. RT-33

256

2x

p 1 4x 2

Fig. RT-35 Z D

x

p 1 x2

x 3 dx p Let 2x D sin  1 4x 2 2 dx D cos  d Z Z 1 sin3  cos  d 1 D .1 cos2  / sin  d D 16 cos  16   1 1 D cos  C cos3  C C 16 3 1p 1 1 4x 2 C C: .1 4x 2 /3=2 D 48 16



37.



Z

1

36.

1

x 3 .ln x/2 dx

d V D x 3 dx U D .ln x/2 1 2 V D x4 d U D ln x dx 4 x Z 1 4 1 x 3 ln x dx D x .ln x/2 4 2 U D ln x d V D x 3 dx 1 1 d U D dx V D x4 x 4 Z 1 1 4 1 D x 4 .ln x/2 x 3 dx x ln x C 4 8 8 " # 1 1 x4 ln x C .ln x/2 C C: D 4 2 8

3 x 2 3x 2 x3x 1 x 3 3x C C1 I0 ln 3 ln 3 ln 3 ln 3 ln 3 ln 3 " # 3 6x 6 3x 2 x x D3 C C1 : C ln 3 .ln 3/2 .ln 3/3 .ln 3/4 D

ADAMS and ESSEX: CALCULUS 9

Z

e 1=x dx x2 Z

Let u D du D

e u du D

1 x 1 dx x2

eu C C D

e 1=x C C:

xC1 p dx x2 C 1 Z p dx D x2 C 1 C p Let x D tan  x2 C 1 dx D sec2  d Z p D x 2 C 1 C sec  d p D x 2 C 1 C ln j sec  C tan  j C C p p D x 2 C 1 C ln.x C x 2 C 1/ C C:

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REVIEW EXERCISES ON TECHNIQUES OF INTEGRATION (PAGE 390)

42. p

1Cx 2 x

 1

Fig. RT-37 38.

Z

e .x

D3

1=3 /

Z

Let x D u3 dx D 3u2 du

u2 e u du D 3I2

43.

See solution to #16 of Section 6.6 for Z n u In D u e dx D un e u nIn 1 .

D 3Œu2 e u De 39.

I D

.x 1=3 /

Z

2.ue u

.3x 2=3

x3 x3

e u / C C

Assume that x  1 and let x D sec u and dx D sec u tan u du. Then Z x 2 dx p x2 1 Z Z sec3 u tan u du D sec3 u du D tan u 1 1 D sec u tan u C ln j sec u C tan uj C C 2 2 p 1 p 1 D x x 2 1 C ln jx C x 2 1j C C: 2 2 Differentiation shows that this solution is valid for x  1 also. Z Z .x C 1 1/ dx x dx D Let u D x C 1 I D x 2 C 2x 1 .x C 1/2 2 du D dx Z Z du u 1 1 2 D du D ln ju 2j : u2 2 2 u2 2 B A p C p D u 2 uC 2 p p Au C 2A C Bu 2B D 2 u 2  ACB D0 p ) 2.A B/ D 1 1 )AD B D p : 2 2 1

u2

6x 1=3 C 6/ C C:  Z  9x 3 3 dx D dx: 1C 3 9x x 9x

9x 3 A B C D C C x 3 9x x x 3 xC3 Ax 2 9A C Bx 2 C 3Bx C C x 2 3C x D x 3 9x 8 ( < A D 1=3 ACB CC D0 ) B D 4=3 ) 3B 3C D 9 : C D 5=3: 9A D 3

Thus we have

Z Z 4 dx dx 1 C 3 x 3 x 3 1 4 D x C ln jxj C ln jx 3j 3 3

40.

41.

Z

p

10 xC2 dx p xC2

Z 5 dx 3 xC3 5 ln jx C 3j C K: 3

p

xC2 dx du D p 2 xC2 Z p 2 2 u 10u C C D 10 xC2 C C: D 2 10 du D ln 10 ln 10 Z sin5 x cos9 x dx Z D .1 cos2 x/2 cos9 x sin x dx Let u D cos x du D sin x dx Z D

.1

Let u D

2u2 C u4 /u9 du

u12 u14 u10 C CC 10 6 14 12 10 cos x cos x cos14 x D C C: 6 10 14 D

ˇ ˇ ˇ u p2 ˇ 1 ˇ ˇ 2j p ln ˇ p ˇCK 2 2 ˇu C 2ˇ ˇ ˇ ˇ x C 1 p2 ˇ 1 1 ˇ ˇ 2 D ln jx C 2x 1j p ln ˇ p ˇ C K: 2 2 2 ˇx C 1 C 2ˇ

1 I D ln ju2 2

Thus we have I DxC

2

44.

45.

Z

2x

3

Let u D 4 3x C x 2 du D . 3 C 2x/ dx Z p p du D p D 2 u C C D 2 4 3x C x 2 C C: u Z x 2 sin 1 2x dx p

4

3x C x 2

D D D D

1

d V D x 2 dx x3 dU D p V D 3 1 4x 2 Z 3 2 x3 x dx sin 1 2x Let v D 1 4x 2 p 3 3 1 4x 2 dvD 8x dx  Z 1 v 2 1 x3 1 sin 2x dv 3 3 8 4v 1=2 Z   x3 1 sin 1 2x C v 1=2 v 1=2 dv 3 48 1p x3 1 3=2 sin 1 2x C v CC v 3 24 72 3 p x 1 1 sin 1 2x C .1 4x 2 /3=2 C C: 1 4x 2 3 24 72 U D sin

D

dx

2x 2 dx

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46. Let

p

3x D sec u and

Z p

3x 2 x

1

p

3 dx D sec u tan u du. Then

48.

D D

1 8

Z

2

sin

1

.2x

1 8u

1 2

Let x

dx

dx D

cos u du D

Thus

C

1 2

D

x2 2 x2 D 2

sin u

cos u du

1 8

p

x

x x2

Fig. RT-48 dx p Let x D u2 .4 C x/ x dx DZ 2u du Z 2u du du D D2 .4 C u2 /u 4 C u2 p x u 2 C C: D tan 1 C C D tan 1 2 2 2

258

1 2

sin u cos u C C p 1/ C 14 .2x 1/ x x 2 C C:

u

Z

3

1 2

52.

dx x 

1

3

d V D x dx x2 V D 2

3 dx 9 C x2 x 3 Z x2 x2 dx tan 1 D 2 3 2 9 C x2 !   3Z x2 9 1 x D dx 1 tan 2 3 2 9 C x2  x  3x x  9 x2 tan 1 C tan 1 C C: D 2 3 2 2 3 Z x4 1 dx I D x 3 C 2x 2 Z 4 3 x C 2x 2x 3 4x 2 C 4x 2 1 D dx x 3 C 2x 2  Z  2 4x 1 D dx: x 2C 3 x C 2x 2

I D

1 2

49.

51.

Z p

1 2 2/

x

dU D

Z 1 sin4 2x dx cos4 x sin4 x dx D 16 Z 1 D .1 cos 4x/2 dx 64  Z  1 1 C cos 8x D 1 2 cos 4x C dx 64 2   sin 8x 1 3x sin 4x C CC D 64 2 2 16   1 sin 8x D 3x sin 4x C C C: 128 8

1 4

1

U D tan

Z

x x 2 dx Z q 1 D .x 4

x tan

dx

1 Z tan u p sec u tan u du 3 D 1 p sec u 3 Z Z 2 D tan u du D .sec2 u 1/ du p p D tan u u C C D 3x 2 1 sec 1 . 3x/ C C   p 1 D 3x 2 1 C sin 1 p C C1 : 3x

47.

50.

Z

ADAMS and ESSEX: CALCULUS 9

A C B 4x 2 1 D C 2 C x 3 C 2x 2 x x xC2 Ax 2 C 2Ax C Bx C 2B C C x 2 D x 3 C 2x82 ( < A D 1=4 ACC D4 ) 2A C B D 0 ) B D 1=2 : C D 15=4: 2B D 1 Z 1 dx 4 x 1 2x C ln jxj C 4 2x C

Z Z 15 1 dx dx C 2 x2 4 xC2 1 15 C ln jx C 2j C K: 2x 4

Let u D x 2 and du D 2x dx; then we have Z Z Z du 1 x dx dx D D : I D 2 2 2 2 2 x.x C 4/ x .x C 4/ 2 u.u C 4/2

Since 1 A B C D C C 2 u.u C 4/ u uC4 .u C 4/2 2 2 A.u C 8u C 16/ C B.u C 4u/ C C u D u.u C 4/2 ( ACB D0 1 1 ; BD ; C D ) 8A C 4B C C D 0 ) A D 16 16 16A D 1 therefore Z Z Z 1 1 1 du du du I D 32 u 32 uC4 8 .u C 4/2 ˇ ˇ 1 ˇˇ u ˇˇ 1 1 D ln C CC 32 ˇ u C 4 ˇ 8 u C 4 ˇ ˇ 1 1 ˇˇ x 2 ˇˇ ln C C: C D 32 ˇ x 2 C 4 ˇ 8.x 2 C 4/ Copyright © 2018 Pearson Canada Inc.

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INSTRUCTOR’S SOLUTIONS MANUAL

53.

Z

REVIEW EXERCISES ON TECHNIQUES OF INTEGRATION (PAGE 390)

sin.2 ln x/ dx x

therefore

Let u D 2 ln x 2 du D dx x Z 1 1 D cos u C C sin u du D 2 2 1 D cos.2 ln x/ C C: 2

I D

Z

8x xC 2 x

1 x2 C 4C p D 2 7 D

54. Since Z

sin.ln x/ dx x2

57.

dx dV D 2 U D sin.ln x/ x cos.ln x/ 1 dx dU D V D x x Z cos.ln x/ sin.ln x/ dx C D x x2 dx U D cos.ln x/ dV D 2 x sin.ln x/ 1 dU D dx V D x x sin.ln x/ cos.ln x/ D I; x x

58.

I D

i 1 h sin.ln x/ C cos.ln x/ C C: 2x

55.

1

e 2 tan x dx 1 C x2

Let u D 2 tan 1 x 2 dx du D 1 C x2 Z 1 1 1 e u du D e u C C D e 2 tan D 2 2 2

1

x

C C:

61. I D

Z

x3 C x 2 dx D x2 7 D

Z

Z

x3

7x C 8x 2 dx x2 7 ! 8x 2 dx: xC 2 x 7

Since p B .A C B/x C .B A/ 7 2 A p C p D D 7 x2 7 xC 7 x 7 ( ACB D8 1 1 ) B A D p2 ) A D 4 C p ; B D 4 p ; 7 7 7

8x x2

!Z !

x

1 p ln jx 7

dx p

7

p

7j C C:

Let u D ln.3 C x 2 / 2x dx du D 3 C x2 Z 2 u2 1 1 u du D CC D ln.3 C x 2 / C C: D 2 4 4 Z Z cos7 x dx D .1 sin2 x/3 cos x dx Let u D sin x du D cos x dx Z Z u2 /3 du D

.1

u3 C 53 u5

.1

3u2 C 3u4

u6 / du

1 7 7u C C 3 sin5 x 71 5

sin7 x C C: D sin x sin3 x C Z sin 1 .x=2/ dx Let u D sin 1 .x=2/ .4 x 2 /1=2 dx dx du D p D p 2 2 1 .x =4/ 4 x2 Z   2 2 u 1 D u du D CC D sin 1 .x=2/ C C: 2 2

We have Z Z tan4 .x/ dx D tan2 .x/Œsec2 .x/ 1 dx Z Z D tan2 .x/ sec2 .x/ dx Œsec2 .x/ 1 dx D

56. We have

!

1 p 7

ln.3 C x 2 / x dx 3 C x2

Du

60. Z

Z

D

59.

therefore

dx p C 4 xC 7

p 1 x C 4 C p ln jx C 7j C 4 2 7 2

I D

! 2 dx 7 !Z

1 tan3 .x/ 3

1 tan.x/ C x C C: 

Z

.x C 1/ dx p 2 Z x C 6x C 10 .x C 3 2/ dx D p Let u D x C 3 .x C 3/2 C 1 du D dx Z .u 2/ du p D u2 C 1 Z p du D u2 C 1 2 p Let u D tan  u2 C 1 du D sec2  d Z p D x 2 C 6x C 10 2 sec  d p D x 2 C 6x C 10 2 ln j sec  C tan  j C C   p p D x 2 C 6x C 10 2 ln x C 3 C x 2 C 6x C 10 C C:

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p

ADAMS and ESSEX: CALCULUS 9

p

x 2 C6xC10

x



 1

63.

Z

e x .1

Z

p x 3 dx Let x D 2 tan  p .x 2 C 2/7=2 dx D 2 sec2  d p Z p 3 2 2 tan  2 sec2  d D p 7 Z 8 2 sec  1 sin3  cos2  d D p 2 2Z 1 D p .1 cos2  / cos2  sin  d Let u D cos  2 2  sin  d  5 du3 D Z 1 u 1 u 4 2 CC D p .u u / du D p 3 2 20 2 2 5 !5 !3 1 p p 1 @1 1 2 2 ACC D p p p 3 2 2 5 2 C x2 2 C x2 2 5.2 C x 2 /5=2

260

2

1 C C: 3.2 C x 2 /3=2

! Z 3 1 1C 2 dx D dx 2x 2 3 2 2x 3 ! p Z 1 x 3 1 p p dx D C p p 2 4 2x 3 2x C 3 ˇ ˇ p ˇ p p x 3 ˇˇ 2x 3ˇ D C p ln ˇ p p ˇ C C: ˇ 2 4 2 2x C 3 ˇ

64.

Z

65.

Z

e 2x /5=2 dx

Let e x D sin u e x dx D cos u du  3 Z Z 1 D cos6 u du D .1 C cos 2u/3 du 2 Z 1 D .1 C 3 cos 2u C 3 cos2 2u C cos3 2u/ du 8 Z 3 3 u sin 2u C .1 C cos 4u/ duC D C 8 16 16 Z 1 .1 sin2 2u/ cos 2u du 8 5u 3 3 sin 2u D C sin 2u C sin 4u C 16 16 64 16 1 3 sin 2u C C 48 5 1 D sin 1 .e x / C sinŒ2 sin 1 .e x /C 16 4 1 3 1 x sinŒ4 sin .e / sin3 Œ2 sin 1 .e x / C C 64 48 5 1 p D sin 1 .e x / C e x 1 e 2x 16 2   3 xp C e 1 e 2x 1 2e 2x 16 3=2 1 3x  e 1 e 2x C C: 6

D

p

Fig. RT-63

Fig. RT-61

62.

2Cx 2

xC3

66.

x2

x 1=2 dx Let x D u6 1 C x 1=3 dx D 6u5 du Z 8 u D6 du u2 C 1 Z 8 u C u6 u6 u4 C u4 C u2 u2 1 C 1 du D6 u2 C 1  Z  1 D6 du u6 u4 C u2 1 C 2 u C1   7 u5 u3 u C u C tan 1 u C C D6 7 5 3 p 6 6 5=6 D x 7=6 x C 2 x 6x 1=6 C 6 tan 1 x 1=6 C C: 7 5

We have Z

dx x.x 2 C x C 1/1=2 Z dx D 1 2 xŒ.x C 2 / C 43 1=2 p

p 1 3 Let x C D tan  2 p2 3 sec2  d dx D 2

3 sec2  d 2 D p    p 3 3 1 tan  sec  2 2 2 Z Z d 2 sec  d D2 p p D 3 tan  1 3 sin  cos  Z p 3 sin  C cos  d D2 3 sin2  cos2  Z p Z cos  d sin  d D2 3 C 2 2 2 2  3 sin  cos 3 sin  cos2  Z p Z sin  d cos  d D2 3 C2 3 4 cos2  4 sin2  1 Let u D cos  , du D sin  d in the first integral; Z

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INSTRUCTOR’S SOLUTIONS MANUAL

REVIEW EXERCISES ON TECHNIQUES OF INTEGRATION (PAGE 390)

let v D sin  , dv D cos  d in the second integral. Z p Z du dv C 2 D 2 3 3 4u2 4v 2 1 p Z Z 3 1 du du D 3 1 2 2 2 u v2 4 p ˇ ˇ 4 ˇ ˇ p    ˇ cos  C 3 ˇ ˇ ˇ 3 1 2 2 p ln ˇˇ p ˇˇ D 2 2 3 3ˇ ˇ ˇ cos  ˇ 2 ˇ ˇ 1ˇ ˇ   ˇ sin  C ˇ 1 1 ˇ 2 ˇˇ C C .2/ ln ˇ 1ˇ ˇ 2 2 ˇ sin  ˇ 2 ˇ p  ˇ ˇ 1 ˇˇ 3 ˇ cos  sin  ˇ 1 ˇˇ 2 2 ˇ p  D ln ˇ   ˇ C C: ˇ 2 ˇ ˇ cos  C 3 sin  C 1 ˇ ˇ 2 2 ˇ

69.

70.

p 3 2x C 1 and cos  D p , Since sin  D p 2 x2 C x C 1 2 x2 C x C 1 therefore Z

67.

68.

ˇ ˇ p 1 ˇˇ .x C 2/ 2 x 2 C x C 1 ˇˇ dx D ln ˇ p ˇCC: 2 ˇ .x C 2/ C 2 x 2 C x C 1 ˇ x.x 2 C x C 1/1=2

71.

Z

1Cx p dx Let x D u2 1C x dx D 2u du Z u.1 C u2 / du D2 1Cu Z 3 u C u2 u2 u C 2u C 2 2 D2 du 1Cu  Z  2 D2 u2 u C 2 du 1Cu   3 u2 u C 2u 2 ln j1 C uj C C D2 3 2 p p 2 D x 3=2 x C 4 x 4 ln.1 C x/ C C: 3

Z D D D D

x dx Let u D x 2 4x 4 C 4x 2 C 5 du D 2x dx Z 1 du 2 4u2 C 4u C 5 Z 1 du Let w D 2u C 1 2 .2u C 1/2 C 4 dw D 2du Z w dw 1 1 D tan 1 CC 2 4 w C4 8 2   1 1 tan 1 x 2 C C C: 8 2

72.

Z

x dx Let u D x 2 4 .x 2 4/2 du D 2x dx Z 1 1 du D D CC 2 u2 2u 1 1 D CC D C C: 2.x 2 4/ 2x 2 8

Use the partial fraction decomposition A Bx C C 1 D C 2 x3 C x2 C x x x CxC1 A.x 2 C x C 1/ C Bx 2 C C x D x3 C x2 C x ( ACB D0 ) A C C D 0 ) A D 1; B D 1; C D 1: AD1 Therefore, Z dx x3 C x2 C x Z Z xC1 dx dx Let u D x C 21 D x x2 C x C 1 du D dx Z u C 12 D ln jxj du u2 C 43    2x C 1 1 1  2 C C: ln x C x C 1 p tan 1 p D ln jxj 2 3 3 Z

1

x dx

U D tan 1 x d V D x 2 dx dx x3 dU D V D 1 C x2 3 Z x3 1 x 3 dx 1 D tan x 3 3 1 C x2 Z 3 3 x Cx x 1 x tan 1 x dx D 3 3 x2 C 1 x3 1 2 1 D tan 1 x x C ln.1 C x 2 / C C: 3 6 6 Z e x sec.e x / dx Let u D e x du D e x dx Z D

73.

x 2 tan

sec u du D ln j sec u C tan uj C C

D ln j sec.e x / C tan.e x /j C C: Z x 2 dz dx Let z D tan ; dx D I D 4 sin x 3 cos x 2 1 C z2 2z 1 z2 ; sin x D cos x D 1 C z2 1 C z2 2 dz Z 1 C z2 D 8z 3 3z 2 2 1 C z2 Z Z1Cz dz dz D2 D2 : 2 3z C 8z 3 .3z 1/.z C 3/

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.3z

Thus

74.

75.

1 A B D C 1/.z C 3/ 3z 1 zC3 Az C 3A C 3Bz B D .3z 1/.z C 3/  n A D 3=10 A C 3B D 0 ) ) B D 1=10: 3A B D 1 Z Z 3 dz dz 1 I D 5 3z 1 5 zC3 1 1 D ln j3z 1j ln jz C 3j C C 5 ˇ 5 ˇ 1 ˇ 3 tan 1 .x=2/ 1 ˇˇ C C: D ln ˇˇ 5 tan 1 .x=2/ C 3 ˇ

Z

dx x 1=3 1

D

3 1=3 .x 2

Let x D .u C 1/3 dx D 3.u C 1/2 du ! Z Z 1 .u C 1/2 uC2C D3 du D 3 du u u ! u2 C 2u C ln juj C C D3 2

Z

1/2 C 6.x 1=3

dx tan x C sin x Z cos x dx D sin x.1 C cos x/

1/ C 3 ln jx 1=3

Let z D tan.x=2/; 1 z2 ; cos x D 1 C z2

77.

dx D

1 z 2 2 dz 1 C z2 1 C z2 D   1 z2 2z 1 C 1 C z2 1 C z2 Z Z 2 .1 z / dz 1 z2 1 D D dz z.1 C z 2 C 1 z 2 / 2 z 1 z2 D ln jzj CC 2 4 ˇ ˇ xˇ 1  x 2 1 ˇ tan C C: D ln ˇtan ˇ 2 2 4 2 Remark: Since

x sin2 x 2 D 1 cos x ; tan2 D x 2 1 C cos x 2 cos 2 the answer can also be written as ˇ ˇ 1 ˇˇ 1 cos x ˇˇ 1 1 cos x ln ˇ  C C: 4 1 C cos x ˇ 4 1 C cos x

p

D

1 4

D

1j C C:

2 dz 1 C z2 2z sin x D 1 C z2

Z

D

78.

Z

262

76.

79.

Z

ADAMS and ESSEX: CALCULUS 9

x dx

3 Z

4x

4x 2

u 1 p 4 u2 1p 4 u2 4 1p 3 4x 4

D

Z

du 1 sin 4 4x 2

p 4 1

x dx

u 2

1 sin 4

.2x C 1/2

CC 1

1 xC 2

!

Let u D 2x C 1 du D 2 dx

C C:

p

x dx Let x D u2 1Cx dx D 2udu  Z Z 1 u2 du du D 2 1 D2 1 C u2 1 C u2  p p D 2 u tan 1 u C C D 2 x 2 tan 1 x C C: Z p 1 C e x dx Let u2 D 1 C e x 2u du D e x dx! Z Z 2 2 2u du D du 2C 2 D u2 1 u 1 ! Z 1 1 D 2C du u 1 uC1 ˇ ˇ ˇu 1ˇ ˇCC D 2u C ln ˇˇ u C 1ˇ ˇp ˇ ˇ 1 C ex 1 ˇ p ˇ ˇ x D 2 1 C e C ln ˇ p ˇ C C: ˇ 1 C ex C 1 ˇ

I D

Z

x 4 dx D x3 8

Z  xC

8x

x3

8



dx:

8x A Bx C C D C 2 x3 8 x 2 x C 2x C 4 Ax 2 C 2Ax C 4A C Bx 2 2Bx C C x D x 3 8( ( ACB D0 BD A ) 2A 2B C C D 8 ) C D 2A 6A D 8 4A 2C D 0 Thus A D 4=3, B D

2C

4=3, C D 8=3. We have

Z Z dx x 2 4 4 x2 C dx 2 3 x 2 3 x 2 C 2x C 4 Z x2 4 4 xC1 3 D C ln jx 2j dx 2 3 3 .x C 1/2 C 3 x2 4 2 D C ln jx 2j ln.x 2 C 2x C 4/ 2 3 3 4 xC1 C p tan 1 p C K: 3 3

I D

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INSTRUCTOR’S SOLUTIONS MANUAL

OTHER REVIEW EXERCISES 6 (PAGE 391)

80. By the procedure used in Example 4 of Section 7.1, Z e x cos x dx D 21 e x .sin x C cos x/ C C; Z e x sin x dx D 12 e x .sin x cos x/ C C: Now

Z

3.

Z

csc x dx D lim

c!0C

0

c!0C

xe x cos x dx

Z

1

dx D lim R!1 x C x3

1

D 12 xe x .sin C cos x/ D

1 xe 2

.sin x C cos x/

1 x e 2

sin x C C:

5.

Z

D

1.

h

d x e .ax C b/ cos x C .cx C d / sin x dx h D e x .ax C b/ cos x C .cx C d / sin x C a cos x C c sin x i .ax C b/ sin x C .cx C d / cos x h  D e x .a C c/x C b C a C d cos x   i C .c a/x C d C c b sin x

If a C c D 1, b C a C d D 0, c a D 0, and d C c b D 0, then a D c D d D 1=2 and b D 0. Thus Z i ex h x cos x C .x 1/ sin x C C: I D xe x cos x dx D 2 If a C c D 0, b C a C d D 0, c a D 1, and d C c b D 0, then b D c D a D 1=2 and d D 0. Thus Z i ex h J D xe x sin x dx D x sin x .x 1/ cos x C C: 2 2.

Z

1

xr e

0

D lim

c!0C R!1

x

Z

xr e

x

d V D e x dx dr V D e x ˇR Z 1 ˇ ˇ D lim x r e x ˇ C r x r 1 e x dx c!0C ˇ 0 R!1 c Z 1 r c D lim c e C r x r 1 e x dx c!0C

p

Z

6.

Z

0



dx

u.2 ln u/2u du

0

Z

1

u2 ln u du

0

4 lim c 3 ln c 3 c!0C

1

p

dx

x 1

Therefore

7.

8.

Z

x2

>

1 1

Z

p

4 .1 9

1 0

4 9

dx D 1 (diverges) x

dx

x 1

c3/ D

x2

diverges:

Z 1 Z 1 dx D I1 C I2 C p x D xe 1 0 0 Z 1 Z 1 dx dx I1 D p x < p D2 xe x 0 0 Z 1 Z 1 dx 1 e x dx D I2 D p x < e xe 1 1 Thus I converges, and I < 2 C .1=e/. I D

Z

1

R 60

Volume =

0

T6 D

0

because limR!1 Rr e R D 0 for any r. In order to ensure that limc!0C c r e c D 0 we must have limc!0C c r D 0, so we need r > 0.

x 1 C x2

Let x D u2 dx D 2u du

x ln x dx

1

D

dx

1

1 x

c

c

U D xr d U D rx r

1



U D ln u d V D u2 du du u3 dU D V D u 3 0 1 ˇ1 Z 1 ˇ u3 1 ˇ D 4 lim @ ln uˇ u2 duA ˇ c!0C 3 3 c

dx R

1

D4

i

R

ˇˇR 1 ˇ 2 ln.1 C x / ˇ ˇ R!1 2 1   ln 2 R2 1 C ln 2 D ln D lim R!1 2 1 C R2 2

0

Other Review Exercises 6 (page 391)

Z

 D lim ln jxj

d V D e x cos x dx V D 21 e x .sin x C cos x/ Z D 21 xe x .sin C cos x/ 12 e x .sin x C cos x/ dx U Dx d U D dx

cos x C sin x C cos x/ C C

c

D lim ln j csc c C cot cj D 1 (diverges)

4.

1 x 4 e .sin x x

ˇ=2 ˇ ˇ ln j csc x C cot xjˇ ˇ

=2

A.x/ dx. The approximation is

10 h 10; 200 C 2.9; 200 C 8; 000 C 7; 100 2 i C 4; 500 C 2; 400/ C 100

 364; 000 m3 .

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9.

S6 D

ADAMS and ESSEX: CALCULUS 9

10 h 10; 200 C 4.9; 200 C 7; 100 C 2; 400/ 3 i C 2.8; 000 C 4; 500/ C 100

Integrating both sides over Œ0; 1 leads at once to Z

3

10.

 367; 000 m Z 1p 2 C sin.x/ dx I D 0 h p p 1 p 2 C 2. 2 C sin.=4/ C 2 C sin.=2/ T4 D 8 p p i C 2 C sin.3=4/ C 2

0

13.

Z

Thus I > .22=7/

4T8

T4 D 5:504. 3 c) Yes, S4 D S8 suggests that Sn may be independent of n, which is consistent with a polynomial of degree not exceeding 3.

1

(page 391)

22 7

:

 > I =2, or

22 7

c) I D

R1 0

.x 8

a) In D

Z

I : x2 C 1 2

0

22 7

I : 2

4x 5 C x 4 / dx D

1 22 0, then we have

ˇ1 x.1 x 2 /n ˇˇ 2n Jn Jn D ˇ C 2n C 1 ˇ 2n C 1

1

D

2n Jn 2n C 1

Therefore, 1.

a) Long division of x 2 C 1 into x 4 .1 x/4 D x 8 4x 7 C 6x 6 4x 5 C x 4 yields x 4 .1 x/4 D x6 x2 C 1

264

4x 5 C 5x 4

4x 2 C 4

dx

D x.1 x 2 /n 2nIn C 2nIn 1 ; so 2n 1 x.1 x 2 /n C In 1 : In D 2n C 1 2n C 1 Z 1 b) Let Jn D .1 x 2 /n dx. Observe that J0 D 1. By

0

Challenging Problems 6

1D

0

T8 D

b) If T8 D 5:5095, then S8 D

1

on .0; 1/, we have I >

1 .T4 C M4 /  1:617996 2 1 S8 D .T4 C 2M4 /  1:62092 3 I  1:62 Z 1 x2 dx Let x D 1=t I D 5 3 1=2 x C x C 1 dx D .1=t 2 / dt Z 2 Z 2 4 t dt .1=t / dt D D 5 / C .1=t 3 / C 1 5 C t2 C 1 .1=t t 0 0 T4  0:4444 M4  0:4799 T8  0:4622 M8  0:4708 S8  0:4681 S16  0:4680 I  0:468 to 3 decimal places   0:730 2:198 C 1:001 C 1:332 C 1:729 C a) T4 D 1 2 2 D 5:526   1 S4 D 0:730 C 2:198 C 4.1:001 C 1:729/ C 2.1:332/ 3 D 5:504:

4tan

x 4 .1 x/4 22 > 0 on .0; 1/,  > 0, and so x2 C 1 7 22 . < 7 Z 1 x 4 .1 x/4 dx, then since 1 < x 2 C 1 < 2 b) If I D

 1:626765 I  1:6

12.

x 4 .1 x/4 22 dx D x2 C 1 7

Since

 1:609230 p 1 hp M4 D 2 C sin.=8/ C 2 C sin.3=8/ 4 i p p 2 C sin.5=8/ C 2 C sin.7=8/

11.

1

2n 2n 2 4 2      J0 2n C 1 2n 1 5 3 Œ.2n/.2n 2/    .4/.2/2 22n .nŠ/2 D D : .2n C 1/Š .2n C 1/Š

Jn D

4 : x2 C 1

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INSTRUCTOR’S SOLUTIONS MANUAL

CHALLENGING PROBLEMS 6 (PAGE 391)

c) From (a):

5.

In

1

D

2n C 1 In 2n

1 x.1 2n

x 2 /n :

Thus Z

x2/

.1

3=2

dx D I

2. 1=2/ C 1 I 1 x : D p 1 x2 D

3.

1=2

3=2

1 x.1 1

x2/

1=2

4.

Im;n D D

Z

m

n

x .ln x/ dx 1

e

0

D . 1/n

mt

Z

. t /n e

1 0

t ne

t

D nIn

Let u D .m C 1/t du D .m C 1/ dt

Z 1 . 1/n un e u du .m C 1/n 0 . 1/n €.n C 1/ (see #50 in Section 7.5) D .m C 1/n . 1/n nŠ D : .m C 1/n

1

x n dx D

if n  1 0

In D nŠ @1

1 n 1X 1 A e jŠ j D0

holds for n D 0 by part (b). Assume that it holds for some integer n D k  0. Then by (b), 0 1 k X 1 1 1 A 1 D .k C 1/kŠ @1 IkC1 D .k C 1/Ik e e jŠ e j D0 0 1 k X 1 1 1 A D .k C 1/Š @1 e j Š e.k C 1/Š j D0 1 0 kC1 X 1 1 A: D .k C 1/Š @1 e jŠ j D0

Thus the formula holds for all n  0, by induction. d) Since limn!1 In D 0, we must have 0 1 n 1X 1 A D 0: lim @1 n!1 e jŠ j D0

6. dt

dx
100 100 1 1 D .1 C   / > 300 300 1 1 .e K=200 C   / < : D 100 100

T100 D S100 M100

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CHALLENGING PROBLEMS 6 (PAGE 391)

ADAMS and ESSEX: CALCULUS 9

In each case the    represent terms much less than the first term (shown) in the sum. Evidently M100 is smallest if k is much greater than 100, and is therefore the best approximation. T100 appears to be the worst. 7.

8.

a) f 0 .x/ < 0 on Œ1; 1/, and limx!1 f .x/ D 0. Therefore Z

a) Let f .x/ D Ax 5 C Bx 4 C C x 3 C Dx 2 C Ex C F . Then  5  Z h Bh Dh3 C C Fh : f .x/ dx D 2 5 3 h

1

2a C

2b 1 D ; 4 3

16 C e 45

C

7 3=4 C e 90

1

2 e 15 #

ˇZ ˇ ˇ ˇ

7 e 45 2 5=8 C e 15 3=8

C

b)

Z

1

R

Z

R

jf 0 .x/j dx ! 0 as R ! 1:

f 0 .x/ cos x dx exists.

f .x/ sin x dx

1

1

the integral converges.

c) f .x/ D 1=x satisfies the conditions of part (a), so Z

1 1

sin x dx x

converges

by part (b). Similarly, it can be shown that

1=2

Z

1

1

Z

cos.2x/ dx x

converges:

16 e 45

7=8

C

7 e 90

1

#

1 1

j sin xj dx  x

Z

1 1

cos.2x//, we have 1

cos.2x/ : 2x

R1 The latter integral diverges R 1 because 1 .1=x/ dx diverges to infinity while 1 .cos.2x//=.2x/ dx converges. Therefore

 0:63212055883:

266

1

But since j sin xj  sin2 x D 12 .1

C

f .R// D f .1/:

U D f .x/ d V D sin x dx d U D f 0 .x/ dx V D cos x ˇR Z ˇ 1 ˇ D lim f .x/ cos x ˇ C f 0 .x/ cos x dx ˇ R!1 1 1 Z 1 D f .1/ cos.1/ C f 0 .x/ cos x dxI

1=2

3=4

R

ˇ Z ˇ f .x/ cos x dx ˇˇ  0

R!1 1

With two intervals having h D 1=4 and m D 1=4 and m D 3=4, we get " Z 1 1 7 0 16 1=8 2 x e dx  e C e C e 1=4 2 90 45 15 0 16 e 45 16 C e 45

1

Thus lim

 0:63212087501:

C

R!1 1

Thus

Solving these equations, we get a D 7=90, b D 16=45, and c D 2=15. The approximation for the integral of any function f on Œm h; m C h is " Z mCh 7 16 f .x/ dx  2h f .m h/ C f .m 21 h/ 90 45 m h # 16 7 2 1 C f .m/ C f .m C 2 h/ C f .m C h/ : 15 45 90

1=4

f 0 .x/ dx Z R lim f 0 .x/ dx 1

R!1

2a C 2b C c D 1:

b) If m D h D 1=2, we obtain " Z 1 7 0 16 x e dx  1 e C e 90 45 0

1

D lim .f .1/

These expressions will be identical if the coefficients of like powers of h on the two sides are identical. Thus 1 2b D ; 16 5

Z

jf 0 .x/j dx D D

Also h i 2h af . h/ C bf . h=2/ C cf .0/ C bf .h=2/ C af .h/   D 2 a 2Bh5 C 2Dh3 C 2F    2Bh5 2Dh3 Cb C C 2F C cF h : 16 4

2a C

1

Z

1 1

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j sin xj dx x

diverges to infinity.

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 7.1 (PAGE 401)

CHAPTER 7. APPLICATIONS OF INTEGRATION

3.

By slicing:

Section 7.1 Volumes by Slicing—Solids of Revolution (page 401) 1.

Z

V D

V D

1

D

V D 2 D 2

x2 2

By shells:

 cu. units. x dx D 5

x 4 / dx ˇ1 x 5 ˇˇ 3 cu. units. ˇ D 5 ˇ 10 0

4

0

V D 2

By shells: Z

.x 0



By slicing: Z

1

1

y.1

y/ dy !ˇ1 2y 5=2 ˇˇ  cu. units. ˇ D ˇ 5 5

y2 2

1

p y. y

0

2y 5=2 5

D 2

p

0

Z

0

y

p yD x

0

y

y 2 / dy !ˇ1 y 4 ˇˇ 3 cu. units. ˇ D 4 ˇ 10

.1;1/

yDx 2

yDx 2

x

x

x

x

Fig. 7.1-3 4.

Fig. 7.1-1

Slicing:

2. Slicing: V D

Z

V D

1

.1 0

 D y Shells: V D 2

y/ dy ˇ1 1 2 ˇˇ  y ˇ D cu: units: ˇ 2 2 0

Z

1

3

x dx 0  4  ˇˇ1  x ˇ cu: units: D 2 ˇ D ˇ 4 2

Z

D



V D 2

Z

1

.y 0

1 2 y 2

Shells:

D 2

0



y

1

y 4 / dy ˇ1 1 5 ˇˇ 3 y ˇ D cu: units: ˇ 5 10 0

x.x 1=2

0

2 5=2 x 5

x 2 / dx ˇ1 1 4 ˇˇ 3 x ˇ D cu: units: ˇ 4 10 0

y

.1;1/ p yD x yDx 2

yDx 2

1 x

x

Fig. 7.1-4

Fig. 7.1-2

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267

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SECTION 7.1 (PAGE 401)

ADAMS and ESSEX: CALCULUS 9

y

5. a) About the x-axis:

.1;1/

V D D D

Z

2

x 2 .2

x/2 dx

yDx

0

Z

2

.4x 2

0



yDx 2

4x 3 C x 4 / dx ˇ2 16 x 5 ˇˇ 4 x C cu. units. ˇ D 5 ˇ 15

4x 3 3

x

Fig. 7.1-6

0

b) About the y-axis:

7. V D 2 D 2

Z

2

x 2 .2

0



2x 3 3

x/ dy ˇ2 x 4 ˇˇ 8 cu. units. ˇ D ˇ 4 3

a) About the x-axis: V D 2

3

y 2 y/ dy ˇ3 27 y 4 ˇˇ cu. units. ˇ D 4 ˇ 2

y.4y

0

 D 2 y 3

0

y

(a)

Z

0

b) About the y-axis:

yD2x x 2

Z 3h i .4y y 2 /2 y 2 dy 0 Z 3 D .15y 2 8y 3 C y 4 / dy 0  ˇ3 y 5 ˇˇ 108 D  5y 3 2y 4 C cu. units. ˇ D 5 ˇ 5

V D 2 x

0

y

y

(b)

yD2x x 2

.3;3/ xDy

2 x

xD4y y 2

Fig. 7.1-5

x

6. Rotate about Fig. 7.1-7

a) the x-axis V D D

Z



1

.x 2

0

1 3 x 3

b) the y-axis V D 2 D 2

268

Z



x 4 / dx ˇ1 1 5 ˇˇ 2 x ˇ D cu: units: ˇ 5 15

8.

Rotate about a) the x-axis

0

V D D

1

x.x

0

1 3 x 3

x 2 / dx ˇ1 1 4 ˇˇ  x ˇ D cu: units: ˇ 4 6 0

D



Z

Z

 0  0

Œ.1 C sin x/2

.2 sin x C sin2 x/ dx

 2 cos x C x 2

1 D 4 C  2 cu: units: 2

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1 dx

 sin 2x 4

ˇˇ ˇ ˇ ˇ 0

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 7.1 (PAGE 401)

y

b) the y-axis

.1=3;3/

V D 2

Z



x sin x dx

3xC3yD10

0

U Dx d V D sin x dx d U D dx ˇ V D cos x   ˇ Z  ˇ D 2 x cos x ˇ C cos x dx ˇ 0

1 yD x

x

0

Fig. 7.1-10

D 2 2 cu: units:

9. a) About the x-axis: Z 1 V D 4 0

D 4



D 4



Z

Z

11. 1 .1 C x 2 /2

=4 0 =4



Let x D tan  dx D sec2  d

dx

sec2  d sec4 

.3;1=3/

Z 1 V D 2  2 .2 x/.1 x/ dx 0 Z 1 D 4 .2 3x C x 2 / dx 0 ˇ1  3x 2 x 3 ˇˇ 10 D 4 2x C cu. units. ˇ D 2 3 ˇ 3 0

cos2  d

y

0

ˇ=4 ˇ  . C sin  cos  /ˇˇ D 4 2 0 2  15 2 D 4 D cu. units. 8 4 4 8 b) About the y-axis:  Z 1  1 V D 2 dx x 2 1 C x2 0  ˇˇ1 1 ˇ D 2 x 2 ln.1 C x 2 / ˇ ˇ 2 0   1 ln 2 D 2  ln 2 cu. units. D 2 1 2

y

xCyD1

xD2

x

x

Fig. 7.1-11

12.

V D

Z

1

 D x

y

Œ.1/2

.x 2 /2  dx ˇ1 1 5 ˇˇ x ˇ ˇ 5

1

1

8 cu: units: D 5

yD2

y

yD

1 1Cx 2

yD1 x2 yD1 x 2

x

1

dx

x

x

Fig. 7.1-9 10. By symmetry, rotation about the x-axis gives the same volume as rotation about the y-axis, namely  Z 3  1 10 x dx V D 2 x 3 x 1=3 ˇ  ˇ3 5 2 1 3 ˇ D 2 x x x ˇ ˇ 3 3

Fig. 7.1-12 13.

The volume remaining is V D 2  2

1=3

D

512 cu: units: 81

x

D 2

Z

3

Z

2

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x 2 dx

1

p

0

p x 4

ˇ3 4 3=2 ˇˇ u du D u ˇ ˇ 3 0

Let u D 4 x 2 du D 2x dx p D 4 3 cu. units.

269

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SECTION 7.1 (PAGE 401)

ADAMS and ESSEX: CALCULUS 9

32 4 3 2 D cu. units., 3 3 p 32 4 3 cu. units. therefore the volume removed is 3 The percentage removed is Since the volume of the ball is

p 4 3

32 3

The volume remaining is Z b  V D 2 xh 1

x dx b a ˇ  2 b x x 3 ˇˇ D 2h ˇ 2 3b ˇ a   a3 2 2 2 h b 2 a / D h.b 3 b  3 1 2a D h b 2 3a2 C cu. units. 3 b

p ! 3 3  35: 8

 100 D 100 1

32 3

15.

About 35% of the volume is removed. y

y

p yD 4 x 2

h

dx

1

2 x

x

x y C D1 b h

xDa

dx b x

Fig. 7.1-13

14.

The radius of the hole is the remaining volume is

V D

Z

D 2

L=2 L=2

q

16.

"

L2 x 4

Fig. 7.1-15

1 2 L . 4

R2

R2

x2

1 3 x 3



!ˇL=2 ˇ ˇ ˇ ˇ

 R2

Thus, by slicing,

L2 4

#

dx

0

 D L3 cu. units (independent of R). 6 y

x

Let a circular disk with radius a have centre at point .a; 0/. Then the disk is rotated about the y-axis which is one of its tangent lines. The volume is: Z 2a p V D 2  2 x a2 .x a/2 dx Let u D x a 0 du D dx Z a p 2 2 D 4 .u C a/ a u du Z aa p Z ap u a2 u2 du C 4a D 4 a2 u2 du a a   1 D 0 C 4a a2 D 2 2 a3 cu: units: 2

(Note that the first integral is zero because the integrand is odd and the interval is symmetric about zero; the second integral is the area of a semicircle.)

p yD R2 x 2

y R

q L 2

R2

L2 4

.x a/2 Cy 2 Da2 x

2a a

L

Fig. 7.1-16

Fig. 7.1-14

270

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x

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

17.

Volume of the smaller piece: Z a V D .a2 x 2 / dx b ˇa  x 3 ˇˇ 2 D a x ˇ 3 ˇ b  a3 2 D  a .a b/  D .a 3  D .a 3

b/Œ3a

2

SECTION 7.1 (PAGE 401)

19.

The volume of the ellipsoid is Z

V D 2

b3 3 2

D 2b



a 0

2

 x2 dx a2 ˇa  x 3 ˇˇ 4 ˇ D ab 2 cu. units. 3a2 ˇ 3

 b 1 2



x

0

y

.a C ab C b 2 /

yDb b

b/2 .2a C b/ cu. units.

q

1

x2 a2

y p yD a2 x 2

dx

a

x

dx b

x

a

x

x

Fig. 7.1-19

20. Fig. 7.1-17 18. Let the centre of the bowl be at (0, 30). Then the volume of the water in the bowl is Z 20 h i V D 302 .y 30/2 dy 0 Z 20 D 60y y 2 dy 0  ˇ20 1 3 ˇˇ D  30y 2 y ˇ ˇ 3

V D

Z

D 2

ah

Z aa 0

D 8b

p a2

.b C

p 4b a2

y 2 /2

.b

y 2 dy

p

a2

i y 2 /2 dy

a2 D 2 2 a2 b cu. units.: 4

We used the area of a quarter-circle of radius a to evaluate the last integral.

0

 29322 cm3 : y

The cross-section at height p y is an annulus (ring) having inner radius b a2 y 2 and outer radius p 2 2 bC a y . Thus the volume of the torus is

21.

a) Volume of revolution about the x-axis is V D

Z

1

2x

dx ˇR  e 2x ˇˇ cu. units. D  lim ˇ D R!1 2 ˇ 2

30

20

e

0

0

b) Volume of revolution about the y-axis is x 2 C.y 30/2 D302 x

V D 2 Fig. 7.1-18

Z

1

xe

x

dx

0

D 2 lim . xe R!1

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x

e

x

ˇR ˇ /ˇˇ D 2 cu. units. 0

271

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SECTION 7.1 (PAGE 401)

ADAMS and ESSEX: CALCULUS 9

y

25. 1 x

yDe

dx x

x

The volume os S is still the constant cross-sectional area a2 =2 times the height b, that is, V D a2 b=2 cm3 .

Fig. 7.1-21 26. 22. The volume is

V D

Z

1

x

2k

1

D  lim

R!1

ˇR x 1 2k ˇˇ dx D  lim ˇ R!1 1 2k ˇ 1

 R1 2k C : 1 2k 2k 1

2k < 0;

that is;

k>

Z

8

D 3072

1 : 2

D 3072 D 3072 D 3072

y

27.

k

x.4

x 2=3 /3=2 dx

Z

sin5 u cos4 u du

0

D 3072

R1 23. The volume is V D 2 1 x 1 k dx. This improper integral converges if 1 k < 1, i.e., if k > 2. The solid has finite volume only if k > 2.

yDx

The region is symmetric about x D y so has the same volume of revolution about the two coordinate axes. The volume of revolution about the y-axis is V D 2

In order for the solid to have finite volume we need 1

Since all isosceles right-angled triangles having leg length a cm are congruent, S does satisfy the condition for being a prism given in early editions. It does not satisfy the condition in this edition because one of the line segments joining vertices of the triangular cross-sections, namely the x-axis, is not parallel to the line joining the vertices of the other end of the hypotenuses of the two bases.

Z

Z

Z

=2 0 =2

.1

1

1

1

.v 4

0



1 5

2v 6 C v 8 / dv  2 1 8192 C D cu. units. 7 9 105

4 R3 . Expressing this volume 3 as the “sum” (i.e., integral) of volume elements that are concentric spherical shells having thickness dr and varying radius r, and therefore having surface area kr 2 and volume kr 2 dr, we obtain

The volume of the ball is

4 R3 D 3

Z

R 0

kr 2 dr D

k 3 R : 3

Thus k D 4.

A solid consisting of points on parallel line segments between parallel planes will certainly have congruent crosssections in planes parallel to and lying between the two base planes, any solid satisfying the new definition will certainly satisfy the old one. But not vice versa; congruent cross-sections does not imply a family of parallel line segments giving all the points in a solid. For a counterexample, see the next exercise. Thus the earlier, incorrect definition defines a larger class of solids than does the current definition. However, the formula V D Ah for the volume of such a solid is still valid, as all congruent cross-sections still have the same area, A, as the base region.

272

v 2 /2 v 4 dv

.1

Let v D cos u dv D sin u du

0

x

Fig. 7.1-23

24.

cos2 u/2 cos4 u sin u du

0

dx x

Let x D 8 sin3 u dx D 24 sin2 u cos u du

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R

dr r

Fig. 7.1-27

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 7.1 (PAGE 401)

R D sin ˛, so R D .x C h/ sin ˛. xCh Using the result of Exercise #17, the volume of liquid displaced by the ball is

28. Using heights f .x/ estimated from the given graph, we obtain Z 9 2 V D f .x/ dx 1 h 2 3 C 4.3:8/2 C 2.5/2 C 4.6:7/2 C 2.8/2  3 i C 4.8/2 C 2.7/2 C 4.5:2/2 C 32  938 cu. units.

Note that

V D

 .R 3

x/2 .2R C x/:

We would like to consider V as a function of x for 2R  x  R since V D 0 at each end of this interval, and V > 0 inside the interval. However, the actual interval of values of x for which the above formulation makes physical sense is smaller: x must satisfy R  x  h tan2 ˛. (The left inequality signifies nonsubmersion of the ball; the right inequality signifies that the ball is tangent to the glass somewhere below the rim.) We look for a critical point of V , considered as a function of x. (As noted above, R is a function of x.) We have

29. Using heights f .x/ estimated from the given graph, we obtain Z 9 V D 2 xf .x/ dx 1 h 2 1.3/ C 4.2/.3:8/ C 2.3/.5/ C 4.4/.6:7/ C 2.5/.8/  3 i C 4.6/.8/ C 2.7/.7/ C 4.8/.5:2/ C 9.3/  1537 cu. units.

" dV  0D D 2.R dx 3

30. Using heights f .x/ estimated from the given graph, we obtain Z 9 V D 2 .x C 1/f .x/ dx 1 h 2 2.3/ C 4.3/.3:8/ C 2.4/.5/ C 4.5/.6:7/ C 2.6/.8/  3 i C 4.7/.8/ C 2.8/.7/ C 4.9/.5:2/ C 10.3/  1832 cu. units.

C .R

x/



dR dx

 1 .2R C x/

#  dR C1 x/ 2 dx 2

dR .4R C 2x C 2R dx Thus

2x/ D 4R C 2x

.R

x/:

  R 6R sin ˛ D 3.R C x/ D 3 R C h sin ˛ 2R sin2 ˛ D R sin ˛ C R h sin ˛ h sin ˛ h sin ˛ RD : D cos 2˛ C sin ˛ 1 2 sin2 ˛ C sin ˛

31. Let the ball have radius R, and suppose its centre is x units above the top of the conical glass, as shown in the figure. (Clearly the ball which maximizes liquid overflow from the glass must be tangent to the cone along some circle below the top of the cone — larger balls will have reduced displacement within the cone. Also, the ball will not be completely submerged.)

This value of R yields a positive value of V , and corresponds to x D R.2 sin ˛ 1/. Since sin ˛  sin2 ˛, RxD

h sin ˛.2 sin ˛ 1/ h sin2 ˛ D h tan2 ˛:  2 cos2 ˛ 1 C sin ˛ 2 sin ˛

Therefore it gives the maximum volume of liquid displaced. x R

32.

h h sec ˛ .hCx/ cos ˛ ˛

Let P be the point .t; 25 t /. The line through P perpendicular to AB has equation y D x C 52 2t , and meets the curve xy D 1 at point Q with x-coordinate s equal to the positive root of s 2 C . 52 2t /s D 1. Thus, " 1 2t sD 2

Fig. 7.1-31

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5 C 2

s



5 2

2t

2

#

C4 :

273

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SECTION 7.1 (PAGE 401)

ADAMS and ESSEX: CALCULUS 9

y A.1=2;2/

yD

Section 7.2 More Volumes by Slicing (page 405)

p 2 dt

1 x

P xCyD

Q

5 2

1.

Z

V D

B.2;1=2/

2. s

t

x

The volume element at P has radius p PQ D 2.t s/ 3 2 s 2  p 5 1 5 2t C 45 D 24 4 2 2

3.

and thickness 2 dt . Hence, the volume of the solid is s #2  2 Z 2 "p  p 5 1 5 V D 2 2 dt 2t C 4 4 2 2 1=2 1 0s 2  2 p Z 2 25 5 5 @ 4 2t C 4A C D 2 2 16 4 2 1=2 #  2 1 5 2t C 4 dt Let u D 2t 52 4 2 du D 2!dt p Z 3=2 41 5 p u2 du D 2 u2 C 4 C 4 4 3=2 16 !ˇ3=2 ˇ p 41 1 ˇ D 2 u C u3 ˇ ˇ 16 12 3=2 p Z 3=2 p 5 2 u2 C 4 du Let u D 2 tan v 4 3=2 du D 2 sec2 v dv p Z 1 tan .3=4/ p 33 2 5 2 sec3 v dv D 4 tan 1 . 3=4/ p p Z tan 1 .3=4/ 3 33 2 10 2 sec v dv D 4 0 p p  33 2 5 2 sec v tan vC D 4 ˇ 1 ˇtan .3=4/ ˇ ln j sec v C tan vj ˇ ˇ 0 "  # p 33 15 D 2 5 C ln 2 0 ln 1 4 16   p 57 5 ln 2 cu: units: D 2 16

0

A horizontal slice of thickness dz at height a has volume d V D z.h z/ dz. Thus the volume of the solid is Z

h

Z

V D

1

5.

V D

Z

V D

Z

3 1

p z 1

Z

1

0

z3 3

ˇ ˇh 3 ˇ ˇ D h units3 : ˇ 6 ˇ 0

p

let u

1

z2

ˇ1 ˇ  2 3=2 ˇˇ  u du D u ˇ D units3 : 2 3 3 ˇ

ˇ3 x 3 ˇˇ 26 x dx D cu. units ˇ D 3 ˇ 3 2

1

6

0

.2 C z/.8

Z 6 z/ dz D .16 C 6z 0 ˇ 6  z 3 ˇˇ ˇ D 132 ft3 3 ˇ

z 2 / dz

0

p The area of anequilateral triangle of edge x is p p  p p A.x/ D 21 x 23 x D 43 x sq. units. The volume of the solid is V D

7.

hz 2 2

0

 D 16z C 3z 2

6.

z 2 dz

0

 D 2

4.

z/ dz D

.z.h 0



A horizontal p slice of thickness dz at height a has volume d V D z 1 z 2 dz. Thus the volume of the solid is

p

274

0

V D

Fig. 7.1-32

ˇ2 3 2 ˇˇ 3x dx D x ˇ D 6 m3 2 ˇ

2

Z

4

ˇ4 p p 3 3 2 ˇˇ 15 3 x dx D x ˇ D cu. units. ˇ 4 8 8

p

1

1

The area of cross-section at height y is A.y/ D

2.1

 .y= h// .a2 / D a2 1 2

y sq. units. h

The volume of the solid is V D

Z

0

h

 a2 1

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a2 h y cu. units. dy D h 2

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 7.2 (PAGE 405)

8. Since V D 4, we have 4D

Z

2

0

ˇ2 x 4 ˇˇ kx dx D k ˇ D 4k: 4 ˇ 3

y

0

Thus k D 1.

p

3y x

2y

9. The volume between height 0 and height z is z 3 . Thus Z

z3 D

x 2 Cy 2 Dr 2

z

A.t / dt; 0

Fig. 7.2-12

where A.t / is the cross-sectional area at height t . Differentiating the above equation with respect to z, we get 3z 2 D A.z/. The cross-sectional area at height z is 3z 2 sq. units.

10. This is similar to Exercise 7. We have 4z D

Z

13.

The cross-section at distance y from the vertex of the partial cone is a semicircle of radius y=2 cm, and hence area y 2 =8 cm2 . The volume of the solid is V D

z

A.t / dt ,

0

Z

12 0

123  2 y dy D D 72 cm3 . 8 24

so A.z/ D 4. Thus the square cross-section at height z has side 2 units.

11.

V D2 D8

Z

Z r p 2 r2

0

0

r

.r 2

y2

2

r

z

dy

 y 2 / dy D 8 r 2 y z

p

2

y3 3

y

ˇˇr 16r 3 ˇ cu. units. ˇ D ˇ 3

x

0

.12; 12; 0/ Fig. 7.2-13

r 2 y2

14. y

p

x

12 y

xD

r2

y2

The volume of a solid of given height h and given crosssectional area A.z/ at height z above the base is given by Z h V D A.z/ dz: 0

If two solids have the same height h and the same area function A.z/, then they must necessarily have the same volume.

Fig. 7.2-11

12. The area triangle of base 2y is p of an equilateral p 2 1 3y . Hence, the solid has volume 2 .2y/. 3y/ D V D2

Z

r 0

p

3.r 2

 p D 2 3 r 2x

x 2 / dx ˇr 1 3 ˇˇ x ˇ ˇ 3 0

4 D p r 3 cu: units: 3

15.

Let the x-axis be along the diameter shown in the figure, with the origin at the centre of the base. The cross-section perpendicular to the x-axis at x is a rectangle having base p aCb a b C x: Thus the 2 r 2 x 2 and height h D 2 2 volume of the truncated cylinder is V D D

Z

Z

r r r r

p .2 r 2

x2/

p .a C b/ r 2

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 aCb a b C x dx 2 2r 2  r .a C b/ cu. units. x 2 dx D 2

275

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SECTION 7.2 (PAGE 405)

ADAMS and ESSEX: CALCULUS 9

17.

Cross-sections of the wedge removed perpendicular to the x-axis are isosceles, right triangles. The volume of the wedge removed from the log is Z

1 p . 400 x 2 /2 dx 2 0 ˇ20  16; 000 x 3 ˇˇ cm3 : D 400x ˇ D ˇ 3 3

V D2 h

20

0

x y

yD

p

x

r x2

r2

z

Fig. 7.2-15 16. The plane z D k meets the ellipsoid in the ellipse  2 k a b c 2 y2 x "  2 # C "  2 # D 1 k k 2 2 a 1 b 1 c c  x 2

that is,

C

 y 2

D1

45ı 20 x x

Fig. 7.2-17

which has area "

A.k/ D ab 1

 2 # k : c

The volume of the ellipsoid is found by summing volume elements of thickness d k:

18. The solution is similar to that of Exercise 15 except that the legs of the right-triangular cross-sections are y 10 p p instead of y, and x goes from 10 3 to 10 3 instead of 20 to 20. The volume of the notch is V D2

 2 # c k dk V D ab 1 c c #ˇc " 1 3 ˇˇ k ˇ D ab k ˇ 3c 2 Z

"

D

c

x2 a2

C

y2 b2

C

A.k/

y

x2

500

x2

10/2 dx

p 20 400

 x 2 dx

4; 000  1; 007 cm3 : 3

20.

One eighth of the region lying inside both cylinders is shown in the figure. If the region is sliced by a horizontal plane at height z, then the intersection is a rectangle with area p p A.z/ D b 2 z 2 a2 z 2 :

z2 D1 c2

k

b

0 p 10 3 

1 p . 400 2

The hole has the shape of two copies of the truncated cylinder of Exercise 15, placed base to base, p with a C b D 3 2 in and r D 2 in. Thus the volume of wood p volume of the hole) is p removed (the V D 2.22 /.3 2=2/ D 12 2 in3 .

(one-eighth of the solid is shown)

a

0

p 10 3

19.

z

c

Z

Z

p D 3; 000 3

4 D abc cu: units: 3

The volume of the whole region is

x

V D8

Fig. 7.2-16

276

y

p yD 400 x 2

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Z

0

b

p

b2

p z 2 a2

z 2 dz:

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 7.3 (PAGE 412)

z

5.

b z

p b2 z 2

A.z/p a2 z 2 a

y

6.

x

Fig. 7.2-20 21.

By the result given in Exercise 18 with a D 4 cm and b D 2 cm, the volume of wood removed is Z

V D8

2

p

z2

4

p

z 2 dz  97:28 cm3 :

16

0

(We used the numerical integration routine in Maple to evaluate the integral.)

7.

Section 7.3 Arc Length and Surface Area (page 412)

y D x 2=3 ; r

y0 D

2 x 3

1=3

; p 9x 2=3 C 4 4 2=3 dx D ds D 1 C x dx 9 3jxj1=3 p Z 1 9x 2=3 C 4 dx Let u D 9x 2=3 C 4 LD2 3x 1=3 0 du D 6x 1=3 dx Z 13 3=2 p 1 2.13 / 16 units. D u du D 9 4 27 q 2.x C 1/3 D 3.y 1/2 ; y D 1 C 23 .x C 1/3=2 q y 0 D 32 .x C 1/1=2 ; r r 3x C 5 3x C 3 ds D 1 C dx D dx 2 2 ˇ0 p Z 0 ˇ p 2 1 3=2 ˇ 3x C 5 dx D .3x C 5/ ˇ LD p ˇ 9 2 1 1 p   2 3=2 5 23=2 units. D 9 1 x2 1 x3 C ; y0 D 2 12 x 4 x s 2   2  2 x x 1 1 ds D 1 C dx dx D C 4 x2 4 x2 ˇ   3 4 Z 4 2 x 1 1 ˇˇ x C 2 dx D LD ˇ D 6 units. 4 x 12 x ˇ 1 yD

1

1.

y D 2x 1; y 0 D 2; ds D Z 3p p LD 5 dx D 2 5 units.

p

1 C 22 dx

8.

1

2. y D ax C b, A  x  B, y 0 D a. The length is LD

3.

Z

B

A

p

1 C a2 dx D

p 1 C a2 .B

9.

0

4.

3p y 2 D .x 1/3 ; y D .x 1/3=2 ; y 0 D x 1 2 Z 2p Z 2r 1 9 LD 1 C .x 1/ dx D 9x 5 dx 4 2 1 1 ˇ2 ˇ 133=2 8 1 ˇ .9x 5/3=2 ˇ D units. D ˇ 27 27

1 4x 2  2  1 1 2 dx D x C dx 4x 2 4x 2 ˇ 2   3 Z 2 1 ˇˇ 59 x 1 units. LD x 2 C 2 dx D ˇ D 4x 3 4x ˇ 24 1 y 0 D x2

1

A/ units.

p p y D 32 x 3=2 ; y 0 D x; ds D 1 C x dx ˇ8 Z 8 ˇ p 52 2 3=2 ˇ units. LD 1 C x dx D .1 C x/ ˇ D ˇ 3 3 0

1 x3 C ; 3 4x s  ds D 1 C x 2 yD

x2 1 x ; y0 D 4 2x 2     1 1 x 2 x ds D 1 C dx D C dx 2x 2 2x 2 ˇ   e Z e x ln x x 2 ˇˇ 1 C C dx D LD ˇ 2x 2 2 4 ˇ 1 yD

ln x s2

1

1 e2 1 e2 C 1 D C D units. 2 4 4

10. If y D x 2

1

ln x then y 0 D 2x 8

1 and 8x

  1 2 : 1 C .y 0 /2 D 2x C 8x

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ADAMS and ESSEX: CALCULUS 9

Thus the arc length is given by s   Z 2 1 2 1 C 2x sD dx 8x 1   Z 2 1 D 2x C dx 8x 1 ˇ ˇ2  1 1 ˇ D x 2 C ln x ˇ D 3 C ln 2 units: ˇ 8 8

15.

1

11.

Z

Z a 1 C sinh2 x dx D cosh x dx 0 0 ˇa ˇ ea e a ˇ units: D sinh x ˇ D sinh a D ˇ 2

sD

a

p

ex 1 ; 2x4 ex C 1 e x C 1 .e x C 1/e x .e x y0 D x e 1 .e x C 1/2 2e x D 2x : e 1 The length of the curve is y D ln

LD D

13.

sD

=4 p

=6

14.

0

Let 2x D tan  2 dx D sec2  d

Z 1 xD2 3 sec  D 2 xD0 ˇˇxD2 1 D sec  tan  C ln j sec  C tan  j ˇˇ 4 xD0 ˇˇ2 p 1 p 2x 1 C 4x 2 C ln.2x C 1 C 4x 2 / ˇˇ D 4 0 p  1 p D 4 17 C ln.4 C 17/ 4 p p 1 D 17 C ln.4 C 17/ units. 4

278

16.

2

4e 2x dx 1/2

.e 2x

4

We have sD

=4

y D x 2 ; 0  x  2; y 0 D 2x. Z 2p length D 1 C 4x 2 dx

1C

Z

e

r

1 1 C 2 dx x Z ep 2 x C1 D dx Let x D tan u, dx D sec2 u du x 1 Z xDe Z xDe du sec3 u du D D 2 tan u xD1 cos u sin u xD1 Z xDe sin u du D v D cos u, dv D sin u du 2 2 xD1 cos u sin u Z xDe dv : D 2 v2/ xD1 v .1

1 C tan2 x dx

ˇ=4 ˇ ˇ D sec x dx D ln j sec x C tan xjˇ ˇ =6 =6   p 2 1 D ln. 2 C 1/ ln p C p 3 3 p 2C1 units: D ln p 3 Z

s

1 units

1=2

Z

Z

4

e 2x C 1 dx 2x 1 2 e ˇ4 Z 4 x ˇ e Ce x x x ˇ D dx D ln e je j ˇ x e x 2 e 2     1 1 4 2 D ln e ln e e4 e2   8 e4 C 1 e 1 e2 D ln units. D ln 4 4 e e 1 e2

0

2x . 12. y D ln.1 x 2 /, 12  x  21 , y 0 D 1 x2 s Z 1=2 4x 2 length D 1C dx .1 x 2 /2 1=2 Z 1=2 1 C x2 dx D x2 1=2 1  Z 1=2  2 dx D 1C 1 x2 1=2  ˇ1=2 1 C x ˇˇ D x C ln D 2 ln 3 ˇ 1 x ˇ

Z

1/e x

1

Since 1 C A B D D C 2C C v 2 .1 v 2 / v v 1 v 1Cv A.v v 3 / C B.1 v 2 / C C.v 2 C v 3 / C D.v 2 D v 2 .1 v 2 / 8 A C C D D 0 ˆ < B CC CD D0 ) ˆ :A D 0 BD1 1 ) A D 0; B D 1; C D D D ; 2

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 7.3 (PAGE 412)

therefore, Z

19. xDe

"

#



1 1 1 1 C C dv sD v2 2 1 v 1Cv xD1 ˇ ˇ ˇxDe 1 1 ˇˇ 1 C v ˇˇ ˇˇ 1 ln D / .but v D cos u D p ˇ 2 C1 v 2 ˇ1 v ˇˇ x xD1 #ˇxDe " p 1 .1 C v/2 ˇˇ 2 x C1 ln D ˇ 2 j1 v 2 j ˇ xD1 3 2 20. 2 1 ˇe ˇ 1C p C 2 p 6 ˇ 1 x C17 x2 C 1 2 7ˇ D6 4 x C 1 2 ln 5ˇ 1 ˇ 1 1 x2 C 1 #ˇ " p e p 1 2 C x 2 C 2 1 C x 2 ˇˇ ln x2 C 1 D ˇ ˇ 2 x2 1 p 2 p 2 p p 1 2 C e C 2 1 C e 1 2 C ln.3 C 2 2/ ln D e2 C 1 2 e2 2 p p p 1 .3 C 2 2/e 2 2 D e C1 2 C ln p units: 2 2 C e2 C 2 1 C e2 17.

x 2=3 C y 2=3 D x 2=3 . By symmetry, the curve has congruent arcs in the four quadrants. For the first quadrant arc we have  3=2 y D a2=3 x 2=3 1=2  2 3  2=3 x a x 2=3 y0 D 2 3

1=3



21.

y D x 1=3 ; 1  x  2; y 0 D Length D

have

LD4

D 4a

a 0

1=3

D 4a1=3

s Z

1C a

x

LD

1

1=3

0

22.

0

0

Z p 3 2 1 C .4x / dx D

1 0

p 1 C 16x 6 dx:

Using a calculator we calculate some Simpson’s Rule approximations as described in Section 7.2: S2  1:59921 S8  1:60025

S4  1:60110 S16  1:60023:

r

1C

1 . We 9x 4=3

M4 D 1:03363 M8 D 1:03374 M16 D 1:00376:

Thus the length is approximately 1.0338 units. For the ellipse 3x 2 C y 2 D 3, we have 6x C 2yy 0 D 0, so y 0 D 3x=y. Thus s

ds D

9x 2 dx D 1C 3 3x 2

s

3 C 6x 2 dx: 3 3x 2

The circumference of the ellipse is

4

Z

s

1 0

3 C 6x 2 dx  8:73775 units 3 3x 2

(with a little help from Maple’s numerical integration routine.) For the ellipse x 2 C 2y 2 D 2, we have 2x C 4yy 0 D 0, so y 0 D x=.2y/. Thus

Z

a2=3 x 2=3 dx x 2=3

dx ˇa 3 2=3 ˇˇ x ˇ D 6a units. 2

.

s

x2 dx D 1C 4 2x 2

s

4 x2 dx 4 2x 2

p The length of the short arc from .0; 1/ to .1; 1= 2/ is

18. The required length is Z

1

ds D :

2=3

f .x/ dx, where f .x/ D

T4 D 1:03406 T8 D 1:03385 T16 D 1:03378

Thus the length of the whole curve is Z

R2

1 x 3

23.

1 0

s

4 x2 dx  1:05810 units 4 2x 2

(with a little help from Maple’s numerical integration routine). Z 2 p S D 2 jxj 1 C 4x 2 dx Let u D 1 C 4x 2 0 du D 8x dx ˇ17 Z   2 3=2 ˇˇ  17 p u du D D u ˇ ˇ 4 1 4 3 1 p  D .17 17 1/ sq: units: 6 p y D x 3 , 0  x  1. ds D 1 C 9x 4 dx. The area of the surface of rotation about the x-axis is S D 2 D

To four decimal places the length is 1.6002 units.

 18

Z

1

0

Z

p x 3 1 C 9x 4 dx

10 1

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p

u du D

Let u D 1 C 9x 4 du D 36x 3 dx

 .103=2 27

1/ sq. units.

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SECTION 7.3 (PAGE 412)

24.

ADAMS and ESSEX: CALCULUS 9

q y D x 3=2 , 0  x  1. ds D 1 C 94 x dx. The area of the surface of rotation about the x-axis is

S D 2

Z

1

x 0

128 243

D

128 243

D

3=2

Z

3=2 0

Z tan

r

9x 1C dx 4

p u4 1 C u2 du 1

.3=2/

25.

1

.3=2/

Let 9x D 4u 9 dx D 8u du

Let u D tan v du D sec2 v dv

D

32 D 81

.sec7 v

64 D 81

2 sec5 v C sec3 v/ dv:

26. secn v dv D

1 n

1

secn

2

v tan v C

n n

2 1

Z

secn

2

v dv

(see Exercise 36 of Section 7.1) to reduce the powers of secant down to 3, and then use Z

a 0

sec3 v dv D

1 .sec a tan a C ln j sec a C tan aj: 2

D D

D D

Z

a 0

0

Z

9x dx 4

du D 13=4

2 5=2 u 5

9x 4

9 dx 4

p 1/ u du

.u

1



Let u D 1 C

2 3=2 u 3

.13=4/5=2 5

1

ˇˇ13=4 ˇ ˇ ˇ 1

.13=4/3=2 3

1

!

sq. units.

We have Z

1

ex

p

Let e x D tan  e x dx D sec2  d Z xD1 Z xD1 p D 2 1 C tan2  sec2  d D 2 sec3  d xD0 xD0  ˇˇxD1 ˇ D  sec  tan  C ln j sec  C tan  j ˇ : ˇ

S D 2

0

1 C e 2x dx

xD0

Since

p 1 C e2 ; p x D 0 ) tan  D 1; sec  D 2;

.sec7 v

2 sec5 v C sec3 v/ dv

ˇa  Z a Z a 5 sec5 v tan v ˇˇ 2 sec5 v dv C sec3 v dv ˇ C ˇ 6 6 0 0 0 ˇa # " Z sec5 a tan a 7 sec3 v tan v ˇˇ 3 a 3 sec v dv C ˇ ˇ 6 6 4 4 0 0 Z a sec3 v dv C 0 27. Z 1 a sec5 a tan a 7 sec3 a tan a C sec3 v dv 6 24 8 0 sec a tan a C ln j sec a C tan aj sec5 a tan a 7 sec3 a tan a C : 6 24 16

Substituting a D arct an.3=2/ now gives the following value for the surface area: p ! p 8 3 C 13 28 13 C ln SD sq. units. 81 243 2

280

x 1C

x D 1 ) tan  D e; sec  D

We have

I D

r

1

32 81

tan4 v sec3 v dv

At this stage it is convenient to use the reduction formula Z

Z

S D 2

2

0

Z 128 tan D 243 0

If y D x 3=2 , 0  x  1, is rotated about the y-axis, the surface area generated is

therefore   p p p p 2 ln j 2 C 1j S D  e 1 C e 2 C ln j 1 C e 2 C ej " # p p p 1 C e2 C e 2 sq: units: D e 1Ce 2 C ln p 2C1 If y D sin x; 0  x  , is rotated about the x-axis, the surface area generated is S D 2 D 2 D 2

Z



0

Z

Z

1 1

p sin x 1 C cos2 dx

Let u D cos x du D sin x dx

p 1 C u2 du

=4

=4

Let u D tan  du D sec2  d Z =4 sec3  d D 4 sec3  d 0

ˇˇ=4 D 2 sec  tan  C ln j sec  C tan  j ˇˇ 0 p p  2 C ln.1 C 2/ sq. units. D 2 

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INSTRUCTOR’S SOLUTIONS MANUAL

28.

SECTION 7.3 (PAGE 412)

 2 2  2 2 x x 1 1 D C 1 C .y 0 /2 D 1 C 4 x2 4 x2  2  Z 4 3 1 x 1 x C C 2 dx S D 2 12 x 4 x 1  Z 4 5 x x 1 C C 3 dx D 2 48 3 x 1  ˇˇ4  6 2 x 1 x ˇ C D 2 ˇ 288 6 2x 2 ˇ

32.

dy x D p , and dx 2 4 x2 S D 2  2

1

D

D

Z

D

Z

275  sq: units: 8

1 x3 C , 1  x  4, we have 29. For y D 12 x  2  1 x C 2 dx. ds D 4 x The surface generated by rotating the curve about the yaxis has area  Z 4  2 x 1 x S D 2 C 2 dx 4 x 1 ˇˇ4  4 x ˇ C ln jxj ˇ D 2 ˇ 16  1  255 C ln 4 sq. units. D 2 16 30. The area of the cone obtained by rotating the line y D .h=r/x, 0  x  r, about the y-axis is ˇr p Z r p r 2 C h2 x 2 ˇˇ 2 S D 2 x 1 C .h=r/ dx D 2 ˇ r 2 ˇ 0 0 p D  r r 2 C h2 sq. units. b/2 C y 2 D a2 we have

31. For the circle .x

dy D0 dx

b/ C 2y

2.x Thus s ds D

The top half of x 2 C 4y 2 D 4 is y D

1C

.x

b/2 y2

dx D

)

dy D dx

a dx D p y a2

x

b y

a b/2

:

dx

p

2

p

x2

4 2

0

s

3x 2 dx

16

=3 0

x 2 , so

2 x p dx 2 4 x2 r 16 Let x D sin  3 r 16 dx D cos  d 3

0

1C



4 .4 cos  / p cos  d 3

Z 16 =3 cos2  d D p 3 0  ˇˇ=3 8 ˇ D p  C sin  cos  ˇ ˇ 3 0 p 2.4 C 3 3/ p sq: units: D 3 3

33.

For the ellipse x 2 C 4y 2 D 4 we have 2x

dx C 8y D 0 dy

)

dx D dy

y 4 : x

The arc length element on the ellipse is given by

ds D D

.x (if y > 0). The surface area of the torus obtained by rotating the circle about the line x D 0 is Z bCa a dx Let u D x b S D 2  2 xp 2 a .x b/2 b a du D dx Z a uCb p D 4a du 2 u2 Zaa a du p by symmetry D 8ab a2ˇ u2 0 a u ˇˇ D 8ab sin 1 ˇ D 4 2 ab sq. units. aˇ 0

2

Z

1p 4 2

s

1C s 1C



dx dy

2

dy

16y 2 1p dy D 4 C 12y 2 dy: 2 x x

If the ellipse is rotated about the y-axis, the resulting surface has area Z 1 1p S D 2  2 x 4 C 12y 2 dy x 0 Z 1p p 1 C 3y 2 dy Let 3y D tan  D 8 p 0 3dy D sec2  d Z =3 8 D p sec3  d 3 0 ˇˇ=3 8  D p sec  tan  C ln j sec  C tan  j ˇˇ 2 3 0 p  8  p D p 2 3 C ln.2 C 3/ 2 3 p ! ln.2 C 3/ sq. units. p D 8 1 C 2 3

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ADAMS and ESSEX: CALCULUS 9

Thus, the surface area depends only on the radius R of the sphere, and the distance .b a/ between the parellel planes.

34. As in Example 4, the arc length element for the ellipse is

ds D

s



1C

dy dx

2

y

v u u 2 ta

dx D

a

2

a2

2

b 2 x a2 dx: x2

To get the area of the ellipsoid, we must rotate both the upper and lower semi-ellipses (see the figure for Exercise 20 of Section 8.1): S D 2  2

Z a"

c

r

1

v u Z au t a2

 x 2

b 1

0

cCb

D 8c

r

 x 2 a

!#

a2

a

!

C

Fig. 7.3-36 k

37. If the curve y D x , 0 < x  1, is rotated about the y-axis, it generates a surface of area

x2

p

R =2 p a2 b 2 and E."/ D 0 1 a defined in Example 4.

where " D

S D 2 D 2

"2 sin t dt as

If k 

10 

Z

s

=2

0

Z

s

=2

1C

S D 2

2

  sin2 t dt 4 4 s Z =2 2 5p 4 C 2 1 D sin2 t dt  4 C 2 0    5p : D 4 C  2E p  4 C 2 D

0

1C

D 2 < 2

38. 36. Let the equation of the sphere be x 2 C y 2 D R2 . Then the surface area between planes x D a and x D b . R  a < b  R/ is S D 2 D 2

Z

282

b

R2

x2

p

R2

x2 p

a

Z

s

p

a

Z

D 2R

b

1C



dy dx

R R2

x2

2

dx D 2R.b

0

Z

1

0

p x 1 C k 2 x 2.k

p

1/

dx

x 2 C k 2 x 2k dx: Z

1

x k dx, which is infinite.

0

Z

1

0

Z

0

1

p x 1 C k 2 x 2.k

p

x2

2k

Z p 1 C k2

1 0

1/

x k dx < 1:

Thus the area is finite if and only if k > 1. Z 1 r 1 S D 2 jxj 1 C 2 dx x 0 Z 1p D 2 x 2 C 1 dx Let x D tan  0 dx D sec2  d Z =4 D 2 sec3  d 0

ˇ ˇ=4 ˇ D  sec  tan  C ln j sec  C tan  j ˇ ˇ 0 p p D Œ 2 C ln. 2 C 1/ sq: units:

dx

a/ sq: units:

dx

C k 2 x k dx



dx

b a

1

1, we have S  2k

2 cos2 t dt 4 2

Z

If k  0, the surface area S is finite, since x k is bounded on .0; 1 in that case. Hence we need only consider the case 1 < k < 0. In this case 2 < 2 2k < 4, and

35. From Example 3, the length is 10 sD 

x

x 2 Cy 2 DR2

dx  0 1 D 8c of the circumference of the ellipse 4 D 8caE."/ a2

b

ds

b2

a2 x2

a

39.

a) Volume V D 

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R 1 dx D  cu. units. 1 x2

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 7.4 (PAGE 419)

b) The surface area is S D 2 > 2

Z

1

Z 11 1

r 1 1 1 C 4 dx x x dx D 1: x

3.

c) Covering a surface with paint requires applying a layer of paint of constant thickness to the surface. Far to the right, the horn is thinner than any prescribed constant, so it can contain less paint than would be required to cover its surface.

The mass of the plate is m D 0  area D The moment about x D 0 is MxD0 D D

a

p x0 a2

0 2

Z

a2

p

u du

0

0

The mass of the wire is Z L Z L s ds mD ı.s/ ds D sin L 0 0 ˇL s ˇˇ L 2L cos : D ˇ D  Lˇ 

0 a3 4 4a MxD0 D D . By symmetry, 2 m 3 0 a 3 x. Thus the centre of mass of the plate is 4a . 3

Thus x D

y D  4a ; 3

y

0

p yD a2 x 2

Since ı.s/ is symmetric about s D L=2 (that is, ı..L=2/ s/ D ı..L=2/ C s/), the centre of mass is at the midpoint of the wire: s D L=2.

2. A slice of the wire of width dx at x has volume d V D .a C bx/2 dx. Therefore the mass of the whole wire is Z L mD ı0 .a C bx/2 dx 0 Z L D ı0  .a2 C 2abx C b 2 x 2 / dx  0 1 2 3 2 2 D ı0  a L C abL C b L : 3 Its moment about x D 0 is Z L MxD0 D xı0 .a C bx/2 dx 0 Z L D ı0  .a2 x C 2abx 2 C b 2 x 3 / dx 0   1 1 2 2 2 a L C abL3 C b 2 L4 : D ı0  2 3 4 Thus, the centre of mass is   1 1 2 2 2 a L C abL3 C b 2 L4 ı0  2 3 4   xD 1 ı0  a2 L C abL2 C b 2 L3 3   1 2 2 1 2 2 L a C abL C b L 2 3 4 D : 1 a2 C abL C b 2 L2 3

Let u D a2 x 2 du D 2x dx

x 2 dx

0

ˇa 2 0 2 3=2 ˇˇ 0 a3 D u ˇ D : ˇ 2 3 3

Section 7.4 Mass, Moments, and Centre of Mass (page 419) 1.

Z

0 a2 . 4

dx x

a

x

Fig. 7.4-3

4.

p A vertical strip has area dA D a2 x 2 dx. Therefore, the mass of the quarter-circular plate is Z

a

p .0 x/ a2

Let u D a2 x 2 du D 2x dx  ˇa2 Z a2 p 2 3=2 ˇˇ 1 1 1 u u du D 0 D 0 ˇ D 0 a3 : ˇ 2 2 3 3 0

mD

x 2 dx

0

0

The moment about x D 0 is MxD0 D

Z

a

p 0 x 2 a2

0

D 0 a4

Z

=2

x 2 dx

Let x D a sin  dx D a cos  d

sin2  cos2  d

0

Z 0 a4 =2 2 sin 2 d 4 0 Z 0 a4 0 a4 =2 .1 cos 4 / d D : D 8 16 0

D

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SECTION 7.4 (PAGE 419)

ADAMS and ESSEX: CALCULUS 9

The moment about y D 0 is Z

1 D 0 2

MyD0

a

x.a

2

0 2 2

a x 1 0 2 2

D

The moment about x D 0 is Z 3 MxD0 D 10 h2

2

x / dx !ˇa x 4 ˇˇ 1 ˇ D a4 0 : 4 ˇ 8

0

D 10

0

mD2

Z

4

0

D 2k D 2k

Z

p ky 4

4

0



0

MyD0 D 2

4

0

D 2k D 2k

Z

p ky 2 4

4

1=2

.16u

0



32 3=2 u 3

3=2

8u

Cu

/ du ˇ4 16 5=2 2 7=2 ˇˇ 4096k u C u : ˇ D ˇ 5 7 105

4096k 15 16  D . The centre of mass of the 105 256k 7 plate is .0; 16=7/. y

p xD 4 y

density ky

7.

The mass of the plate is Z a ka3 : mD kx a dx D 2 0

2

3 0

 .5h/ 2



h2 D 10 2

284

a 0

kx 2 a dx D

ka4 : 3

y

a

Fig. 7.4-5

Z

x

3

2a 2 ka4 Thus x D D  . The centre of mass of the 3 3  3  ka 2a a plate is ; . 3 2

x

6. A vertical strip at h has area dA D .2 mass of the plate is

2 3 h/ dh.

 Z 3 2 h dh D 10 h 3 0 ˇ 3 h3 ˇˇ ˇ D 15 kg: 9 ˇ

1 . The centre 2

Fig. 7.4-6

By symmetry, y D a=2. Z MxD0 D

4

mD

D

dh h

5=2

2



2 yD2 3 x

0

Thus y D

15 2 15

2

Let u D 4 y du D dy

y dy



y

By symmetry, MxD0 D 0, so x D 0. Z

0

45 3 2 Thus, x D D and y D 15 2 of mass is located at . 32 ; 21 /.

ˇ4 2 5=2 ˇˇ 256k u : ˇ D ˇ 5 15

8 3=2 u 3

h3 3

0



u/u1=2 du

.4



Let u D 4 y du D dy

y dy



The moment about y D 0 is   Z 3  1 1 2 2 MyD0 D 10 h h h dh 2 3 3 0 2  Z 3 2 2 1 3 h C h dh D 10 h 3 9 0 ˇ3  2 3 4 ˇ h 2h h ˇ 15 D 10 C kg-m: ˇ D 2 9 36 ˇ 2

3 3 a and y D a. Hence, the centre of mass 16 8 3 3 is located at . a; a/. 16 8 5. The mass of the plate is Thus, x D

 h3 dh 3 ˇ 3 h4 ˇˇ 45 kg-m. ˇ D ˇ 12 2

h2 3

Thus, the 

density

kx

dh a

Fig. 7.4-7

0

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x

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 7.4 (PAGE 419)

  a 8. A vertical strip has area dA D 2 p r dr. Thus, the 2 mass is  Z a=p2   a r dr kr 2 p mD2 2 0  Z a=p2  a k D 4k p r r 2 dr D p a3 g: 2 3 2 0

50 .8000/k 40 Thus, x D 3 D . Since the density is inde10000k 3 5 pendent of y and z, y D and z D 5. Hence, the centre 2 of mass is located on the 20 cm long central axis of the brick, two-thirds of the way from the least dense 10  5 face to the most dense such face. y

5

Since the mass is symmetric about the y-axis, and the plate is symmetric about both the x- and y-axis, therefore the centre of mass must be located at the centre of the square. y

a p 2

dx

a x yD p 2 a p dr 2

r

x

x

z

20

10

Fig. 7.4-10 x

Fig. 7.4-8 9.

mD MxD0 D

Z

b

a

Z

b

a

Z

 .x/ g.x/

 f .x/ dx

 x.x/ g.x/

 f .x/ dx

11.

  1 MyD0 D x.x/ .g.x//2 .f .x//2 dx 2 a   MxD0 MyD0 ; : Centre of mass: m m b

y

Choose axes through the centre of the ball as shown in the following figure. The mass of the ball is Z

R

.y C 2R/.R2 y 2 / dy ˇR  8 y 3 ˇˇ 2 D 4R R y ˇ D R4 kg: ˇ 3 3

mD

yDg.x/

R

0

density .x/

By symmetry, the centre of mass lies along the y-axis; we need only calculate y.

yDf .x/ a

b

x

MyD0 D

Fig. 7.4-9 10. The slice of the brick shown in the figure has volume d V D 50 dx. Thus, the mass of the brick is Z 20 ˇ20 ˇ mD kx50 dx D 25kx 2 ˇ D 10000k g: The moment about x D 0, i.e., the yz-plane, is MxD0 D 50k D

Z

0

20

50 3 ˇˇ20 kx ˇ x 2 dx D 0 3

50 .8000/k g-cm: 3

R R

D 2

Z

y.y C 2R/.R2 R

y 2 .R2

0

 y3 D 2 R2 3

0

0

Z

y 2 / dy

y 2 / dy ˇR y 5 ˇˇ 4 R5 : ˇ D 5 ˇ 15 0

4R5 R 3 Thus y D D  : The centre of mass is on 15 8R4 10 the line through the centre of the ball perpendicular to the plane mentioned in the problem, at a distance R=10 from the centre of the ball on the side opposite to the plane.

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ADAMS and ESSEX: CALCULUS 9

y

z y

a

x

z

yC2R R

p a2 z 2

a

a

y

a

2R

x

Fig. 7.4-13 Fig. 7.4-11 12. A slice at height z has volume d V D y 2 dz and density kz g=cm3 . Thus, the mass of the cone is mD

Z

b

d m D 0 z dz

2

kzy dz Z b  D ka2 z 1 0

z b

0

D ka

2



2

dz

2z 3 z4 C 2 3b 4b

z2 2

ˇˇb ˇ ˇ ˇ

MzD0 D ka

Z

b

z

0

2



1

z b

2

dz D

1 ka2 b 3 g-cm: 30

2b . Hence, the centre of mass is on the axis 5 of the cone at height 2b=5 cm above the base. Thus, z D

0 z.a2 2 20 z.a2 D 3

dz z yDa 1

z b

 y

Fig. 7.4-12 13. By symmetry, y D 0.

286

z2/

p 4 a2 z 2 3

z 2 /3=2 :

Thus the mass of the solid is Z 0 a 2 .a z z 3 / dz mD 2 0  ˇa 0 a2 z 2 z 4 ˇˇ 0 a4 D : ˇ D 2 2 4 ˇ 8 0

Also,

z b

a

z 2 /;

dMxD0 D d m x D

0

The moment about z D 0 is 2

 2 .a 2

and its moment about x D 0 is

1 ka2 b 2 g: 12

D

A horizontal slice of the solid p at height z with thickness dz is a half-disk of radius a2 z 2 with centre of mass p 4 a2 z 2 at x D , by Exercise 3 above. Its mass is 3

and z D

Finally,

MzD0 D

0 2

D

0 2

Z

a

.a2 z 2

0



a2 z 3 3

0 a5 8a 8 D  . 15 0 a4 15

z 4 / dz ˇa z 5 ˇˇ 0 a5 ; ˇ D 5 ˇ 15

Z 20 a z.a2 z 2 /3=2 dz 3 0 Z 2 0 a 3=2 u du D 3 0  ˇa2 0 2 5=2 ˇˇ 20 a5 D u ; ˇ D ˇ 3 5 15

MxD0 D

0

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0

Let u D a2 z 2 du D 2z dz

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 7.4 (PAGE 419)

8 16a 20 a5  D . 4 15 0 a  15  8a 16a ; 0; : The centre of mass is 15 15

3 3a ka4  D . By symmetry, x D 0. 3 2 ka 2   3a Thus, the centre of mass of the plate is 0; . 2 Therefore, y D

so x D

14.

Assume the cone has its base in the xy-plane and its vertex at height b on the z-axis. By symmetry, the centre of mass lies on the z-axis. A cylindrical shell of thickness dx and radius x about the z-axis has height z D b.1 .x=a//. Since it’s density is constant kx, its mass is  x dx: d m D 2bkx 2 1 a Also its centre of mass is at half its height, y shell D

b 1 2

ds

MzD0 D

Z

Z

a 0 a

 2bkx 2 1 bkx

2

0



1

x 2 dx: a

x kba3 dx D a 6 x 2 kb 2 a3 dx D a 30

and z D MzD0 =m D b=5. The centre of mass is on the axis of the cone at height b=5 cm above the base. 15. y x 2 Cy 2 Da2 ds

 d

a

 x

Fig. 7.4-16 L The radius of the semicircle is . Let s measure the  distance along the wire from the point where it leaves the positive x-axis. Thus, the density at position s is s  ı.s/ D sin g=cm. The mass of the wire is L mD

s

xa

Fig. 7.4-15 Consider the area element which is the thin half-ring shown in the figure. We have d m D ks s ds D k s ds: k 3 a . 3 Regard this area element as itself composed of smaller elements at positions given by the angle  as shown. Then  Z  .s sin  /s d ks ds dMyD0 D 0

L 0

s sin ds D L

ˇL L s ˇˇ 2L cos g: ˇ D  Lˇ  0

Since an arc element ds at position s is at height L s L sin  D sin , the moment of the wire about y D   L y D 0 is

Thus, m D

D 2ks 3 ds; Z a ka4 : D 2k s 3 ds D 2 0

Z

MyD0 D

2

MyD0

s

L 

 dMzD0 D y shell d m D bkx 2 1

mD

y

x : a

Thus its moment about z D 0 is

Hence

16.

Z

L 0

L 2 s sin ds  L

Let  D s=L d D ds=L

 Z L 2  2 sin  d  0 ˇˇ L2  L2 D  sin  cos  ˇˇ D g-cm: 2 2 2 0 D



Since the wire and the density function are both symmetric about the y-axis, we have MxD0 D 0.   L . Hence, the centre of mass is located at 0; 4

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17.

Z

1

ADAMS and ESSEX: CALCULUS 9

1 rD m

Z

p yD r 2 x 2

r

dx

2

d V D ue u du 2 V D 12 e u 0 ˇ Z 2 R 4 C ue u ˇˇ 1 R D 3=2 lim @ e C ˇ ˇ R!1 2 2 0 k 0   Z 1 1 u2 4 C D 3=2 0 C e du 2 0 k p   3=2 5:57C 4 C  DC  3=2 : D 3=2 4 k k k U Du d U D du

18.

y

2

C e kr .4 r 2 / dr 0 Z 1 p 2 D 4 C r 2 e kr dr Let u D k r p 0 du D k dr Z 4 C 1 2 u2 u e du D 3=2 k 0

mD

x

u2

1

duA

x

r

Fig. 7.5-1 2.

x D 0. A horizontal strip at y has By symmetry, p p mass d m D 2 9 y dy and moment dMyD0 D 2y 9 y dy about y D 0. Thus, mD2

Z

9

0

p

y dy D

9

  2 .9 2 3

y/

and

1

rC e

0

4 C D C  3=2 k

3=2

Z

3=2

4k D p

kr 2

Z

2

.4 r / dr

1

3

r e

kr 2

dr

0

1

MyD0 D 2

2

Let u D kr du D 2kr dr

D4

1 ue u du  2k 2 0 U Du d V D e u du d U D du 0 V D e u 1 ˇR Z ˇ R 2 ˇ lim @ ue u ˇ C e u duA D p ˇ k R!1 0 0  2 2  0 C lim .e 0 e R D p : D p R!1 k k

Section 7.5 Centroids

Z

Z

p y 9

y dy

.9u2

u4 / du D 4.3u3

9 0 3 0

ˇ9 ˇ ˇ D 36 ˇ

3=2 ˇ

Let u2 D 9 y 2u du D dy

0

ˇ3 ˇ

1 5 ˇ u /ˇ 5

0

D

648 : 5

648 18 D . Hence, the centroid is at Thus, y D 5  36 5   18 0; . 5 y

9 yD9 x 2 dy

y

3

(page 424)

3

x

Fig. 7.5-2 3. r2 AD Z4

1.

r

p x r2

AD

Let u D r 2 x 2 0 du D 2x dx ˇr 2 Z r2 3=2 ˇ 1 u ˇ r3 1=2 D u du D ˇ D 2 0 3 ˇ 3

MxD0 D

The area and moments of the region are

D

Z

MxD0 D

Z

x 2 dx

4r 4 r D  D y by symmetry: 3 r 2 3 4r 4r ; . The centroid is 3 3 xD

288

1

p

0

=4

dx 1 C x2

Let x D tan  dx D sec2  d

sec  d 0

ˇ=4 p ˇ D ln j sec  C tan  jˇˇ D ln.1 C 2/

0

3

Z

MyD0 D

0

1

0

1 2

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Z

p 1

0

x dx

ˇ1 p p ˇ D 1 C x 2 ˇˇ D 2

1 C x2 dx 1 D tan 1 C x2 2

1

0 ˇ1 ˇ

x ˇˇ D 0

 : 8

1

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INSTRUCTOR’S SOLUTIONS MANUAL

Thus x D centroid is

p

SECTION 7.5 (PAGE 424)

2

1  p , and y D p . The 2/ 8 ln.1 ! C 2/ 1  . p ; p ln.1 C 2/ 8 ln.1 C 2/

5.

ln.1 C p 2

y yD p

By symmetry, x D 0. We have

1

p

x

MyD0

Fig. 7.5-3

3 p

4

0

D2 4

1Cx 2

1

Z

AD2

Z

=3

MxD0 D

Z

p r= 2

0

r3 D p 6 2

1 2 8 r .

x 2 dx C 1 2 .r 3

p

cos2  d

0

3

Let x D 2 sin  ! dx D 2 cos  d

ˇ=3 p ˇ D 4. C sin  cos  /ˇˇ 2 3 0 p ! p  4 p 3 D4 3 C 2 3D 3 4 3 p Z 3 p 2 1 4 x 2 1 dx D 2 2 0 Z p3   p D 5 x 2 2 4 x 2 dx 0

4. The area of the sector is A D x D 0 is

 1 dx

x2

p D5 3

p 3

p D4 3

4

2

Z

p

3

p

4

x 2 dx

0

p ! p  3 C D3 3 3 4

4 : 3

p p 9 3 4 3 9 3 4 Thus y D  p D p . The 3 4! 3 3 4 3 3 p 9 3 4 centroid is 0; p . 4 3 3

Its moment about

y

Z

p x r 2 x 2 dx ˇr ˇ r3 2 3=2 ˇ x / ˇ D p : ˇ p 3 2 r= 2 r

1

p r= 2

r3 8r 8 D p . By symmetry, the p  r2 3 2 3 2  p  D x. 2 1/. centroid must lie on the line y D x tan 8 p 8r. 2 1/ Thus, y D p . 3 2

p

Fig. 7.5-5

6.

By symmetry, x D 0. The area is A D moment about y D 0 is MyD0

p yD r 2 x 2

yDx

p x 3

3

Thus, x D

y

p yD 4 x 2 1

"

1 2 ab.

 2 # Z a x 2 b 1 dx D b 1 a a 0 ˇ  a x 3 ˇˇ 2 D b2 x ˇ D ab 2 : 3a2 ˇ 3 1 D 2

Z

a

2

The

x2 dx a2

0

pr

Fig. 7.5-4

r 2

x

Thus, y D

2 4b 2ab 2  D . 3 ab 3

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ADAMS and ESSEX: CALCULUS 9

y

8. yDb

q

1

x2 a2

dx a

x

ax

Fig. 7.5-6 7.

The quadrilateral consists of two triangles, T1 and T2 , as shown in the figure. The area and centroid of T1 are given by 41 D 2; 2 0C3C4 7 x1 D D ; 3 3

The region is the union of a half-disk and atriangle.  The 4 and centroid of the half-disk is known to be at 1; 3   2 2 ; . The area of the semithat of the triangle is at 3 3  and the triangle is 2. Hence, circle is 2     2 3 C 8 MxD0 D I .1/ C .2/ D 2 3 6       4 2 2 MyD0 D C .2/ D : 2 3 3 3  C 2, then Since the area of the whole region is 2 3 C 8 4 xD and y D . 3. C 4/ 3. C 4/

A1 D

y

0C1C0 1 y1 D D : 3 3

The area and centroid of T2 are given by 42 D 4; 2 0C2C4 D 2; x2 D 3

y2 D

0

2C0 D 3

M1;yD0

M2;xD0 D 2  4 D 8 2 M2;yD0 D 4D 3

8 : 3

Since areas and moments are additive, we have for the whole quadrilateral A D 2 C 4 D 6; 14 38 MxD0 D C8D ; 3 3

2

x

Fig. 7.5-8 9.

14 3 2 3

1

2

2 : 3

It follows that 7 2D 3 1 D 2D 3

1 .x 1/2

yDx 2

A2 D

M1;xD0 D

p

yD

MyD0 D

38 19 2 D , and y D D Thus x D 36 9 6  19 1 of the quadrilateral is ; . 9 3

2 3

8 D 3

2:

1 . The centroid 3

A circular strip of the surface between heights y and y C dy has area dS D 2x

r dy D 2x dy D 2 r dy: cos  x

The total surface area is S D 2 r

Z

0

r

dy D 2 r 2 :

The moment about y D 0 is ˇr Z r ˇ 2 ˇ MyD0 D 2 r y dy D  r.y /ˇ D  r 3 : 0

0

3

r r D . By symmetry, the centroid of the Thus y D 2 r 2 2 hemispherical surface is on the axis of symmetry of the hemisphere. It is halfway between the centre of the base circle and the vertex. y

y

.3;1/

T1

 4 x

.x;y/

dS

T2 r

y

 x

.2; 2/

Fig. 7.5-9

Fig. 7.5-7

290

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x

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 7.5 (PAGE 424)

z h

10. By symmetry, x D y D 0. The volume is V D 32  r 3 . A thin slice of the solid at height z will have volume d V D y 2 dz D .r 2 z 2 / dz. Thus, the moment about z D 0 is Z

MzD0 D

z.r 2

0

D

dz z

r



r 2z2 2

z 2 / dz  ˇr z 4 ˇˇ r4 : ˇ D 4 ˇ 4

yDr 1

y

r4 3r 3 D  . Hence, the centroid is on 4 2 r 3 8 the axis of the hemisphere at distance 3r=8 from the base. z

p yD r 2 z 2

Fig. 7.5-11 12. A band  z with vertical width dz has radius  at height z , and has actual (slant) width yDr 1 h s s  2 dy r2 dz D 1 C 2 dz: ds D 1 C dz h Its area is

dz y



r

dA D 2 r 1

x

(See the following The cone has volume V D figure.) The disk-shaped slice with vertical width dz has   z , and therefore has volume radius y D r 1 h z 2 r2 dz D  2 .h h h

D

r2 h2

r2 D 2 h

Z

h

z.h

z/2 dz

0

Z

h

.h



hu3 3

Let u D h z du D dz

u/u2 du

0

u4 4

1C

r2 dz: h2

0

z/2 dz:

We have r2 h2

s

The moment about z D 0 is s   Z z r2 h z 1 dz MzD0 D 2 r 1 C 2 h 0 h s ˇh  p r 2 z2 z 3 ˇˇ 1 D 2 r 1 C 2 ˇ D  rh r 2 C h2 : ˇ h 2 3h 3

1 2 3  r h.

MzD0 D

z h

Thus the area of the conical surface is s Z p r2 h  z 1 dz D  r r 2 C h2 : A D 2 r 1 C 2 h 0 h

Fig. 7.5-10

 dV D r2 1



r

0

Thus, z D

11.

z h

ˇˇh  r 2 h2 ˇ : ˇ D ˇ 12 0

 r 2 h2 3 h  D . The centroid of the Therefore z D 12  r 2h 4 solid cone is on the axis of the cone, at a distance above the base equal to one quarter of the height of the cone.

13.

p  rh r 2 C h2 h 1 p D . By  Thus, z D 3 3  r r 2 C h2 symmetry, x D y D 0. Hence, the centroid is on the axis of the conical surface, at distance h=3 from the base.  By symmetry, x D . The area and y-moment of the 2 region are given by Z  sin x dx D 2 AD 0 Z  1 MyD0 D sin2 x dx 2 0 ˇ ˇ 1  D .x sin x cos x/ˇˇ D : 4 4 0      ; . Thus y D , and the centroid is 8 2 8

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ADAMS and ESSEX: CALCULUS 9

y

Hence x D r 2 

2r 2 D , and the centroid is r  y



 2r 2r ; .  

yDsin x x 2 Cy 2 Dr 2

r

ds 

=2

x r

Fig. 7.5-13 14.



The area of the region is

x xCdx

ˇ=2 Z =2 ˇ ˇ AD cos x dx D sin x ˇ D 1: ˇ 0

r

x

Fig. 7.5-15

0

16.

The moment about x D 0 is Z =2 MxD0 D x cos x dx 0

U Dx d V D cos x dx d U D dx V D sin x ˇ=2 Z ˇ =2  ˇ sin x dx D D x sin x ˇ ˇ 2 0

By symmetry, the centroid of the solid lies on its vertical axis of symmetry; let us continue to call this the y-axis. We need only determine y S . Since D lies between y D 1 and y D 2, its centroid satisfies yD D 3=2. Also, by Exercise 11, the centroid of the solid cone satisfies y C D 3=4. Thus C and D have moments about y D 0:

1:

0

Thus, x D

 2

1. The moment about y D 0 is 1 2

MyD0 D

Z

=2

cos2 x dx

MC;yD0 D

0

 ˇˇ=2 1  1 ˇ x C sin 2x ˇ D : D ˇ 4 2 8

Thus, y D

y 1

yDcos x

 . The centroid is 8

 2

1;

  . 8

17.

 2

x

r . By symmetry, x D y. An 2 element of the arc between x and x C dx has length The arc has length L D

r dx r dx dx D D p ds D : sin  y r 2 x2 Thus MxD0 D

292

Z

r 0

xr dx p D r 2 x2

p r r2

  3 D ; 4

MD;yD0 D .4/

  3 D 6: 2

  2 8 3x D 2.1/ C 1 D 3 3     3 2 11 : C1 D 3y D 2 2 3 3

Fig. 7.5-14 15.

4 3

The region in figure (a) is the union of a rectangle of area 2 and centroid .1; 3=2/ and a triangle of area 1 and centroid .2=3; 2=3/. Therefore its area is 3 and its centroid is .x; y/, where

dx x



Thus MS;yD0 D  C 6 D 7, and z S D 7=.16=3/ D 21=16. The centroid of the solid S is on its vertical axis of symmetry at height 21/16 above the vertex of the conical part.

0



The solid S in question consists of a solid cone C with vertex at the origin, height 1, and top a circular disk of radius 2, and a solid cylinder D of radius 2 and height 1 sitting on top of the cone. These solids have volumes VC D 4=3, VD D 4, and VS D VC C VD D 16=3.

Therefore, the centroid is .8=9; 11=9/. 18. The p region in figure (b) is the union of a square of area . 2/2 D 2 and centroid .0; 0/ and a triangle of area 1/2 and centroid .2=3; 2=3/. Therefore its area is 5/2 and its centroid is .x; y/, where

ˇr ˇ x 2 ˇˇ D r 2 : 0

5 1 x D 2.0/ C 2 2

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  2 1 D : 3 3

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 7.5 (PAGE 424)

Therefore, x D y D 2=15, and the centroid is .2=15; 2=15/.

23.

19. The region in figure (c) is the union of a half-disk of area =2 and centroid .0; 4=.3// (by Example 1) and a triangle of area 1 and centroid .0; 1=3/. Therefore its area is .=2/ C 1 and its centroid is .x; y/, where x D 0 and  C2  yD 2 2



4 3



C1



1 3



D

y

1 : 3

1

T

Therefore, the centroid is .0; 2=Œ3. C 2//.

20. The region in figure (d) is the union of three half-disks, one with area =2 and centroid .0; 4=.3//, and two with areas =8 and centroids . 1=2; 2=.3// and .1=2; 2=.3//. Therefore its area is 3=4 and its centroid is .x; y/, where 3 .x/ D 4 3 .y/ D 4

      1  1 .0/ C C D0 2 8 2 8 2       4 2 2   1  C C D : 2 3 8 3 8 3 2

xD2

24.

By symmetry the centroid is .1; 2/. y

Fig. 7.5-23 p s 3 . Its centroid is at The altitude h of the triangle is 2 h s height D p above the base side. Thus, by Pappus’s 3 2 3 Theorem, the volume of revolution is p !   s 3s s 3 s V D 2  cu: units: D p 2 2 4 2 3 p h s 3 The centroid of one side is D above the base. 2 4 Thus, the surface area of revolution is p ! p 3s .s/ D s 2  3 sq: units: S D 2  2 4

.1;1/ yD2x x 2

x

.1; 2/

x

1

Therefore, the centroid is .0; 2=.3//. 21.

 The triangle T has centroid 31 ; 13 and area 21 . By Pappus’s Theorem the volume of revolution about x D 2 is   1 5 1 cu. units. D V D  2 2 2 3 3

yD 2

s h

s

Fig. 7.5-21 22. The line segment from .1; 0/ to .0; 1/ has centroid . 12 ; 12 / p and length 2. By Pappus’s Theorem, the surface area of revolution about x D 2 is 

A D 2 2

 1 p

2

p

2 D 3 2 sq: units:

y 1

1

25.

For the purpose of evaluating the integrals in this problem and the next, the definite integral routine in the TI-85 calculator p was used. For the region bounded by y D 0 and y D x cos x between x D 0 and x D =2, we have AD

r

1 2

Fig. 7.5-24

2

3

x

Fig. 7.5-22

Z

0

=2

p

x cos x dx  0:704038

Z 1 =2 3=2 x cos x dx  0:71377 A 0 Z =2 1 x cos2 x dx  0:26053: yD 2A 0 xD

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ADAMS and ESSEX: CALCULUS 9

29. 26. The region bounded by y D 0 and y D ln.sin x/ between x D 0 and x D =2 lies below the x-axis, so Z

AD

=2

ln.sin x/ dx  1:088793

0

Z 1 =2 xD x ln.sin x/ dx  0:30239 A 0 Z =2  2 1 yD ln.sin x/ dx  0:93986: 2A 0

27.

c

MxD0 MyD0

AD MxD0 D D

0

Z

0

1

x dx .1 C x/3

0

Z

1

u

1

D lim

R!1

MyD0

1 D 2

Z

30.

ˇR ˇ 1 1 dx ˇ D lim ˇ D 3 2 R!1 2.1 C x/ ˇ .1 C x/ 2

1

1

0

1

u3 

Let u D x C 1 du D dx

du

1 1 C 2 u 2u

ˇˇR ˇ ˇ D1 ˇ 1

1 D 2 Z D

Z

c

d

c

The area and moments of the region are Z

By analogy with the formulas for the region a  x  b, f .x/  y  g.y/, the region c  y  d , f .y/  x  g.y/ will have centroid .MxD0 =A; MyD0 =A/, where Z d  AD g.y/ f .y/ dy d h

2 g.y/

 y g.y/

 2 i f .y/ dy

 f .y/ dy:

Let us take L to be the y-axis and suppose that a plane curve C lies between x D a and x D b where 0 < a < b. Thus, r D x, the x-coordinate of the centroid of C. Let ds denote an arc length element of C at position x. This arc length element generates, on rotation about L, a circular band of surface area dS D 2x ds, so the surface area of the surface of revolution is Z xDb S D 2 x ds D 2MxD0 D 2rs: xDa

1 1 D 2 2

ˇR ˇ dx 1 1 ˇ D lim : ˇ D R!1 10.1 C x/5 ˇ .1 C x/6 10

31.

y

0

 The centroid is 1; . 1 5

y

1 yD

1 .x C 1/3

1 t .=4/ L

t 1 p 2

x

p .=4/

t

P

x

2

t

N

Fig. 7.5-27 28. The surface Z 1area ispgiven by 2 S D 2 e x 1 C 4x 2 e 1

lim 1 C 4x 2 e

x!˙1

2x 2

2x 2

D 1, this expression must be bounded

for all x, that is, 1  1 C Z4x 2 e

stant K. Thus, S  2K

1

1

Fig. 7.5-31

2x 2

 K 2 for some conp 2 e x dx D 2K . The

integral converges and the surface area is finite. Since the 2 whole curve y D e x lies above the x-axis, its centroid would have to satisfy y > 0. However, Pappus’s Theorem would then imply that the surface of revolution would have infinite area: S D 2y  .length of curve/ D 1. The curve cannot, therefore, have any centroid.

294

M

dx. Since

We need to find the x-coordinate xLMNP of the centre of buoyancy, that is, of the centroid of quadrilateral LMNP . From various triangles in the figure we can determine the x-coordinates of the four points: xL D sec t; xP D sec t; xM D sec t C .1 C tan t / sin t xN D sec t C .1 tan t / sin t

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 7.6 (PAGE 431)

Triangle LMN has area 1 C tan t , and the x-coordinate of its centroid is xLMN sec t D D

2 sin t

3

sec t C .1 C tan t / sin t C sec t C .1 3 sec t :

Triangle LNP has area 1 its centroid is

tan t / sin t

2 m

sec t C sec t C sec t C .1 3 sec t C .1 tan t / sin t D : 3

2 m

tan t / sin t

Fig. 7.6-1 2.

Therefore,

D D D D

6 m

tan t , and the x-coordinate of

xLNP D

xLMNP D

h

dh

1h .2 sin t sec t /.1 C tan t / 6 i C .sec t C sin t sin t tan t /.1 tan t / i 1h 3 sin t 2 sec t tan t C sin t tan2 t 6 " # sin2 t 2 sin t C 3 6 cos2 t cos2 t i sin t h 3 cos2 t C sin2 t 2 2 6 cos t i i sin t h sin t h 2 cos2 t 1 D cos.2t / 2 2 6 cos t 6 cos t

A vertical slice of water at position y with thickness dy is in contact withpthe botttom over an area 8 sec  dy D 54 101 dy m2 , which is at depth 1 x D 10 y C 1 m. The force exerted on this area is then p 1 y C 1/ 45 101 dy. Hence, the total force dF D g. 10 exerted on the bottom is 20 

 1 y C 1 dy 10 0 ˇˇ20  2 y 4p ˇ Cy ˇ 101 .1000/.9:8/ D ˇ 5 20

4p 101 g F D 5

Z

0

 3:1516  106 N:

20

which is positive provided 0 < t < =4. Thus the beam will rotate counterclockwise until an edge is on top.

y

1 y

dy 3 y xD 10 C1

Section 7.6 Other Physical Applications (page 431)

1.

a) The pressure at the bottom is p D 9; 800  6 N/m2 . The force on the bottom is 4  p D 235; 200 N. b) The pressure at depth h metres is 9; 800h N/m2 . The force on a strip between depths h and h C dh on one wall of the tank is dF D 9; 800h  2 dh D 19; 600 h dh N. Thus, the total force on one wall is F D 19; 600

Z

Fig. 7.6-2 3.

A strip along the slant wall of the dam between depths h and h C dh has area dA D

26 200 dh D 200  dh: cos  24

The force on this strip is dF D 9; 800 h dA  2:12  106 h dh N. Thus the total force on the dam is

6 0



x

h dh D 19; 600  18 D 352; 800 N.

F D 2:12  106

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Z

24 0

h dh  6:12  108 N.

295

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SECTION 7.6 (PAGE 431)

ADAMS and ESSEX: CALCULUS 9

5.

The unbalanced force is F D 9; 800  5

20

h dh  2 ˇˇ20 h ˇ D 9; 800  5 ˇ  8:92  106 N. 2 ˇ

 h hCdh

Z

6

6

26

24

Fig. 7.6-3

5 m

p 4. The height of each triangular p face is 2 3 m and the height of the pyramid is 2 2 m. Let the angle between r 2 the triangular face and the base be  , then sin  D 3 1 and cos  D p . 3

20 m

6 m p 2 2

p 2 3

Fig. 7.6-5

2 

4

6.

4

Fig. 7.6-4

The spring force is F .x/ D kx, where x is the amount of compression. The work done to compress the spring 3 cm is 100 Ncm D W D

Z

0

y

front view of

dy p 10 2 2

p dy sec D 3dy

p p xD 2yC10 2 2

 x

W D

ı 60

2

7.

Fig. 7.6-4 A vertical slice of water with thickness dy at a distance y from the vertex of the pyramid exerts a force on the shaded strip shown in the front view,pwhich has areap p 2 3y dy m2 and which is at depth 2y C 10 2 2 m. Hence, the force exerted on the triangular face is Z 2 p p p . 2y C 10 2 2/2 3y dy F D g 0 p ˇ2 p 2 ˇˇ p 2 3 y C .5 D 2 3.9800/ 2/y ˇ ˇ 3 0

 6:1495  105 N:

296

Z

4 3

kx dx D

4

side view of one face

ˇ3 1 2 ˇˇ 9 kx dx D kx ˇ D k: ˇ 2 2 0

200 Hence, k D N/cm. The work necessary to compress 9 the spring a further 1 cm is

one face 10

3

200 9



ˇ4 1 2 ˇˇ 700 x ˇ D Ncm: 2 ˇ 9 3

A layer of water in the tank between depths h and h C dh has weight dF D g d V D 4g dh. The work done to raise the water in this layer to the top of the tank is d W D h dF D 4gh dh. Thus the total work done to pump all the water out over the top of the tank is W D 4g

8.



Z

6 0

h dh D 4  9; 800  18  7:056  105 Nm.

The horizontal cross-sectional area of the pool at depth h is  160; if 0  h  1; A.h/ D 240 80h; if 1 < h  3.

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 7.6 (PAGE 431)

The work done to empty the pool is Z 3 W D g hA.h/ dh 0  Z 1 Z 3 240h 80h2 dh 160h dh C D g 1 0 ˇ1  " ˇ3 # ˇ 80 3 ˇˇ 2ˇ 2 h ˇ D 9800 80h ˇ C 120h ˇ ˇ 3 1

0

10. When the water surface is y m above the centre of the piston face ( R  y  R), a horizontal strip on the piston face at height z m above thepcentre of the piston face, having height dz has width 2 .R2 z 2 / and so its p area is dA D 2 R2 z 2 dz. The strip is y z m below the surface of the water, and the pressure at that depth is g.y z/ D 9;800.y z/ N/m2 . Thus, the p force of the water on that strip is dF D 19;600.y z/ R2 z 2 dz Newtons. The total force of the water on the piston is

D 3:3973  106 Nm:

F D

R

D 19;600

h 3 A.h/

11.

Fig. 7.6-8 9. A layer of water between depths y and y C dy has volume d V D .a2 y 2 / dy and weight 2 2 dF D 9; 800.a y / dy N. The work done to raise this water to height h m above the top of the bowl is d W D .h C y/ dF D 9; 800.h C y/.a2

y 2 / dy Nm.

Thus the total work done to pump all the water in the bowl to that height is Z a W D 9; 800 .ha2 C a2 y hy 2 y 3 / dy 0 ˇa  y 4 ˇˇ a2 y 2 hy 3 2 D 9; 800 ha y C ˇ 2 3 4 ˇ 0  3  2a h a4 D 9; 800 C 3 4   8h 3a C 8h 3 3 D 2450a a C Nm. D 9; 800a 12 3

y

19;600.y

a

Z

1 .y=R/

sin

.y

z 2 dz

(let z D R sin  )

R sin  / R2 cos2  d

=2

ˇsin 1 .y=R/ ˇ R2 y R3 . C sin  cos  / C cos3  ˇˇ 2 3 =2  2  2  R y yR 1 3=2 y sin 1 C C R2 y 2 D 19;600 N: 2 R 4 3

8

1

p z/ R2

y

D 19;600

20

dy

Z



Initially the water occupies the bottom half of a cylinder of length X. Half of this water (say, a bottom halfcylinder of length X=2, must be moved to fill the top half of a cylinder of length X=2. By symmetry, we can accomplish this by moving a thin horizontal slice of water of thickness dy at distance y below the central axis of the cylinder to height y above that axis, that is, p X dy of wawe move a volume d V D 2 R2 y 2 2 ter up a distance p 2y. The work required to do this is d W D 2gXy R2 y 2 dy Nm. Thus the work to raise the half-cylinder of water is W D 2gX

Z

D 9;800X

R 0

Z

p y R2

R2

p

0

y 2 dy

u du D

let u D R2

y2

19;600 XR3 Nm: 3

Since no work is lost to friction, the work to push the piston in to distance X=2 is equal to this work needed to raise the water. 12. Let the time required to raise the bucket to height h m be h t minutes. Given that the velocity is 2 m/min, then t D . 2 The weight of the bucket at time t is h 16 kg .1 kg/min/.t min/ D 16 kg. Therefore, 2 the work done required to move the bucket to a height of 10 m is W Dg

Z

0

10 

16

 D 9:8 16h

Fig. 7.6-9

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 h dh 2 ˇ  10 h2 ˇˇ ˇ D 1323 Nm: 4 ˇ 0

297

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SECTION 7.6 (PAGE 431)

ADAMS and ESSEX: CALCULUS 9

8.

Section 7.7 Applications in Business, Finance, and Ecology (page 435) 1.

Cost D $4; 000 C D $11; 000:

Z

1;000

0

 6

2x 6x 2 C 6 3 10 10



V D

dx 9.

2. The number of chips sold in the first year was 1; 000

Z

52

te

t=10

0

dt D 100; 000

620; 000e

26=5

that is, about 96,580. 3. The monthly charge is Z

x

0

4 p dt 1C t

p x

let t D u2

Z px  u D8 du D 8 1 1Cu 0 0p p  D$8 x ln.1 C x/ : Z

1 1Cu



du

1 0

11.

V D

1;000e

0:02t

0

1;000 e dt D 0:02

ˇ10 ˇ ˇ D $9;063:46: ˇ

0:02t ˇ

7.

V D

298

Z

2

12

1;000e

0:08t

1;000 e dt D 0:08

ˇ12 ˇ 0:08t ˇ ˇ ˇ

2

D $5;865:64:

The present value of continuous payments of $1,000 per year for all future time at a discount rate of 2% is Z

1

0:02t

1;000e

0

dt D

1; 000 D $50; 000: 0:02

After t years, money is flowing at $.1;000 C 100t / per year. The present value of 10 years of payments discounted at 5% is Z

10

.10 C t /e

0

0:05t

dt

0

12. After t years, money is flowing at $1;000.1:1/t per year. The present value of 10 years of payments discounted at 5% is V D 1;000

0

The present value of continuous payments of $1,000 per year for 10 years beginning 2 years from now at a discount rate of 8% is

10

d V D e 0:05t dt e 0:05t V D 0:05 ˇ10 Z 0:05t ˇ 100 10 0:05t e ˇ e dt C D 100.10 C t / ˇ 0:05 ˇ 0:05 0 0 ˇ10 ˇ 100 0:05t ˇ e D 4261:23 C ˇ D $11; 477:54: 2 ˇ .0:05/

ˇ10 10 1;000 0:05t ˇˇ 0:05t 1;000e dt D V D e ˇ D $7;869:39: ˇ 0:05 0 Z

1;000e

ˇ35 ˇ ˇ D $8;655:13: ˇ

0:05t ˇ

U D 10 C t d U D dt

0

6. The present value of continuous payments of $1,000 per year for 10 years at a discount rate of 5% is

1;000 e dt D 0:05

0:05t

10

V D 100

400.10 C 5t / dt  $4; 750:37: 1 C 0:1t

10

35

10. The present value of continuous payments of $1,000 per year beginning 10 years from now and continuing for all future time at a discount rate of 5% is Z 1 1;000 0:5 V D e D $12;130:61: 1;000e 0:05t dt D 0:05 10

5. The present value of continuous payments of $1,000 per year for 10 years at a discount rate of 2% is Z

Z

V D

4. The price per kg at time t (years) is $10 C 5t . Thus the revenue per year at time t is 400.10C5t /=.1C0:1t / $/year. The total revenue over the year is Z

The present value of continuous payments of $1,000 per year for 25 years beginning 10 years from now at a discount rate of 5% is

D

13.

Z

10

e t ln.1:1/ e

0:05t

0

1;000 e t.ln.1:1/ ln.1:1/ 0:05

The amount after 10 years is

A D 5; 000

Z

10

e

0

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0:05t

dt ˇ10 ˇ 0:05 ˇ ˇ D $12; 650:23: ˇ 0

ˇ10 5;000 0:05t ˇˇ dt D e ˇ D $64;872:13: ˇ 0:05 0

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

14.

SECTION 7.7 (PAGE 435)

Let T be the time required for the account balance to reach $1;000;000. The $5; 000.1:1/t dt deposited in the time interval Œt; t C dt  grows for T t years, so the balance after T years is Z

For realistic growth functions, the maximum will occur where Q 0 .x/ D 0, that is, where F 0 .x/ D ı. 17.

T

5; 000.1:1/t .1:06/T t dt D 1; 000; 000  Z T 1; 000; 000 1:1 t dt D D 200 .1:06/T 1:06 5; 000 0 # "  1:1 T .1:06/T 1 D 200 ln.1:1=1:06/ 1:06 0

.1:1/T

.1:06/T D 200 ln

x D .k

Let P ./ be the value at time  < t that will grow to $P D P .t / at time t . If the discount rate at time  is ı./, then d P ./ D ı./P ./; d or, equivalently, dP ./ D ı./ d : P ./

ln P .0/ D

Z

 dx D 0:02x 1 dt

.t/

ˇ dx ˇˇ ˇ dt ˇ

ı./ d  D .t /;

D Pe

.t/

T

P .t /e

.t/

dt;

where

0

.t / D

Z

e) The total present value of all future harvesting revenue if the population level is maintained at 75,000 and ı D 0:05 is

ı./ d :

0

ıx:

ıx:

D 0:02.75; 000/.0:5/ D 750 whales:

d) At 5%, the interest would be .5=2/.$15; 000/ D $37; 500; 000.

t

If the logistic model dx=dt D kx.1 .x=L// is replaced with a more general growth model dx=dt D F .x/, exactly the same analysis leads us to maximize Q.x/ D F .x/

xDL=2

75; 000.$10; 000/.0:02/ D $15; 000; 000:

:

Z

1

e

0

19.

x L

 x : 150; 000

c) If the whole population of 75,000 is harvested and the proceeds invested at 2%, the annual interest will be

16. The analysis carried out in the text for the logistic growth model showed that the total present value of future harvests could be maximized by holding the population size x at a value that maximizes the quadratic expression  Q.x/ D kx 1

D $11; 900:

b) The resulting annual revenue is $750p D $7; 500; 000.

The present value of a stream of payments due at a rate P .t / at time t from t D 0 to t D T is Z



a) The maximum sustainable annual harvest is

and, taking exponentials of both sides and solving for P .0/, we get P .0/ D P .t /e

23; 333:33 80; 000

18. We are given that k D 0:02, L D 150; 000, p D $10; 000. The growth rate at population level x is

t 0

0:07 L D .80; 000/ D 23; 333:33 2k 0:24

 6.0:12/.23; 333:33/ 1

Integrating this from 0 to t , we get ln P .t /

ı/

The annual revenue from harvesting to keep the population at this level (given a price of $6 per fish) is

1:1 : 1:06

This equation can be solved by Newton’s method or using a calculator “solve” routine. The solution is T  26:05 years. 15.

We are given L D 80; 000, k D 0:12, and ı D 0:05. According to the analysis in the text, the present value of future harvests will be maximized if the population level is maintained at

0:05t

7; 500; 000 dt D

7; 500; 000 D $150; 000; 000: 0:05

If we assume that the cost of harvesting 1 unit of population is $C.x/ when the population size is x, then the effective income from 1 unit harvested is $.p C.x//. Using this expression in place of the constant p in the analysis given in the text, we are led to choose x to maximize i  h  x ıx : Q.x/ D p C.x/ kx 1 L

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299

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SECTION 7.7 (PAGE 435)

ADAMS and ESSEX: CALCULUS 9

A reasonable cost function C.x/ will increase as x decreases (the whales are harder to find), and will exceed p if x  x0 , for some positive population level x0 . The value of x that maximizes Q.x/ must exceed x0 , so the model no longer predicts extinction, even for large discount rates ı. However, the optimizing population x may be so low that other factors not accounted for in the simple logistic growth model may still bring about extinction whether it is economically indicated or not.

Section 7.8 Probability 1.

6.

9 9   0:0225 60 60 9 f .3/ D 2   16 D 0:0500 60 1 9  16 C D 0:0778 f .4/ D 2  60 36 9 2 f .5/ D 2   16 C D 0:1056 60 36 3 9  16 C D 0:1333 f .6/ D 2  60 36 9 4 f .7/ D 2   1160 C D 0:1661 60 36 11 3 f .8/ D 2   16 C D 0:1444 60 36 2 11  16 C D 0:1167 f .9/ D 2  60 36 11 1 f .10/ D 2   16 C D 0:0889 60 36 11  16 D 0:0611 f .11/ D 2  60 11 f .12/ D  1160 D 0:0336: 60 f .2/ D

(page 449)

The expected winnings on a toss of the coin are $1  0:49 C $2  0:49 C $50  0:02 D $2:47:

If you pay this much to play one game, in the long term you can expect to break even. P 2. (a) We need 6nD1 Kn D 1. Thus 21K D 1, and K D 1=21. (b) Pr.X  3/ D .1=21/.1 C 2 C 3/ D 2=7:

3. From the second previous Exercise, the mean winings is  D $2:47. Now  2 D 1  0:49 C 4  0:49 C 2;500  0:02  52:45 6:10 D 46:35:

2

The standard deviation is thus   $6:81.

4. Since Pr.X D n/ D n=21, we have D 2 D

6 X

nD1 6 X

nD1

D 21 p

D

nPr.X D n/ D

1  1 C 2  2 C  C 6  6 13 D  4:33 21 3

n2 Pr.X D n/

2 D

12 C 23 C    C 63 21

nD2

Similarly,

E.X 2 / D

12 X

nD2

n2 f .n/  57:1783;

so the standard deviation of X is

20  1:49: 3

D

5. The mean of X is

The expectation of X 2 is 9 1 C.22 C32 C42 C52 / C62 1160  15:7500: 60 6

Hence the standard deviation of X is p 15:75 3:58332  1:7059. 2 29 9 C D  0:4833. Also Pr.X  3/ D 60 6 60

p

E.X 2 /

2  2:4124:

The mean is somewhat larger than the value (7) obtained for the unweighted dice, because the weighting favours more 6s than 1s showing if the roll is repeated many times. The standard deviation is just a tiny bit smaller than that found for the unweighted dice (2.4152); the distribution of probability is just slightly more concentrated around the mean here.

1 9 C .2 C 3 C 4 C 5/  C 6  1160  3:5833: D1 60 6

300

(b) Multiplying each value f .n/ by n and summing, we get 12 X D nf .n/  7:1665:

2

20 169 D  2:22 9 9

E.X 2 / D 12 

(a) Calculating as we did to construct the probability function in Example 2, but using the different values for the probabilities of “1” and “6”, we obtain

7.

(a) The sample space consists of the eight triples .H; H; H /, .H; H; T /, .H; T; H /, .T; H; H /, .H; T; T /, .T; H; T /, .T; T; H /, and .T; T; T /.

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 7.8 (PAGE 449)

(b) We have

9.

We have f .x/ D C x on Œ0; 3. a) C is given by

Pr.H; H; H / D .0:55/3 D 0:166375

Pr.H; H; T / D Pr.H; T; H / D Pr.T; H; H / D .0:55/2 .0:45/ D 0:136125 Pr.H; T; T / D Pr.T; H; T / D Pr.T; T; H / D .0:55/.0:45/2 D 0:111375 Pr.T; T; T / D .0:45/3 D 0:091125:

(c) The probability function f for X is given by

1D Hence, C D

Z

3

C x dx D

0

2 . 9

Z

2  D E.X/ D 9

f .1/ D 3  .0:55/.0:45/2 D 0:334125 2

f .3/ D .0:55/3 D 0:166375: (d) Pr.X  1/ D 1

(e) E.X/ D 0f .0/C1f .1/C2f .2/C3f .3/ D 1:6500.

8. The number of red balls in the sack must be 0:620 D 12. Thus there are 8 blue balls. (a) The probability of pulling out one blue ball is 8=20. If you got a blue ball, then there would be only 7 blue balls left among the 19 balls remaining in the sack, so the probability of pulling out a second blue ball is 7=19. Thus the probability of pulling out two 8 7 14 blue balls is  D . 20 19 95 (b) The sample space for the three ball selection consists of all eight triples of the form .x; y; z/, where each of x; y; z is either R(ed) or B(lue). Let X be the number of red balls among the three balls pulled out. Arguing in the same way as in (a), we calculate Pr.X Pr.X

Pr.X

Pr.X

Z

2 Since E.X / D 9 variance is 2

Pr.X D 0/ D 0:908875.

8 7 6 14 D 0/ D Pr.B; B; B/ D   D 20 19 18 285  0:0491 D 1/ D Pr.R; B; B/ C Pr.B; R; B/ C Pr.B; B; R/ 12 8 7 28 D3   D  0:2947 20 19 18 95 D 2/ D Pr.R; R; B/ C Pr.R; B; R/ C Pr.B; R; R/ 8 44 12 11   D  0:4632 D3 20 19 18 95 12 11 10 11 D 3/ D Pr.R; R; R/ D   D 20 19 18 57  0:1930

Thus the expected value of X is

3 0

ˇ3 2 3 ˇˇ x ˇ D 2: x dx D 27 ˇ 2

0

ˇ3 9 2 4 ˇˇ x ˇ D , the x dx D 36 ˇ 2

3

3

0

0

 2 D E.X 2 /

2 D

9 2

4D

1 ; 2

p and the standard deviation is  D 1= 2. c) We have Pr. D

  X   C / D

. C /2

/2

. 9

D

2 9

Z

C

x dx  

4  0:6285: 9

10. We have f .x/ D C x on Œ1; 2. a) To find C , we have

1D Hence, C D

Z

2

1

ˇ2 3 C 2 ˇˇ C x dx D x ˇ D C: 2 ˇ 2 1

2 . 3

b) The mean is 2  D E.X/ D 3

Z

2 Since E.X / D 3 variance is 2

14 28 44 11 E.X/ D 0  C1 C2 C3 285 95 95 57 9 D D 1:8: 5

0

b) The mean is

f .0/ D .0:45/3 D 0:911125

f .2/ D 3  .0:55/ .0:45/ D 0:408375

ˇ3 9 C 2 ˇˇ x ˇ D C: 2 ˇ 2

2 1

Z

1

2

1

 2 D E.X 2 /

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ˇ2 2 3 ˇˇ 14  1:556: x dx D x ˇ D 9 ˇ 9 2

ˇ2 1 4 ˇˇ 5 x dx D x ˇ D , the 6 ˇ 2 3

1

2 D

5 2

196 13 D 81 162

301

lOMoARcPSD|6566483

SECTION 7.8 (PAGE 449)

ADAMS and ESSEX: CALCULUS 9

Since

and the standard deviation is r 13 D  0:283: 162

E.X 2 / D

D 11.

2 3

  X   C / D

. C /2

.

/2

3

D

Z

C

x dx

 

0

ˇ1 Z 1 C 3 ˇˇ C 2 1D C x dx D x ˇ D : 3 ˇ 3 0

D

3

/

3 4

r

C

D

3 80

x 2 dx

Hence, C D

 0

C sin x dx D

1 . 2

2

8

 0:684:

4

ˇ ˇ ˇ C cos x ˇ D 2C: ˇ 0

We have f .x/ D C.x

Z

Z

C

sin x dx  

x 2 / on Œ0; 1.

a) C is given by

1D

Z

1

C.x

0

2

x / dx D C



Hence, C D 6.

1  D E.X/ D 2

1 2

  X   C / D

i 1h cos. C / cos. / 2 D sin  sin  D sin   0:632:

13.

b) The mean is

x2 2

x3 3

 ˇˇ1 C ˇ ˇ D : ˇ 6 0

b) The mean, variance, and standard deviation are



x sin x dx

0

U Dx d V D sin x dx d U D dx ˇ V D cos x   ˇ Z  1 ˇ D x cos x ˇ C cos x dx ˇ 2 0 0  D 1:571: D 2

302

Pr.

 0:668:

a) To find C , we calculate 1D

s

D

12. We have f .x/ D C sin x on Œ0; . Z

2 2 8 D  0:467 4 4

4 2

c) Then

 

!3

2

and the standard deviation is

c) We have

  X   C / D 3

4/:

 2 D E.X 2 / 2 D

b) The mean, variance, and standard deviation are Z 1 3  D E.X/ D 3 x 3 dx D 4 0 Z 1 9 3 9 3  2 D E.X 2 / 2 D 3 x 4 dx D D 16 5 16 80 0 p  D 3=80: Z

1 2 . 2

Hence, the variance is

0

Hence, C D 3.

D . C / . r !3 3 3 D C 4 80

x 2 sin x dx

0

U Dx d V D cos x dx d"U D dx V D ˇ sin Zx  # ˇ  1 2 ˇ  C 2 x sin x ˇ sin x dx D ˇ 2 0

a) C is given by

3



0

4  0:5875: 3

We have f .x/ D C x 2 on Œ0; 1.

Pr.

Z

d V D sin x dx U D x2 d U D 2x dx ˇ VZD cos x   ˇ  1 ˇ x 2 cos x ˇ C 2 x cos x dx D ˇ 2 0

c) We have Pr.

1 2

1

1 .x 2 x 3 / dx D 2 0 Z 1 2  D6 .x 3 x 4 / dx

 D E.X/ D 6  2 D E.X 2 /

Z

3 1 1 D D 10 4 20 p  D 1=20:

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0

1 4

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 7.8 (PAGE 449)

c) Finally,

c) We have

Pr.

Z .1=2/C .x   X   C / D 6 .1=2/  " #   Z .1=2/C 1 1 2 D6 dx x 4 2 .1=2/  Let u D x 21 du D dx   Z   1 u2 du D 12 D 12 4 4 0   1 12 1  0:626: D p 20 4 60

14.

  X   C / Z C D k2 xe kx dx Let u D kx   du D k dx Z k.C / D ue u du

x 2 / dx

Pr.

k.  /

3

Z k.C / C e u du ˇ ˇ k.  / k.  / p p p 2/e .2 C 2/e .2C 2/ C .2

D

 3

ˇk.C / ˇ uˇ

ue

D

e  0:738:

p .2C 2/

.2

Ce

p

.2

p

2/

2/

It was shown in Section 6.1 (p. 349) that Z If In D

n

x

x e

Z

1

dx D

xne

x

Since I0 D

Z

1

kx

0

R

R e

e

x

0

Let u D kx; then xn e

x e

Cn

Z

15. x

n 1

x

e

dx:

dx D

1

D nIn

if n  1:

1

dx D 1, therefore In D nŠ for n  1. Z

k nC1

Now let f .x/ D C xe

1

un e

u

0

kx

1 nŠ In D nC1 : k nC1 k

du D

on Œ0; 1/.

Z

1

xe

kx

0

dx D

C : k2

0

dx D

C 2

Z

1

e

1

x2

dx D

C

p 2



:

b) The mean, variance, and standard deviation are ˇ Z 1 2 1 e x ˇˇ 2 1 x2 dx D p ˇ D p D p xe  0  ˇ  0 Z 1 1 2 2 2 D x 2 e x dx Cp   0 U Dx d U D dx 1 2 Cp  

D

2

d V D xe x dx 2 V D 12 e x ˇ1 ! Z x x 2 ˇˇ 1 1 x2 e e dx ˇ C ˇ 2 2 0 p0    1 1 1 D 0C  2 2 2 

Z C 2 2 e x dx   X   C / D p    p Let x D z= 2 p dx D dz= 2 r Z p 2.C / 2 2 D e z =2 dz: p  2.  / p p But 2. /  0:195 and 2. C /  1:40. Thus, if Z is a standard normal random variable, we obtain by interpolation in the table on page 386 in the text, Pr.

 D E.X/ D k 2 Z

x2

c) We have

b) The mean is

E.X 2 / D k 2

e

1 2 Cp   r 1 1 D  0:426: 2 

Hence, C D k 2 .

Since

1

D

a) To find C , observe that 1DC

Z

p Thus C D 2= .

C nIn

1

a) We have 1DC

dx, then

n

R!1

1

x

0

In D lim

Z

n

1

Z

1

x2e

kx

0

x3e

0

then the variance is  2 D E.X 2 /

kx

dx D k 2 

dx D k 2

2 D

6 k2



6 k4

2 k3





D

4 2 D 2 k2 k p

D

2 : k

6 ; k2

Pr.

2 and the standard deviation is  D . k

  X   C / D 2Pr.0:195  Z  1:400/  2.0:919 0:577/  0:68:

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303

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SECTION 7.8 (PAGE 449)

16. No. The identity constant C .

17.

Z

1 1

1 p e 2 Z 1 mean D p  2

f; .x/ D

ADAMS and ESSEX: CALCULUS 9

b) For f .x/ D ke kx on Œ0; 1/, we know that 1 (Example 6). Thus  2 < 0 and  D  D k 3  C 2 D . We have k   3 Pr.jX j  2/ D Pr X  k Z 1 kx Dk e dx 3=k ˇ1 ˇ D e 3  0:050: D e kx ˇˇ

C dx D 1 is not satisfied for any

.x /2 =2 2



1

xe

.x /2 =2 2

Let z D

dx

1

dz D

x

 

1 dx 

Z 1 1 2 D p . C z/e z =2 dz 2 1 Z 1  2 e z =2 dz D  D p 2 1  variance D E .x /2 Z 1 1 2 2 D p .x /2 e .x / =2 dx  2 1 Z 1 1 2  2 z 2 e z =2 dz D Var.Z/ D  D p  2 1

3=k

1 2 2 p e .x / =2 , which has mean   2 and standard deviation , we have

c) For f; .x/ D Pr.jX

j  2/ D 2Pr.X   2/ Z  2 1 D2 p e  2 1

Z

0

1

2 dx D lim tan R!1  1 C x2

1

.R/ D

dz D

 D E.X/ D

2 

Z

1 0

20.

x dx 1 C x2

D

b

Z

1

e

t=20

12

dt D 1 12=20

0

1 20

Z

12

e

t=20

dt

0

 0:549:

The probability that the system will last at least 12 hours is about 0.549. If X is distributed normally, with mean  D 5; 000, and standard deviation  D 200, then Pr.X  5500/ Z 1 1 p e D 200 2 5500 Let z D

a

p : 2 3

bCa b a Since  C 2 D C p > b, and similarly, 2 3  2 < a, therefore Pr.jX j  2/ D 0.

304

1 20

ˇ12 ˇ t=20 ˇ D1Ce ˇ De ˇ

21.

bCa ; D 2

1 dx 

The density function for T is f .t / D ke k t on Œ0; 1/, 1 1 D (see Example 6). Then where k D  20 Pr.T  12/ D

No matter what the cost per game, you should be willing to play (if you have an adequate bankroll). Your expected winnings per game in the long term is infinite.

a) The density function for the uniform distribution on Œa; b is given by f .x/ D 1=.b a/, for a  x  b. By Example 5, the mean and standard deviation are given by

 

from the table in this section.

1 D lim ln.1 C R2 / D 1: R!1 

19.

dx

Z 2 2 2 e z dz D p 2 1 D 2Pr.Z  2/  2  0:023 D 0:046

2   D 1;  2

therefore f .x/ is a probability density function on Œ0; 1/. The expectation of X is

x

Let z D

2 18. Since f .x/ D > 0 on Œ0; 1/ and .1 C x 2 / 2 

.x /2 =2 2

dz D

.x 5000/2 =.22002 /

x

5000 200

dx 200

Z 1 1 2 D p e z =2 dz 2 5=2 D Pr.Z  5=2/ D Pr.Z 

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dx

5=2/  0:006

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 7.9 (PAGE 458)

from the table in this section.

2.

22. If X is the random variable giving the spinner’s value, then Pr.X D 1=4/ D 1=2 and the density function for the other values of X is f .x/ D 1=2. Thus the mean of X is   Z 1 1 3 1 1 1 Pr X D x f .x/ dx D C D : C 4 4 8 4 8 0

 D E.X/ D Also,

  Z 1 1 1 1 19 1 Pr X D C C D x 2 f .x/ dx D 16 4 32 6 96 0 9 11 19 D :  2 D E.X 2 / 2 D 96 64 192

E.X 2 / D

3.

p 11=192.

Thus  D 23.

4.

(a) The integral exists for p D 0 as a degenerate case. For p > 0, Z

1

x p S˛ .x/dx

1

D 2 lim

y!1

D 2 lim

y!1



Z

 x c˛ x p

c˛ p

˛

x

p ˛

 CO x

.1C˛/

CO x

p

.1C2˛/

  2˛



dx



jxDy

!

5.

This limit will be finite if p < ˛. The case p D ˛ is logarithmically divergent. (b) The mean will not exist for ˛  1. The variance will not exist for ˛ < 2.

6.

x2 dy D 2 ) y 2 dy D x 2 dx dx y y3 x3 D C C1 ; or x 3 y 3 D C 3 3 y D 0 is a constant solution. Otherwise, dy D x2y2 dx Z Z dy D x 2 dx y2 1 1 1 D x3 C C y 3 3 3 : ) yD x3 C C Y D 0 is a constant solution. Otherwise dY dY D tY ) D t dt dt Y t2 2 ln Y D C C1 ; or Y D C e t =2 2 dx D e x sin t dt Z Z e

24. 1 D D

FS .x/ D Pr.X > x/ D Z

1 x

n c˛ 

h c ˛  ˛

.1C˛/

˛

 CO 

CO 



Z

1

.1C2˛/

i

jDx

x



o

) d

7.

c˛ ˛ x ; ˛

Section 7.9 First-Order Differential Equations (page 458) y D 0 is a constant solution. Otherwise y dy D dx 2x dy dx 2 D y x 2 ln y D ln x C C1 ) y2 D C x

dx D

e

S˛ ./d 

x

where higher order terms were discarded in the last step.

1.

y D 1=3 is a constant solution. Otherwise 3y 1 dy D dx x Z Z dy dx D 3y 1 x 1 1 ln j3y 1j D ln jxj C ln C 3 3 3y 1 DC x3 1 ) y D .1 C C x 3 /: 3

8.

x

D xD

sin t dt

cos t C ln.cos t C C /:

y D 1 and y D 1 are constant solutions, Otherwise dy dy D dx D 1 y2 ) dx 1 y2   1 1 1 C dy D dx 2 1Cy 1 y ˇ ˇ 1 ˇˇ 1 C y ˇˇ ln D x C C1 2 ˇ1 yˇ 1Cy C e 2x 1 D C e 2x or y D 1 y C e 2x C 1

dy dx Z dy 1 C y2 tan 1 y ) y

D 1 C y2 Z D dx

DxCC D tan.x C C /:

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305

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SECTION 7.9 (PAGE 458)

9.

ADAMS and ESSEX: CALCULUS 9

dy dy D dt D 2 C ey ) dt 2 C ey Z Z y e dy D dt 2e y C 1 1 ln.2e y C 1/ D t C C1 2  2e y C 1 D C2 e 2t ; or y D ln C e

13. 2t

1 2



10. y D 0 and y D 1 are constant solutions. For the other solutions we have dy D y 2 .1 y/ dx Z Z dy D dx D x C K: y 2 .1 y/ Expand the left side in partial fractions: C A B 1 D C 2 C y 2 .1 y/ y y 1 y A.y y 2 / C B.1 y/ C Cy 2 D y 2 .1 y/ ( A C C D 0I ) A B D 0I ) A D B D C D 1: B D 1: Hence,  Z  Z 1 1 1 dy D C C dy y 2 .1 y/ y y2 1 y 1 D ln jyj ln j1 yj: y Therefore,

11.

dy dx

1 x2 d dx y x2

ˇ ˇ ˇ y ˇ ˇ ln ˇˇ 1 yˇ

306

1 C C 2: x x

R dy Cy D e x . Let  D dx D x, then e  D e x , dx

  dy dy d x .e y/ D e x C ex y D ex C y D e 2x dx dx dx Z 1 2x x 2x ) e y D e dx D e C C: 2 Hence, y D

15.

yDx

16.

1 x e C Ce 2

x

.

 Z dy 1 dx D e x Cy Dx  D exp dx d x .e y/ D e x .y 0 C y/ D xe x dx Z

ex y D

2y 1 dy . Let C D 12. We have 2 dx x x Z 2 D dx D 2 ln x D ln x 2 , then e  D x 2 , and x d 2 dy .x y/ D x 2 C 2xy dx  dx   2y 1 dy C D x2 D1 D x2 dx x x2 Z ) x2y D dx D x C C yD

We have and

1 D x C K: y

2 y D x2 (linear) x Z  2 1  D exp dx D 2 x x dy 2 yD1 dx x 3 y D1 x2 D x C C; so y D x 3 C C x 2

)

14.

 Z dy 2 dx D e 2x C 2y D 3  D exp dx d 2x .e y/ D e 2x .y 0 C 2y/ D 3e 2x dx 3 3 e 2x y D e 2x C C ) y D C C e 2x 2 2

xe x dx D xe x

1 C Ce

ex C C

x

R dy We have C 2e x y D e x . Let  D 2e x dx D 2e x , dx then d  2ex  x x dy C 2e x e 2e y e y D e 2e dx dx   dy x x D e 2e C 2e x y D e 2e e x : dx Therefore, x

e 2e y D

Hence, y D

Z

Let u D 2e x du D 2e x dx Z 1 2ex 1 u e du D e C C: D 2 2

1 C Ce 2

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x

e 2e e x dx

2e x

.

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

17.

18.

dy C 10y D 1; y dt Z  D 10 dt D 10t

1 10



D

2 10

22.

dy d 10t .e y/ D e 10t C 10e 10t y D e 10t dt dt 1 10t e 10t y.t / D e CC 10  e e 2e 1 2 D CC ) C D y 10 D 10 ) 10 10 10 1 1 yD C e 1 10t : 10 10 dy C 3x 2 y D x 2 ; y.0/ D 1 dx Z D

23.

24.

20.

sin x

y C .cos x/y D 2xe ; Z  D cos x dx D sin x

tan

y.x/ D 1 C

Z

y./ D 0 ) 0 D  C C ) C D

21.

 2 /e Z x y.x/ D 2 C 0

sin x

2

x 1

dy D e y; dx ey D x C C

÷

3 D y.0/ D ln C

÷

2 D0 CC ÷ p y D 4 C x2:

y.1/ D 1

y D ln.x C e 3 /: 25.

y D ln.x C C / C D e3

÷

Since a > b > 0 and k > 0,

26.

 ab e .b

a/k t

be .b a/k t ab.0 1/ D b: D 0 a t!1

lim x.t / D lim

t!1

2

t!1

D lim

 ab e .b

a

a/k t

.b a/k t be  ab 1 e .a

b ae .a ab.1 0/ D D a: b 0

y.0/ D 2

27.

1



Since b > a > 0 and k > 0,

t!1

t dt y.t /

÷

i.e. e y dy D dx

lim x.t / D lim



y.0/ D 1

x/:

y.t / dt t .t C 1/

:

x dy D ; i.e. y dy D x dx dx y y2 D x2 C C 2

1

y./ D 0

2

÷

y dy D ; for x > 0 dx x.x C 1/ dx dx dx dy D D y x.x C 1/ x xC1 x ln y D ln C ln C xC1 Cx ; ÷ 1 D C =2 yD xC1 2x yD : xC1 Z x y.x/ D 3 C e y dt ÷ y.0/ D 3

2x dx D x 2 C C

y D .x 2

.y.t //2 dt 1 C t2

t!1

d sin x .e y/ D e sin x .y 0 C .cos x/y/ D 2x dx Z

e sin x y D

0

y D 1=.1

y.1/ D 3e ) 3 D 1 C C ) C D 2 0

x

0

x 2 y 0 C y D x 2 e 1=x ; y.1/ D 3e 1 1=x 0 y C 2y D e Zx 1 1 D dx D x2 x   d  1=x  1 e y D e 1=x y 0 C 2 y D 1 dx x Z e 1=x y D 1 dx D x C C y D .x C 2/e 1=x :

Z

y.x/ D 1 C

y2 dy D ; i.e. dy=y 2 D dx=.1 C x 2 / dx 1 C x2 1 D tan 1 x C C y 1D0CC ÷ C D 1

3x 2 dx D x 3

d x3 3 3 dy 3 .e y/ D e x C 3x 2 e x y D x 2 e x dx dx Z 1 3 3 3 e x y D x 2 e x dx D e x C C 3 1 2 y.0/ D 1 ) 1 D C C ) C D 3 3 2 1 3 yD C e x : 3 3

19.

SECTION 7.9 (PAGE 458)

1



a

b/k t b/k t

The solution given, namely

C D4

xD

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ab e .b be .b

a/k t a/k t

1 a



;

307

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SECTION 7.9 (PAGE 458)

ADAMS and ESSEX: CALCULUS 9

Let a2 D mg=k, where a > 0. Thus, we have

is indeterminate (0/0) if a D b. If a D b the original differential equation becomes

Z

dx D k.a x/2 ; dt which is separable and yields the solution Z Z dx 1 D k dt D k t C C: D a x .a x/2 1 1 1 Since x.0/ D 0, we have C D , so D kt C . a a x a Solving for x, we obtain

kt dv D CC a2 ˇ v 2 ˇ m ˇa C vˇ 1 ˇ D kt C C ln ˇ 2a ˇ a v ˇ m r ˇ ˇ ˇa C vˇ ˇ D 2ak t C C1 D 2 kg t C C1 ln ˇˇ a vˇ m m p aCv 2t kg=m D C2 e : a v

a2 k t : 1 C ak t This solution also results from evaluating the limit of solution obtained for the case a ¤ b as b approaches a (using l’H^opital’s Rule, say). xD

dv D mg kv has constant solution dt v D mg=k. However this solution does not satisfy the initial condition v.0/ D 0. For other solutions we separate variables: Z Z dv D dt k g v ˇm ˇ k ˇˇ m ˇˇ lnˇg v ˇ D t C C: k m m k Since v.0/ D 0, therefore C D ln g. Also, g v k m remains positive for all t > 0, so g m ln Dt k k v g m k g v m D e k t=m g  mg  ) v D v.t / D 1 e k t=m : k mg , the constant solution of the Note that lim v.t / D t!1 k differential equation noted earlier. This limiting velocity can be obtained directly from the differential equation by dv setting D 0. dt p 29. y D mg=k is a constant solution of the equation. For other solutions we proceed by separation of variables:

Assuming v.0/ D 0, we get C2 D 1. Thus p a C v D e 2t kg=m .a v/ p    p  v 1 C e 2t kg=m D a e 2t kg=m 1 r  mg  2t pkg=m e D 1 k p r mg e 2t kg=m 1 p vD k e 2t kg=m C 1

28. The equationt m

dv D mg kv 2 dt k 2 dv Dg v dt m dv D dt k 2 g v Z m Z k kt dv D dt D C C: mg 2 m m v k

m

308

Clearly v ! setting

30.

r

mg as t ! 1. This also follows from k

dv D 0 in the given differential equation. dt

The balance in the account after t years is y.t / and y.0/ D 1000. The balance must satisfy dy y2 D 0:1y dt 1; 000; 000 dy 105 y y 2 D dt 106 Z Z dy dt D 105 y y 2 106  Z  1 1 t 1 C 5 dy D 6 105 y 10 y 10 t ln jyj ln j105 yj D C 10 105 y D e C .t=10/ y 105 y D C .t=10/ : e C1

C 105

Since y.0/ D 1000, we have 1000 D y.0/ D

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105 C1

eC

)

C D ln 99;

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

and 99e The balance after 1 year is

t=10

105

yD

99e

Hence,

105

yD

1=10

C1

REVIEW EXERCISES 7 (PAGE 459)

C1

: .500 C t /5 x D 0:12

 $1; 104:01:

t!1

105

t!1

e .4:60

0:1t/

C1

D

.500 C t /5 dt D 0:02.500 C t /6 C C

) x D 0:02.500 C t / C C.500 C t /

5

:

Since x.0/ D 50, we have C D 1:25  1015 and

As t ! 1, the balance can grow to lim y.t / D lim

Z

x D 0:02.500 C t / C .1:25  1015 /.500 C t /

105 D $100; 000: 0C1

5

:

After 40 min, there will be

For the account to grow to $50,000, t must satisfy

x D 0:02.540/ C .1:25  1015 /.540/

100; 000 50; 000 D y.t / D 99e t=10 C 1 ) 99e t=10 C 1 D 2 ) t D 10 ln 99  46 years:

5

D 38:023 kg

of salt in the tank.

Review Exercises 7 (page 459)

31. The hyperbolas xy D C satisfy the differential equation y Cx

dy D 0; dx

or

dy D dx

y : x

1. 3 cm

Curves that intersect these hyperbolas at right angles must x dy D , or x dx D y dy, a separated therefore satisfy dx y equation with solutions x 2 y 2 D C , which is also a family of rectangular hyperbolas. (Both families are degenerate at the origin for C D 0.)

1 cm 5 cm

32. Let x.t / be the number of kg of salt in the solution in the tank after t minutes. Thus, x.0/ D 50. Salt is coming into the tank at a rate of 10 g=L  12 L=min D 0:12 kg=min. Since the contents flow out at a rate of 10 L=min, the volume of the solution is increasing at 2 L=min and thus, at any time t , the volume of the solution is 1000 C 2t L. x.t / L. Hence, Therefore the concentration of salt is 1000 C 2t salt is being removed at a rate

Fig. R-7-1 The volume of thread that can be wound on the left spool is .32 12 /.5/ D 40 cm3 . The height of the winding region of the right spool at distance r from the central axis of the spool is of the form h D A C Br. Since h D 3 if r D 1, and h D 5 if r D 3, we have A D 2 and B D 1, so h D 2 C r. The volume of thread that can be wound on the right spool is

Therefore,

Z

5x dx D 0:12 dt 500 C t dx 5 C x D 0:12: dt 500 C t

2

5 dt D 5 ln j500 C t j D ln.500 C t /5 for 500 C t t > 0. Then e  D .500 C t /5 , and i dx d h C 5.500 C t /4 x .500 C t /5 x D .500 C t /5 dt dy   dx 5x D .500 C t /5 C dy 500 C t D 0:12.500 C t /5 :

1 cm 5 cm

3 cm

1 cm

5x.t / x.t / kg=L  10 L=min D kg=min: 1000 C 2t 500 C t

Let  D

3 cm

Z

3 1

ˇ3  100 r 3 ˇˇ 2 cm3 : r.2 C r/ dr D 2 r C ˇ D 3 ˇ 3 1

100 .1; 000/ D 833:33 m of The right spool will hold 3  40 thread. 2.

Let A.y/ be the cross-sectional area of the bowl at height y above the bottom. When the depth of water in the bowl is Y , then the volume of water in the bowl is

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V .Y / D

Z

Y

A.y/ dy: 0

309

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REVIEW EXERCISES 7 (PAGE 459)

ADAMS and ESSEX: CALCULUS 9

The water evaporates at a rate proportional to exposed surface area. Thus 60ı

dV D kA.Y / dt dV dY D kA.Y / d Y dt dY A.Y / D kA.Y /: dt 10 cm

Hence d Y =dt D k; the depth decreases at a constant rate. 3. The barrel is generated by revolving x D a by 2 , . 2  y  2/, about the y-axis. Since the top and bottom disks have radius 1 ft, we have a 4b D 1. The volume of the barrel is V D2

Z

2

.a

0

 D 2 a2 y 

DD 2 2a2

Fig. R-7-4 5.

by 2 /2 dy ˇˇ2 ˇ ˇ ˇ 0 32 16 ab C b 2 : 3 5

2aby 3 b2 y 5 C 3 5

6.

32 16 b.1 C 4b/ C b 2 3 5 60 2 D 0: 128b C 80b C 15 



1 cosh.ax/ from x D 0 to x D 1 is a Z 1q Z 1 sD 1 C sinh2 .ax/ dx D cosh.ax/ dx 0 0 ˇ1 ˇ 1 1 ˇ D sinh.ax/ˇ D sinh a: ˇ a a

The arc length of y D

0

Since V D 16 and a D 1 C 4b, we have  2 2.1 C 4b/2

x

D 16

Solving this quadratic gives two solutions, b  0:0476 and b  0:6426. Since the second of these leads to an unacceptable negative value for a, we must have b  0:0476, and so a D 1 C 4b  1:1904.

1 We want sinh a D 2, that is, sinh a D 2a. Solving this a by Newton’s Method or a calculator solve function, we get a  2:1773. p The area of revolution of y D x, .0  x  6/, about the x-axis is s  2 Z 6 dy S D 2 dx y 1C dx 0 r Z 6 p 1 x 1C dx D 2 4x 0 r Z 6 1 D 2 x C dx 4 0   ˇ6   4 4 125 1 1 3=2 ˇˇ 62 D sq. units. xC D ˇ D ˇ 3 4 3 8 8 3 0

4. A vertical slice parallel to the top ridge of the solid at distance x to the right of the centre p p is a rectangle of base 2 100 x 2 cm�and height 3.10 x/ cm. Thus the solid has volume V D2

Z

10

p

3.10

p x/2 100

0

p Z D 40 3

10 0

p

100

x 2 dx

x 2 dx p Z 4 3

0

Let u D 100 x 2 du D 2x dx p 100 p Z 100 p u du D 40 3 2 3 4  0  p 4 D 1; 000 3  cm3 : 3

310

10

p x 100

x 2 dx

7.

The region is a quarter-elliptic disk with semi-axes a D 2 and b D 1. The area of the region is A D ab=4 D =2. The moments about the coordinate axes are s Z 2 x2 x2 dx Let u D 1 MxD0 D x 1 4 4 0 x du D dx 2 Z 1 p 4 D2 u du D 3 0  Z  1 2 x2 MyD0 D dx 1 2 0 4 ˇ  2 2 x 3 ˇˇ 1 x D ˇ D : 2 12 ˇ 3 0

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INSTRUCTOR’S SOLUTIONS MANUAL

CHALLENGING PROBLEMS 7 (PAGE 459)

Thus x D MxD0 =A D 8=.3/ and y D MyD0 =A D 4=.3/. The centroid is 

or, equivalently, f .a/ C g.a/ D 2a. Thus f and g must satisfy

8=.3/; 4=.3/ .

f .x/ C g.x/ D 2x

for every x > 0.

8. y 11.

1

Z dy 3y dx dy D ) D3 dx x 1 y x 1 ) ln jyj D ln jx 1j3 C ln jC j

) y D C.x 1/3 : Since y D 4 when x D 2, we have 4 D C.2 the equation of the curve is y D 4.x 1/3 .

3

x

1/3 D C , so

12. The ellipses 3x 2 C 4y 2 D C all satisfy the differential equation Fig. R-7-8

6x C 8y

Let the disk have centre (and therefore centroid) at .0; 0/. Its area is 9. Let the hole have centre (and therefore centroid) at .1; 0/. Its area is . The remaining part has area 8 and centroid at .x; 0/, where

13.

5

20; 000 20 dy D 20; 000 ln  27; 726 Ncm: y 5

10. We are told that for any a > 0, 

Z a h Z 2  2 i f .x/ g.x/ dx D 2 0

a 0

h i x f .x/ g.x/ dx:

Differentiating both sides of this equation with respect to a, we get 

2 f .a/

 2 h g.a/ D 2a f .a/

i g.a/ ;

Z

2

sin.2 t /e 0:04.2

0

t/

dt  $8; 798:85:

(We omit the details of evaluation of the integral, which is done by the method of Example 4 of Section 7.1.)

We are told that F D 1; 000 N when y D 20 cm. Thus k D 20; 000 Ncm. The work done by the piston as it descends to 5 cm is 20

3x : 4y

The original $8,000 grows to $8; 000e 0:08 in two years. Between t and t C dt , an amount $10; 000 sin.2 t / dt comes in, and this grows to $10; 000 sin.2 t /e 0:04.2 t/ dt by the end of two years. Thus the amount in the account after 2 years is 8; 000e 0:08 C10; 000

k kA D : F .y/ D P .y/A D Ay y

Z

dy D dx

The family is given by y 3 D C x 4 .

9. Let the area of cross-section of the cylinder be A. When the piston is y cm above the base, the volume of gas in the cylinder is V D Ay, and its pressure P .y/ satisfies P .y/V D k (constant). The force exerted by the piston is

W D

or

A family of curves that intersect these ellipses at right 4y dy D . angles must therefore have slopes given by dx 3x Thus Z Z dy dx 3 D4 y x 3 ln jyj D 4 ln jxj C ln jC j:

.9/.0/ D .8/x C ./.1/: Thus x D 1=8. The centroid of the remaining part is 1=8 ft from the centre of the disk on the side opposite the hole.

dy D 0; dx

Challenging Problems 7 (page 459) 1.

a) The nth bead extends from x D .n 1/ to x D n, and has volume Z n Vn D  e 2kx sin2 x dx .n 1/ Z  n D e 2kx .1 cos.2x// dx 2 .n 1/ Let x D u C .n Zdx D du

  2ku 2k.n e e 2 0 Z   D e 2k.n 1/ e 2 0 D e 2k.n 1/ V1 : D

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1/

1/

2ku

h 1 .1

cos.2u C 2.n cos.2u// du

i 1// du

311

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CHALLENGING PROBLEMS 7 (PAGE 459)

e 2k n V1 VnC1 D D e Vn e 2k.n 1/ V1 pends on k but not n. Thus

b) VnC1 =Vn D 1=2 if if k D .ln 2/=.2/.

2k

ADAMS and ESSEX: CALCULUS 9

or, equivalently, a.100 k 2 /2 D 4. The volume of the pool is

; which de-

2k D ln.1=2/ D

ln 2, that is,

VP D 2a D 2a

c) Using the result of Example 4 in Section 7.1, we calculate the volume of the first bead: Z   2kx V1 D e .1 cos.2x// dx 2 0 ˇ ˇ  e 2kx .2 sin.2x/ 2k cos.2x// ˇˇ e 2kx ˇˇ D ˇ ˇ ˇ 4k ˇ 2 4.1 C k 2 / 0 0   2k 2k .1 e / .k ke / D 4k 4.1 C k 2 /  D .1 e 2k /: 4k.1 C k 2 /

 .1 e 2k / 4k.1 C k 2 / h  2   1 C e 2k C e 2k C    C e

 .1 4k.1 C k 2 /  D .1 4k.1 C k 2 /

D

e

2k

e

2k n

/

1 e 1 e

2k

2k n

n

10

r 2 /.r 2

r.100

k 2 / dr

k



250; 000 3

 1 6 k : 12

2; 500k 2 C 25k 4

The volume of the hill is VH D 2a

Z

k 0

 r.r 2 100/.r 2 k 2 / dr D 2a 25k 4

 1 6 k : 12

These two volumes must be equal, so k 2 D 100=3 and k  5:77 m. Thus a D 4=.100 k 2 /2 D 0:0009. The volume of earth to be moved is VH with these values of a and k, namely "

By part (a) and Theorem 1(d) of Section 6.1, the sum of the volumes of the first n beads is Sn D

Z

2.0:0009/ 25

1i

3.



100 3

2

1 12



100 3

4 #

 140 m3 :

y D ax C bx 2 C cx 3 .h; r/

y

2k

x

/:

Thus the total volume of all the beads is V D lim Sn D n!1

 cu. units.: 4k.1 C k 2 /

Fig. C-7-3 f .x/ D ax C bx 2 C cx 3 must satisfy f .h/ D r, f 0 .h/ D 0, and f 0 .x/ > 0 for 0 < x < h. The first two conditions require that ah C bh2 C ch3 D r

2. 10 m

a C 2bh C 3ch2 D 0;

1m

from which we obtain by solving for b and c, bD

3r

2ah ; h2

cD

ah

2r h3

:

The volume of the nose cone is then Fig. C-7-2 h.r/ D a.r 2

h0 .r/ D 2ar.r 2

100/.r 2

k 2 /;

k 2 / C 2ar.r 2

V .a/ D 

where 0 < k < 10 100/ D 2ar.2r 2

2

2

100

The deepest point occurs where 2r D 100 C k , i.e., r 2 D 50 C .k 2 =2/. Since this depth must be 1 m, we require    2 k2 k 50 50 D 1; a 2 2

312

k 2 /:

Z h 2 h .13ahr C 78r 2 C 2a2 h2 /: f .x/ dx D 210 0

Solving d V =da D 0 gives only one critical point, a D 13r=.4h/. This is unacceptable, because the condition f 0 .x/ > 0 on .0; h/ forces us to require a  0. In fact f 0 .x/ D a C

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2.3r

2ah/ h2

xC

3.ah 2r/ 2 x h3

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

CHALLENGING PROBLEMS 7 (PAGE 459)

To minimize this expression for a > 0 we should take k D 0. This gives f .x/ D ax 2 .1 x/. To minimize V .a; k/ for a < 0 we should take k D 1. This gives f .x/ D ax.1 x/2 . Since we want the maximum value of f to be 2 in either case, we calculate the critical points of these two possible functions. For a > 0 the CP is x D 2=3 and f .2=3/ D 2 gives a D 27=2. The volume in this case is V .27=2; 0/ D .27=60/.78 0/. For a < 0 the CP is x D 1=3 and f .1=3/ D 2 gives a D 27=2. The volume in this case is V . 27=2; 1/ D .27=60/.78 155/ D .27=60/.77/. Thus the minimum volume occurs for f .x/ D .27=2/x.1 x/2 , i.e. b D a D 27=2.

is clearly positive for small x if a > 0. Its two roots are x1 D h and x2 D h2 a=.3ah 6r/. a must be restricted so that x2 is not in the interval .0; h/. If a < 2r= h, then x2 < 0. If 2r= h < a < 3r= h, then x2 > h. If a > 3r= h, then 0 < x2 < h. Hence the interval of acceptable values of a is 0  a  3r= h. We have V .0/ D

13 r 2 h ; 35

V



3r h



D

9 r 2 h : 14

The largest volume corresponds to a D 3r= h, which is the largest allowed value for a and so corresponds to the bluntest possible nose. The corresponding cubic f .x/ is f .x/ D

4.

r .3h2 x h3

3hx 2 C x 3 /:

 a C bx C cx 2 for 0  x  1 a) If f .x/ D , then 2 for 1  x  3  p C qx C rx b C 2cx for 0 < x < 1 . We require that f 0 .x/ D q C 2rx for 1 < x < 3 aD1 aCbCc D2 b C 2c D m

p C 3q C 9r D 0 pCqCr D2 q C 2r D m:

The solutions of these systems are a D 1, b D 2 m, c D m 1, p D 32 .1 m/, q D 2m C 1, and r D 12 .1 C m/. f .x; m/ is f .x/ with these values of the six constants. b) The length of the spline is L.m/ D

Z

1 0

Z p 1 C .b C 2cx/2 dx C

1

3

p

1 C .q C 2rx/2 dx

with the values of b, c, q, and r determined above. A plot of the graph of L.m/ reveals a minimum value in the neighbourhood of m D 0:3. The derivative of L.m/ is a horrible expression, but Mathematica determined its zero to be about m D 0:281326, and the corresponding minimum value of L is about p 4:41748. The polygonal line ABC has length 3 2  4:24264, which is only slightly shorter.

6.

Starting with V1 .r/ D 2r, and using repeatedly the formula Vn .r/ D

x/.x C k/:

The requirement that f .x/  0 for 0  x  1 is satisfied provided either a > 0 and k  0 or a < 0 and k  1. The volume of the wall is V .a; k/ D

Z

0

1

2.15 C x/f .x/ dx D

a .78 C 155k/: 30

r

Vn

p

1.

r2

x 2 / dx;

r

Maple gave the following results: V1 .r/ D 2r 4 V3 .r/ D  r 3 3 8 2 5  r V5 .r/ D 15 16 3 7 V7 .r/ D  r 105 32 4 9  r V9 .r/ D 945

V2 .r/ D  r 2 1 V4 .r/ D  2 r 4 2 1 V6 .r/ D  3 r 6 6 1 4 8 V8 .r/ D  r 24 1 5 10  r V10 .r/ D 120

It appears that 1 n 2n  r ; and nŠ 2n  n 1 r 2n 1 .r/ D 1  3  5    .2n 1/ 22n 1 .n 1/Š n 1 2n 1  r : D .2n 1/Š

V2n .r/ D V2n

5. Let b D ka so that the cross-sectional curve is given by y D f .x/ D ax.1

Z

1

These formulas predict that

V11 .r/ D

211 5Š 5 11  r 11Š

and

V12 .r/ D

1 6 12  r ; 6Š

both of which Maple is happy to confirm.

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CHALLENGING PROBLEMS 7 (PAGE 459)

7.

ADAMS and ESSEX: CALCULUS 9

With y and  as defined in the statement of the problem, we have

8.

y

Q y D f .x/

0  y  10 and

L

0   < :

P .x; y/

x .L; 0/

The needle crosses a line if y < 5 sin  . The probability of this happening is the ratio of the area under the curve to the area of the rectangle in the figure, that is,

Fig. C-7-8 If Q D .0; Y /, then the slope of PQ is y x

Pr D

1 10

Z

 0

5 sin  d D

Y dy D f 0 .x/ D : 0 dx

Since jPQj D L, we have .y Y /2 D L2 px 2 . Since the slope dy=dx is negative at P , dy=dx D L2 x 2 =x. Thus

1 : 

yD

p Z p 2 L C L2 L x2 dx D L ln x x

x2

!

p

L2

Since y D 0 when x D L, we have C D 0 and the equation of the tractrix is LC

y D L ln

p L2 x

x2

!

p

L2

x2 :

Note that the first term can be written in an alternate way: y y D L ln

y D 10



L

p

x L2

x2



p

L2

x2:

y D 5 sin x

 Fig. C-7-7

314

9. 

a) S.a; a; c/ is the area of the surface obtained by rotating the ellipse .x 2 =a2 / C .y 2 =c 2 / D 1p(where a > c) about the y-axis. Since y 0 D cx=.a a2 x 2 /, we

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x 2 CC:

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

CHALLENGING PROBLEMS 7 (PAGE 459)

have S.a; a; c/ D 2  2 D

4 a

Z

Z

0

a

a

x

s

p a4

1C

p

c2x2 a2 .a2

.a2

x2 /

0

b a

S.a; b; c/ 



c c



aC

c c





a a

b c



c, we use

dx

c 2 /x 2

dx a2 x 2 Let x D a sin u dx D a cos u du Z q 4 =2 D a sin u a4 .a2 c 2 /a2 sin2 u du a 0 Z =2 p D 4a sin u a2 .a2 c 2 /.1 cos2 u/ du x



c) Since b D

b a

S.a; a; c/ C



a a

b c



S.a; c; c/:

0

Let v D cos u dv D sin u du Z 1p D 4a c 2 C .a2 c 2 /v 2 dv: 0

d) We cannot evaluate S.3; 2; 1/ even numerically at this stage. The double integral necessary to calculate it is not treated until a later chapter. (The value is approximately 48.882 sq. units.) However, using the formulas obtained above,

This integral can now be handled using tables or computer algebra. It evaluates to aC 2ac 2 ln S.a; a; c/ D 2a C p a2 c 2 2

p

a2 c

c2

!

:

b) S.a; c; c/ is the area of the surface obtained by rotating the ellipse p of part (a) about the y-axis. Since y 0 D cx=.a a2 x 2 /, we have S.a; c; c/ D 2  2

Z

a

y 0

s

1C

c2x2 a2 .a2

x2/

S.3; 3; 1/ C S.3; 1; 1/ S.3; 2; 1/  2  p 1 6 18 D 18 C p ln.3 C 8/ C 2 C p cos 2 8 8  49:595 sq. units.

1

 .1=3/

dx

p Z 4c a p 2 a4 .a2 c 2 /x 2 2 dx a x p 2 a a2 x 2 Z0 a p 4c D 2 a4 .a2 c 2 /x 2 dx a 0 s Z a a2 c 2 2 D 4c 1 x dx a4 0 c 2a2 c cos 1 : D 2c 2 C p 2 2 a a c

D

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315

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SECTION 8.1 (PAGE 472)

ADAMS and ESSEX: CALCULUS 9

CHAPTER 8. CONICS, PARAMETRIC CURVES, AND POLAR CURVES Section 8.1 Conics 1.

8.

If x 2 C 4y 2  x2 C 4 y2

(page 472)

4y D 0, then yC

1 4



D 1;

or

1 2 / 2 1 4

D 1:

  1 This represents an ellipse with centre at 0; , semi2 p   3 1 1 major axis 1, semi-minor axis , and foci at ˙ ; . 2 2 2

The ellipse with foci .0; ˙2/ has major axis along the yaxis and c D 2. If a D 3, then b 2 D 9 4 D 5. The ellipse has equation

y

y2 x2 C D 1: 5 9

x 2 C4y 2 4yD0

1 1 2

2. The ellipse with foci .0; 1/ and .4; 1/ has c D 2, centre .2; 1/, and major axis along y D 1. If  D 1=2, then a D c= D 4 and b 2 D 16 4 D 12. The ellipse has equation .x 2/2 .y 1/2 C D 1: 16 12 3. A parabola with focus .2; 3/ and vertex .2; 4/ has a D and principal axis x D 2. Its equation is .x 2/2 D 4.y 4/ D 16 4y.

1

x

Fig. 8.1-8 1

4. A parabola with focus at .0; 1/ and principal axis along y D 1 will have vertex at a point of the form .v; 1/. Its equation will then be of the form .y C 1/2 D ˙4v.x v/. The origin lies on this curve if 1 D ˙4. v 2 /. Only the sign is possible, and in this case v D ˙1=2. The possible equations for the parabola are .y C 1/2 D 1 ˙ 2x.

9.

If 4x 2 C y 2

4y D 0, then 4x 2 C y 2

4y C 4 D 4

2

2/2 D 4

4x C .y x2 C

2/2

.y

4

D1

This is an ellipse with semi-axes 1 and 2, centred at .0; 2/. y 4

5. The hyperbola with semi-transverse axis a D 1 and foci .0; ˙2/ has transverse axis along the y-axis, c D 2, and b 2 D c 2 a2 D 3. The equation is y2

.y x2 C 1

. 1;2/

4x 2 Cy 2 4yD0

.1;2/

2

x2 D 1: 3 x

6. The hyperbola with foci at .˙5; 1/ and asymptotes x D ˙.y 1/ is rectangular, has centre at .0; 1/ and has transverse axis along the line y D 1. Since c D 5 and a D b (because the asymptotes are perpendicular to each other) we have a2 D b 2 D 25=2. The equation of the hyperbola is 25 x 2 .y 1/2 D : 2

7.

If x 2 C y 2 C 2x D 1, then .x C 1/2 C y 2 D 0. This represents the single point . 1; 0/.

316

Fig. 8.1-9

10. If 4x 2 4x 2

y2

4y D 0, then

.y 2 C 4y C 4/ D

4;

or

x2 1

.y C 2/2 D 4

1:

This represents a hyperbola with centre at .0; 2/, semitransversepaxis 2, semi-conjugate axis 1, and foci at .0; 2 ˙ 5/. The asymptotes are y D ˙2x 2.

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 8.1 (PAGE 472)

 3 This is a hyperbola with centre ; 1 , and asymptotes p 2 the straight lines 2x C 3 D ˙2 2.y 1/.

y

y

x 2 4x 2 y 2 4yD0

3 ;1/ 2

.

1

. 3;1/

x 2 2y 2 C3xC4yD2 x

Fig. 8.1-10 11.

If x 2 C 2x y D 3, then .x C 1/2 y D 4. Thus y D .x C 1/2 4. This is a parabola with vertex . 1; 4/, opening upward. y

Fig. 8.1-13 14.

If 9x 2 C 4y 2

18x C 8y D

9.x 2 x

13, then

2x C 1/ C 4.y 2 C 2y C 1/ D 0

1/2 C 4.y C 1/2 D 0:

,9.x

This represents the single point .1; 1/. x 2 C2x yD3

15.

. 1; 4/

If 9x 2 C 4y 2 9.x 2

Fig. 8.1-11 12. If x C 2y C 2y D 1, then

,

1/2

.x

  3 1 D 2 y2 C y C 4 2   3 1 2 xD 2 yC : 2 2

2x C 1/ C 4.y 2 C 2y C 1/ D 23 C 9 C 4 D 36

1/2 C 4.y C 1/2 D 36

9.x 2

4 x

.y C 1/2 D 1: 9

This is an ellipse with centre .1; 1/, and semi-axes 2 and 3. .1;2/ 1 2 /,

focus at

y

. 1; 1/

.1; 1/

x .3; 1/

9x 2 C4y 2 18xC8yD23

xC2yC2y 2 D1 x



2y 2 C 3x C 4y D 2, then   9 3 2 2.y 1/2 D xC 2 4  3 2 2 xC 2 .y 1/ D1 9 9 8

3 1 ; 2 2



.1; 4/

Fig. 8.1-15 16.

Fig. 8.1-12

4

C

y

This represents a parabola with vertex at . 32 ; ; 12 / and directrix x D 13 . . 11 8 8

13. If x 2

18x C 8y D 23, then

The equation .x y/2 .x C y/2 D 1 simplifies to 4xy D 1 and hence represents a rectangular hyperbola with centre at the origin, asymptotes along the coordinate axes, transverse axis alongy D x, conjugate axis along  1 1 y D x, vertices at 12 ; 12 and ; 2 , semi-transverse 2p and semi-conjugate q axes equal to 1= 2, semi-focal sepa-

ration equal to 12 C 21 D 1, and hence foci at the points     p p1 ; p1 p1 ; p1 . The eccentricity is and 2. 2

2

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2

2

317

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SECTION 8.1 (PAGE 472)

ADAMS and ESSEX: CALCULUS 9

p This is a rectangular hyperbola with centre .0; 2/, p p The semi-axes a D b D 2, and eccentricity 2. p semi-focal separation is 2; the 2/. The p foci are at .˙2; asymptotes are u D ˙.v C 2/. In terms of thep original coordinates, the centre is .1; 1/, p the foci are .˙ 2 C 1; ˙ 2 1/, and the asymptotes are x D 1 and y D 1.

y

x



1 1 2;2



y

.x y/2 .xCy/2 D1

xyCx yD2

Fig. 8.1-16 .1; 1/

17.

x

The parabola has focus at .3; 4/ and principal axis along y D 4. The vertex must be at a point of the form .v; 4/, in which case a D ˙.3 v/ and the equation of the parabola must be of the form .y

4/2 D ˙4.3

v/.x

v/:

Fig. 8.1-19

This curve passes through the origin if 16 D ˙4.v 2 3v/. We have two possible equations for v: v 2 3v 4 D 0 and v 2 3v C 4 D 0. The first of these has solutions v D 1 or v D 4. The second has no real solutions. The two possible equations for the parabola are 4/2 D 4.4/.x C 1/

.y .y

2

4/ D 4. 1/.x

4/

or

y2

or

2

y

8y D 16x 8y D

4x

18. The foci of the ellipse are .0; 0/ and .3; 0/, so the centre is .3=2; 0/ and c D 3=2. The semi-axes a and b must satisfy a2 b 2 D 9=4. Thus the possible equations of the ellipse are y2 .x .3=2//2 C 2 D 1: 2 .9=4/ C b b 19. For xy C x y D 2 we have A D C D 0, B D 1. We therefore rotate the coordinate axes (see text pages 407– 408) through angle  D =4. (Thus cot 2 D 0 D .A C /=B.) The transformation is 1 x D p .u 2

v/;

20.

We have x 2 C 2xy C y 2 D 4x 4y C 4 and A D 1, B D 2, C D 1, D D 4, E D 4 and F D 4. We rotate the axes through angle  satisfying  tan 2 D B=.A C / D 1 )  D . Then A0 D 2, 4 p B 0 D 0, C 0 D 0, D 0 D 0, E 0 D 4 2 and the transformed equation is p 2u2 C 4 2v

4D0

)

u2 D

 p 2 2 v

1 p 2

which represents a parabola with vertex at  .u; v/ D 0; p1 and principal axis along u D 0. 2 The distance p a from thepfocus to the vertex is given by 4a D 2 2, so apD 1= 2 and the focus is at .0; 0/. The directrix is v D 2. 1 1 Since x D p .u v/ and y D p .u C v/, the ver2 2 tex of the parabola in terms of xy-coordinates is . 12 ; 12 /, and the focus is .0; 0/. The directrix is x y D 2. The principal axis is y D x. y

yD x

1 y D p .u C v/: 2

x 2 C2xyCy 2 D4x 4yC4 . 1=2;1=2/

The given equation becomes x

1 2 .u 2 u2 u2 u2 2

318

1 v 2 / C p .u v/ 2 p v 2 2 2v D 4  p 2 vC 2 D2 p .v C 2/2 D 1: 2



1 p .u C v/ D 2 2

Fig. 8.1-20

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21.

SECTION 8.1 (PAGE 472)

For 8x 2 C 12xy C 17y 2 D 20, we have A D 8, B D 12, C D 17, F D 20. Rotate the axes through angle  where tan 2 D

B A

C

Thus cos 2 D 3=5, sin 2 D 2 cos2 

1 D cos 2 D

D

12 D 9

Then A0 D 0, B 0 D 0, C 0 D 5, D 0 D transformed equation is

4 : 3

5v 2 C

4=5, and 3 5

cos2  D

)

4 : 5

p

5u D 0

)

p

5, E 0 D 0 and the 1 p u 5

v2 D

which represents a parabola with vertex at .u; v/ D .0; 0/,   1 1 p ; 0 . The directrix is u D p and the focus at 4 5 4 5 2 1 principal axis is v D 0. Since x D p u p v and 5 5 1 2 y D p u C p v, in terms of the xy-coordinates, the ver5 5   1 1 ; . The directrix is tex is at .0; 0/, the focus at 10 20 2x C y D 14 and the principal axis is 2y x D 0.

2 1 We may therefore take cos  D p , and sin  D p . 5 5 The transformation is therefore 1 2 1 2 uD p x p y x D p uC p v 5 5 5 5 1 2 1 2 y D p uC p v vD p xCp y 5 5 5 5 The coefficients of the transformed equation are       4 2 1 A0 D 8 C 12 C 17 D5 5 5 5 B0 D 0       4 2 1 0 12 C 17 D 20: C D8 5 5 5

y

x x 2 4xyC4y 2 C2xCyD0

The transformed equation is

xD2y 2

5u2 C 20v 2 D 20;

or

u C v 2 D 1: 4

This is an ellipse with centre p .0; 0/, semi-axes a D 2 and b D 1, and foci at u D ˙ 3, v D 0. In terms of the original coordinates, the centre is .0; 0/, p p ! 2 3 3 the foci are ˙ p ; p . 5 5

Fig. 8.1-22

y

23. 8x 2 C12xyC17y 2 D20

p The distance from P to F is x 2 C y 2 . The distance from P to D is x C p. Thus p x2 C y2 D xCp x 2 C y 2 D  2 .x 2 C 2px C p 2 /

x

.1

 2 /x 2 C y 2

Fig. 8.1-21

2p 2 x D  2 p 2 :

y

22. We have x 2 4xy C4y 2 C2x Cy D 0 and A D 1, B D 4, C D 4, D D 2, E D 1 and F D 0. We rotate the axes through angle  satisfying tan 2 D B=.A C / D 43 . Then p 5 3 ) cos 2 D sec 2 D 1 C tan2 2 D 3 5 r r 8 1 C cos 2 4 2 ˆ ˆ D D p I < cos  D 2 5 r r 5 ) ˆ 1 cos 2 1 1 ˆ : sin  D D D p : 2 5 5

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P D.x;y/

xD p D F

x

Fig. 8.1-23

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SECTION 8.1 (PAGE 472)

24.

ADAMS and ESSEX: CALCULUS 9

y

Let the equation of the parabola be y 2 D 4ax. The focus F is at .a; 0/ and vertex at .0; 0/. Then the distance from the vertex p to the focus is a. At x D a, y D 4a.a/ D ˙2a. Hence, ` D 2a, which is twice the distance from the vertex to the focus.

` x

a c x2

y

a2

y2 D1 b2

y 2 D4ax `

Fig. 8.1-26 x

.a;0/

27.

S2

Fig. 8.1-24

C2

`2 c2 25. We have 2 C 2 D 1. Thus a b  2 2 ` Db 1  D b2 1

B F2

2

c a2 a2

but c 2 D a2  b2 b2 D b2 2 : 2 a a

b2

P F1

S1

C1

Therefore ` D b 2 =a.

y b

A

x2 y2 C D1 a2 b 2

` c

a x

V

Fig. 8.1-27 Let the spheres S1 and S2 intersect the cone in the circles C1 and C2 , and be tangent to the plane of the ellipse at the points F1 and F2 , as shown in the figure. Let P be any point on the ellipse, and let the straight line through P and the vertex of the cone meet C1 and C2 at A and B respectively. Then PF1 D PA, since both segments are tangents to the sphere S1 from P . Similarly, PF2 D PB. Thus PF1 C PF2 D PA C PB D AB D constant (distance from C1 to C2 along all generators of the cone is the same.) Thus F1 and F2 are the foci of the ellipse.

Fig. 8.1-25

y2 x2 D 1. The 2 a b2 vertices p are at .˙a; 0/ and p the foci are at .˙c; 0/ where c D a2 C b 2 . At x D a2 C b 2 ,

26. Suppose the hyperbola has equation

a2 C b 2 y 2 D1 a2 b2 .a2 C b 2 /b 2 a2 y 2 D a2 b 2 yD˙ Hence, ` D

320

b2 . a

b2 : a

28.

Let F1 and F2 be the points where the plane is tangent to the spheres. Let P be an arbitrary point P on the hyperbola in which the plane intersects the cone. The spheres are tangent to the cone along two circles as shown in the figure. Let PAVB be a generator of the cone (a straight line lying on the cone) intersecting these two circles at A and B as shown. (V is the vertex of the cone.) We have PF1 D PA because two tangents to a sphere from

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SECTION 8.2 (PAGE 478)

a point outside the sphere have equal lengths. Similarly, PF2 D PB. Therefore PF2

PF1 D PB

PA D AB D constant, F P

Y

since the distance between the two circles in which the spheres intersect the cone, measured along the generators of the cone, is the same for all generators. Hence, F1 and F2 are the foci of the hyperbola.

C V

X Q

P F1 A

A

Fig. 8.1-29

V B

Section 8.2 Parametric Curves 1.

F2

(page 478)

If x D t , y D 1 t , .0  t  1/ then x C y D 1. This is a straight line segment. y

Fig. 8.1-28 1

xDt yD1 t .0t1/ x

1

Fig. 8.2-1 2. 29. Let the plane in which the sphere is tangent to the cone meet AV at X. Let the plane through F perpendicular to the axis of the cone meet AV at Y . Then VF D V X, and, if C is the centre of the sphere, F C D XC . Therefore V C is perpendicular to the axis of the cone. Hence YF is parallel to V C , and we have Y V D V X D VF . If P is on the parabola, FP ? VF , and the line from P to the vertex A of the cone meets the circle of tangency of the sphere and the cone at Q, then

If x D 2 t and y D t C 1 for 0  t < 1, then y D 2 x C 1 D 3 x for 1 < x  2, which is a half line. y

xD2 t yDtC1

.2;1/

FP D PQ D YX D 2V X D 2VF:

x

Fig. 8.2-2 Since FP D 2VF , FP is the semi-latus rectum of the parabola. (See Exercise 18.) Therefore F is the focus of the parabola.

3.

1 If x D 1=t , y D t 1, .0 < t < 4/, then y D x is part of a hyperbola.

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1. This

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ADAMS and ESSEX: CALCULUS 9

y

y





1 ;3 4 tD4

bxDay

1 yD x

1

tD0 a

x

tD1 x yD 1

bxD ay

Fig. 8.2-3 4. If x D

Fig. 8.2-6

1 t and y D for 1 C t2 1 C t2

1 < t < 1, then

1 1 C t2 D Dx 2 2 .1 C t / 1 C t2 2 1 1 C y2 D : 2 4

7.

x2 C y2 D

 , x

If x D 3 sin  t , y D 4 cos  t , . 1  t  1/, then y2 x2 C D 1. This is an ellipse. 9 16 y tD0

x2 y2 9 C 16 D1

This curve consists of all points of the circle with centre at . 21 ; 0/ and radius 12 except the origin .0; 0/. y

x

tD1

tD 1 tD1

tD0

tD 1

x

Fig. 8.2-7

xD1=.1Ct 2 / yDt=.1Ct 2 /

8.

Fig. 8.2-4 5. If x D 3 sin 2t , y D 3 cos 2t , .0  t  =3/, then x 2 C y 2 D 9. This is part of a circle. y tD0

If x D cos sin s and y D sin sin s for 1 < s < 1, then x 2 C y 2 D 1. The curve consists of the arc of this circle extending from .a; b/ through .1; 0/ to .a; b/ where a D cos.1/ and b D sin.1/, traversed infinitely often back and forth. y xDcos sin s yDsin sin s

x 2 Cy 2 D9 x tD

1 rad

 3

x

Fig. 8.2-5 6. If x D a sec t and y D b tan t for x2 a2

y2 D sec2 t b2

  < t < , then 2 2

Fig. 8.2-8

tan2 t D 1: 9.

The curve is one arch of this hyperbola.

322

If x D cos3 t , y D sin3 t , .0  t  2/, then x 2=3 C y 2=3 D 1. This is an astroid.

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y

SECTION 8.2 (PAGE 478)

and

tD=2

1 D .cos2 t Csin2 t /2 D cos4 t Csin4 t C2 cos2 t sin2 t:

x 2=3 Cy 2=3 D1

Hence,

tD0

tD

tD2

(b) If x D sec4 t and y D tan4 t , then

tD3=2

y/2 D .sec4 t

.x

Fig. 8.2-9 10. If x D 1

p

4

.x

t2 D 4

D sec4 t C tan4 t C 2 sec2 t tan2 t

2  t  2 then

.y

and

2/2 :

1 D .sec2 t tan2 t /2 D sec4 t Ctan4 t 2 sec2 t tan2 t:

The parametric curve is the left half of the circle of radius 4 centred at .1; 2/, and is traced in the direction of increasing y. p

t2

Hence, y/2 D 2.sec4 t C tan4 t / D 2.x C y/:

1 C .x

y

4 yD2Ct 2t2

xD1

tan4 t /2

D .sec2 t C tan2 t /2

t 2 and y D 2 C t for 1/2 D 4

y/2 D 2.cos4 t C sin4 t / D 2.x C y/:

1 C .x

(c) Similarly, if x D tan4 t and y D sec4 t , then 1 C .x

.1;2/

y/2 D 1 C .y

x/2

2

tan2 t /2 C .sec4 t

D .sec t

tan4 t /2

D 2.tan4 t C sec4 t / D 2.x C y/:

These three parametric curves above correspond to different parts of the parabola 1C.x y/2 D 2.x Cy/, as shown in the following diagram.

x

Fig. 8.2-10 11.

y

x D cosh t , y D sinh t represents the right half (branch) of the rectangular hyperbola x 2 y 2 D 1.

xDtan4 t yDsec4 t

The parabola

12. x D 2 3 cosh t , y D 1 C 2 sinh t represents the left half (branch) of the hyperbola 2/2

.x 9

2.xCy/D1C.x y/2

1 xDcos4 t yDsin4 t

.y C 1/2 D 1: 4

xDsec4 t yDtan4 t

1

x

Fig. 8.2-14 13. x D t cos t , y D t sin t , .0  t  4/ represents two revolutions of a spiral curve winding outwards from the origin in a counterclockwise direction. The point on the curve corresponding to parameter value t is t units distant from the origin in a direction making angle t with the positive x-axis. 14.

(a) If x D cos4 t and y D sin4 t , then .x

y/2 D .cos4 t sin4 t /2 h D .cos2 t C sin2 t /.cos2 t D .cos2 t

sin2 t /2

D cos4 t C sin4 t

15.

16.

The slope of y D x 2 at x is m D 2x. Hence the parabola can be parametrized x D m=2, y D m2 =4, . 1 < m < 1/.

If .x; y/ is any point on the circle x 2 C y 2 D R2 other than .R; 0/, then the line from .x; y/ to .R; 0/ has slope y . Thus y D m.x R/, and mD x R x 2 C m2 .x

i2 sin t / 2

2 cos2 t sin2 t

.m2 C 1/x 2 h .m2 C 1/x 2

) xD

R/2 D R2

2xRm2 C .m2 i .m2 1/R .x

1/R2 D 0 R/ D 0

.m 1/R or x D R: m2 C 1

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ADAMS and ESSEX: CALCULUS 9

y

The parametrization of the circle in terms of m is given by

Y

.m2 1/R xD m2 C 1 " .m2 1/R yDm m2 C 1

b

#

2Rm m2 C 1

R D

P D .x; y/

T

a t

X x

where 1 < m < 1. This parametrization gives every point on the circle except .R; 0/. y .x;y/

slope m x .R;0/

Fig. 8.2-18

x 2 Cy 2 DR2

19.

Fig. 8.2-16

If x D

3t 3t 2 , y D , .t ¤ 1 C t3 1 C t3

x3 C y3 D

17. y P D .x; y/

t

27t 3 27t 3 .1 C t 3 / D D 3xy: 3 3 .1 C t / .1 C t 3 /2

As t ! 1, we see that jxj ! 1 and jyj ! 1, but

T a

1/, then

xCy D

X x

Thus x C y D

3t .1 C t / D 1 C t3 1

3t ! 1: t C t2

1 is an asymptote of the curve. y

tD1

Fig. 8.2-17 t!1

Using triangles in the figure, we see that the coordinates of P satisfy x D a sec t;

tD0

y D a sin t:

x

folium of Descartes

The Cartesian equation of the curve is

t! 1

y2 a2 C D 1: a2 x2 The curve has two branches extending to infinity to the left and right of the circle as shown in the figure.

Fig. 8.2-19 20.

18. The coordinates of P satisfy x D a sec t; The Cartesian equation is

324

y D b sin t:

Let C0 and P0 be the original positions of the centre of the wheel and a point at the bottom of the flange whose path is to be traced. The wheel is also shown in a subsequent position in which it makes contact with the rail at R. Since the wheel has been rotated by an angle  ,

a2 y2 C 2 D 1. 2 b x

OR D arc SR D a:

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SECTION 8.2 (PAGE 478)

y

Thus, the new position of the centre is C D .a; a/. Let P D .x; y/ be the new position of the point; then

Tt

x D OR PQ D a b sin. y D RC C CQ D a C b cos.

 / D a b sin ;  / D a b cos :

These are the parametric equations of the prolate cycloid. y

P

Q

P t D.x;y/

b 

t

b

S

C0

t

Ct

t

A a

C

x

a O x

R P0

Fig. 8.2-21 Fig. 8.2-20

If a D 2 and b D 1, then x D 2 cos t , y D 0. This is a straight line segment. If a D 4 and b D 1, then

y

x D 3 cos t C cos 3t D 3 cos t C .cos 2t cos t sin 2t sin t /   D 3 cos t C .2 cos2 t 1/ cos t 2 sin2 t cos t

xDa b sin  yDa b cos  x 2a

D 2 cos t C 2 cos3 t 2 cos t .1 sin2 t / D 4 cos3 t y D 3 sin t C sin 3t D 3 sin t sin 2t cos t .cos 2t sin t /   D 3 sin t 2 sin t cos2 t .1 2 sin2 t / sin t

Fig. 8.2-20

D 2 sin t

2 sin t C 2 sin3 t C 2 sin3 t D 4 sin3 t

This is an astroid, similar to that of Exercise 11. 22. 21.

Let t and  t be the angles shown in the figure below. Then arc AT t D arc T t P t , that is, at D b t . The centre C t of the rolling circle is C t D .a b/ cos t; .a b/ sin t . Thus x y

Since  t

tD

.a .a a t b

x D .a y D .a

a)

From triangles in the figure, x D jTXj D jOT j tan t D tan t  y D jOY j D si n 2 t D jOY j cos t D jOT j cos t cos t D cos2 t: y

tD

a

b b

yD1

T

b/ cos t D b cos. t t / b/ sin t D b sin. t t /: t , therefore

Y

1 2

  .a b/t b/ cos t C b cos b   .a b/t b/ sin t b sin : b

X

P D .x; y/

t

O

x

Fig. 8.2-22

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b)

ADAMS and ESSEX: CALCULUS 9

y

1 1 . D sec2 t D 1Ctan2 t D 1Cx 2 . Thus y D y 1 C x2

23. x D sin t;

y D sin.2t /

y x x

Fig. 8.2-23 28. 24.

x D sin t;

y D sin.3t /

y

x

tangent to x 2 C y 2 D 1. If n  2 is an integer, the curve closes after one revolution and has n cusps. The figure shows the curve for n D 7. If n is a rational number but not an integer, the curve will wind around the circle more than once before it closes. y

Fig. 8.2-24 25. x D sin.2t /;

y D sin.3t /

Fig. 8.2-27   1 1 cos t C cos..n 1/t / x D 1C n n   1 1 y D 1C sin..n 1/t / sin t n n represents a cycloid-like curve that is wound around the  2 inside circle x 2 C y 2 D 1 C .2=n/ and is externally

y

x

x

Fig. 8.2-25 26. x D sin.2t /;

y D sin.5t /

Fig. 8.2-28 y

Section 8.3 Smooth Parametric Curves and Their Slopes (page 483) x

27.

Fig. 8.2-26   1 1 x D 1C cos.nt / cos t n n   1 1 y D 1C sin.nt / sin t n n represents a cycloid-like curve that is wound around the circle x 2 C y 2 D 1 instead of extending along the x-axis. If n  2 is an integer, the curve closes after one revolution and has n 1 cusps. The left figure below shows the curve for n D 7. If n is a rational number, the curve will wind around the circle more than once before it closes.

326

1.

y D 2t 4 x D t2 C 1 dy dx D 2t D2 dt dt No horizontal tangents. Vertical tangent at t D 0, i.e., at .1; 4/.

2.

y D t 2 C 2t x D t 2 2t dy dx D 2t 2 D 2t C 2 dt dt Horizontal tangent at t D 1, i.e., at .3; 1/. Vertical tangent at t D 1, i.e., at . 1; 3/.

3.

x D t 2 2t y D t 3 12t dx dy D 2.t 1/ D 3.t 2 4/ dt dt Horizontal tangent at t D ˙2, i.e., at .0; 16/ and .8; 16/. Vertical tangent at t D 1, i.e., at . 1; 11/.

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4.

5.

6.

7.

SECTION 8.3 (PAGE 483)

y D 2t 3 C 3t 2 x D t 3 3t dy dx D 3.t 2 1/ D 6t .t C 1/ dt dt Horizontal tangent at t D 0, i.e., at .0; 0/. Vertical tangent at t D 1, i.e., at . 2; 5/. At t D 1 (i.e., at .2; 1/) both dx=dt and dy=dt change sign, so the curve is not smooth there. (It has a cusp.) 2

x D sin.2t / dx D 2 cos.2t / dt Horizontal tangent Vertical tangent at p .˙1; 1= 2/.

D sin t

1

13.

/.

D t sin t

14.

at t D n, i.e., at .0; . 1/n n/ (for

t D .n C

1 2 /,

i.e. at .1; 1/ and

y D sin t dy D cos t dt at t D .n C 21 /, i.e., at .0; ˙1/. p t D 12 .n C 21 /, i.e., at .˙1; 1= 2/ and

3t 3t 8. xD yD 1 C t3 1 C t3 dx dy 3.1 2t 3 / 3t .2 t 3 / D D 3 2 dt .1 C t / dt .1 C t 3 /2 Horizontal tangent at t D 0 and t D 21=3 , i.e., at .0; 0/ and .21=3 ; 22=3 /. Vertical tangent at t D 2 1=3 , i.e., at .22=3 ; 21=3 /. The curve also approaches .0; 0/ vertically as t ! ˙1.

11.

1/ D t

2;

y D 2 C 4.t

1/ D 4t

2:

x D t4 t2 y D t 3 C 2t dy dx D 4t 3 2t D 3t 2 C 2 dt dt dy 3. 1/2 C 2 At t D 1; D D dx 4. 1/3 2. 1/ y D sin t dy D cos t dt cos.=6/ D 2 sin.=3/

 4

1 p 2 1 dx D 1 C sin t D 1 C p dt 2  1 at t D y D 1 sin t D 1 p 4 2  1 dy at t D D cos t D p dt 2 4  1 1  p C 1 C p t, Tangent line: x D 4 2 2 1 t yD1 p p . 2 2 xDt

x D t3

cos t D

t , y D t 2 is at .0; 1/ at t D

1 and t D 1. Since

2t ˙2 dy D 2 D D ˙1; dx 3t 1 2 the tangents at .0; 1/ at t D ˙1 have slopes ˙1. 16.

x D sin t , y D sin.2t / is at .0; 0/ at t D 0 and t D . Since  dy 2 cos.2t / 2 if t D 0 D D 2 if t D , dx cos t the tangents at .0; 0/ at t D 0 and t D  have slopes 2 and 2, respectively.

y D 1 t3 x D t3 C t dy dx D 3t 2 C 1 D 3t 2 dt dt 3.1/2 3 dy D D : At t D 1; dx 3.1/2 C 1 4

x D cos.2t / dx D 2 sin.2t / dt  dy At t D ; D 6 dx

1 C .t

t cos t

15.

10.

3 : 2

y D t C t 3 D 2 at t D 1 x D t 3 2t D 1 dy dx D 3t 2 2 D 1 D 1 C 3t 2 D 4 at t D 1 dt dt Tangent line: x D 1 C t , y D 2 C 4t . This line is at . 1; 2/ at t D 0. If you want to be at that point at t D 1 instead, use xD

2

9.

y D t e 2t dy D e 2t .1 C 2t / dt dy e 4 .1 4/ 2; D D dx 2e 4

x D e 2t dx D 2e 2t dt At t D

2

x D t e t =2 yDe t dx dy 2 2 D .1 t 2 /e t =2 D 2t e t dt dt Horizontal tangent at t D 0, i.e., at .0; 1/. Vertical tangent at t D ˙1, i.e. at .˙e 1=2 ; e y x D sin t dy dx D cos t dt dt Horizontal tangent integers n). Vertical tangent at . 1; 1/.

12.

1 : 2

5 : 2

17.

y D t2 x D t3 dy dx D 3t 2 D 2t both vanish at t D 0. dt dt dy 2 dx 3t D has no limit as t ! 0. D ! 0 as t ! 0, dx 3t dy 2 but dy=dt changes sign at t D 0. Thus the curve is not smooth at t D 0. (In this solution, and in the next five, we are using the Remark following Example 2 in the text.)

18.

x D .t 1/4 y D .t 1/3 dx dy D 4.t 1/3 D 3.t 1/2 both vanish at t D 1. dt dt dx 4.t 1/ Since D ! 0 as t ! 1, and dy=dt does not dy 3 change sign at t D 1, the curve is smooth at t D 1 and therefore everywhere.

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SECTION 8.3 (PAGE 483)

19.

20.

21.

ADAMS and ESSEX: CALCULUS 9

y D t3 x D t sin t dy dx D sin t C t cos t D 3t 2 both vanish at t D 0. dt dt dy 3t 2 6t lim D lim D lim D 0, t!0 dx t!0 sin t C t cos t t!0 2 cos t t sin t but dx=dt changes sign at t D 0. dx=dy has no limit at t D 0. Thus the curve is not smooth at t D 0.

22.

2t and y D t 2

Both f 0 .t / and g 0 .t / vanish at t D 0. Observe that 6t 2 dy D 2 D : dx 3t t Thus, lim

t!0C

dy D 1; dx

! # &

xDt 3 yD3t 2 1 x 1

Fig. 8.3-22 2 j

C C ! " %

!t

The tangent is horizontal at t D 2, (i.e., .0; 4/), and is vertical at t D 1 (i.e., at . 1; 3/. Observe that d 2 y=dx 2 > 0, and the curve is concave up, if t > 1. Similarly, d 2 y=dx 2 < 0 and the curve is concave down if t < 1. y

3

x D t 3t , y D 2=.1 C t 2 /. Observe that y ! 0, x ! ˙1 as t ! ˙1. dx dy 4t D 3.t 2 1/; D dt dt .1 C t 2 /2 dy 4t D dx 3.t 2 1/.1 C t 2 /2 d 2x d 2y 4.3t 2 1/ D 6t; D dt 2 dt 2 .1 C t 2 /3 2 4.3t 1/ 4t .6t / 3.t 2 1/ 2 3 d 2y .1 C t / .1 C t 2 /2 D 2 2 3 dx Œ3.t 1/ 60t 4 C 48t 2 C 12 D 27.t 2 1/3 .1 C t 2 /3 Directional information:

xDt 2 2t yDt 2 4t

x

tD1 tD2

Fig. 8.3-21

328

2 0, then lim y D lim

!0C

!0C

37. r D C C cos  sin.3 / For C < 1 there appear to be 6 petals of 3 different sizes. For C  1 there are only 4 of 2 sizes, and these coalesce as C increases.

sin  D 1: 

Thus y D 1 is a horizontal asymptote.

38.

y

y

yD1 rD1=

r D ln. /

x

x Fig. 8.5-29 30. The graph of r D cos n has 2n leaves if n is an even integer and n leaves if n is an odd integer. The situation for r 2 D cos n is reversed. The graph has 2n leaves if n is an odd integer (provided negative values of r are allowed), and it has n leaves if n is even.

Fig. 8.5-38 We will have Œln 1 ; 1  D Œln 2 ; 2  if

31. If r D f . /, then

2 D 1 C 

x D r cos  D f . / cos  y D r sin  D f . / sin : 32. r D cos  cos.m / For odd m this flower has 2m petals, 2 large ones and 4 each of .m 1/=2 smaller sizes. For even m the flower has m C 1 petals, one large and 2 each of m=2 smaller sizes.

and

ln 1 D

that is, if ln 1 C ln.1 C / D 0. This equation has solution 1  0:29129956. The corresponding intersection point has Cartesian coordinates .ln 1 cos 1 ; ln 1 sin 1 /  . 1:181442; 0:354230/. 39. y

33. r D 1 C cos  cos.m / These are similar to the ones in Exercise 32, but the curve does not approach the origin except for  D  in the case of even m. The petals are joined, and less distinct. The smaller ones cannot be distinguished.

r D 1= x

34. r D sin.2 / sin.m / For odd m there are m C 1 petals, 2 each of .m C 1/=2 different sizes. For even m there are always 2m petals. They are of n different sizes if m D 4n 2 or m D 4n. 35. r D 1 C sin.2 / sin.m / These are similar to the ones in Exercise 34, but the petals are joined, and less distinct. The smaller ones cannot be distinguished. There appear to be m C 2 petals in both the even and odd cases. 36. r D C C cos  cos.2 / The curve always has 3 bulges, one larger than the other two. For C D 0 these are 3 distinct petals. For 0 < C < 1 there is a fourth supplementary petal inside the large one. For C D 1 the curve has a cusp at the origin. For C > 1 the curve does not approach the origin, and the petals become less distinct as C increases.

ln 2 ;

r D ln. / Fig. 8.5-39 The two intersections of r D ln  and r D 1= for 0 <   2 correspond to solutions 1 and 2 of ln 1 D

1 ; 1

ln 2 D

1 : 2 C 

The first equation has solution 1  1:7632228, giving the point . 0:108461; 0:556676/, and the second equation has solution 2  0:7746477, giving the point . 0:182488; 0:178606/.

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SECTION 8.6 (PAGE 497)

ADAMS and ESSEX: CALCULUS 9

y

Section 8.6 Slopes, Areas, and Arc Lengths for Polar Curves (page 497)

1.

Area D

1 2

Z

2

 d D

0

D

 3

A

.2/2 D  2: 4

x

y rDsin 3 p rD 

Fig. 8.6-4 D0

D2x

5. Fig. 8.6-1

Z 1 =8 cos2 4 d Total area D 16  2 0 Z =8 D4 .1 C cos 8 / d 0

ˇ=8  sin 8 ˇˇ  sq. units. D4 C D ˇ ˇ 8 2

ˇ2 Z 1 2 2  3 ˇˇ 4 2. Area D  d D ˇ D  3 sq. units. 2 0 6 ˇ 3

0

0 y

y

rDcos 4

=8

x

x A

rD

Fig. 8.6-5

Fig. 8.6-2

3. Area D 4  D 2a

1 2

Z

=4 0

2 sin 2

2

a2 cos 2 d

6.

ˇ=4 ˇ ˇ D a2 sq. units. ˇ ˇ

The circles r D a and r D 2a cos  intersect at  D ˙=3. By symmetry, the common area is 4  .area of sector area of right triangle/ (see the figure), i.e.,

0

y

r 2 Da2 cos 2

4

"

1 2 a 6





1a 22

x

p

3a 2

#

D

4

p 3 3 2 a sq. units. 6

y rD2a cos 

rDa

Fig. 8.6-3 A

4.

1 Area D 2

Z

=3 0

 1  D 4

338

Z

=3

1 sin2 3 d D .1 cos 6 / d 4 0 ˇ ˇ=3  1 ˇ D sin 6 ˇ sq. units. ˇ 6 12 0

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Fig. 8.6-6

x

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INSTRUCTOR’S SOLUTIONS MANUAL

7.

SECTION 8.6 (PAGE 497)

Z  1  .1 cos  /2 d Area D 2  2 =2 2  Z   1 C cos 2 D d 1 2 cos  C 2 =2 ˇ   3  sin 2 ˇˇ D  2 sin  ˇ ˇ 2 2 4

=2

D

and  D ˙=3. The shaded area is given by  2  2

1 2 2

"Z D



.1 C cos  / d

=3 Z 

y

3 D 2

rD1



=3

 C 2 sq. units. 4

rD1 cos 

2



x

 4

D

9 2

9

1 C 2 cos  C

Z

Z

=2

2

cos  d =3

1 C cos 2 2

=2

=3

.1 C cos 2 / d







#

d

ˇ sin 2 ˇˇ C 2 sin  C ˇ ˇ 4 =3 ˇ  ˇ=2 sin 2 ˇ 9 C ˇ ˇ 2 2 =3 p p ! p 3 3 9  3 C sq. units. D 8 4 2 4

2 3

y

Fig. 8.6-7

=3 rD3 cos 

rD1Ccos 

x

8.

Z 1 2 1 =2 2 a C 2  a .1 sin  /2 d 2 2 0  Z =2  a2 1 cos 2 D C a2 d 1 2 sin  C 2 2 0 ˇˇ=2  1 a2 ˇ 2 3 Ca  C 2 cos  sin 2 ˇ D ˇ 2 2 4 0   5 2 2 a sq. units. D 4

Area D

Fig. 8.6-9 5  and ˙ , 6 6 the area inside the lemniscate and outside the circle is

10. Since r 2 D 2 cos 2 meets r D 1 at  D ˙

y

4

rDa

x

A

1 2

Z

=6 h

2 cos 2

0

ˇ=6 ˇ ˇ D 2 sin 2 ˇˇ ˇ

i 12 d

p  D 3 3

 sq. units. 3

0

y

rDa.1 sin / rD1

Fig. 8.6-8 A

A x r 2 D2 cos 2

9. For intersections: 1 C cos  D 3 cos  . Thus 2 cos  D 1

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Fig. 8.6-10

339

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SECTION 8.6 (PAGE 497)

11.

ADAMS and ESSEX: CALCULUS 9

r D 0 at  D ˙2=3. The shaded area is 1 2 2

Z



14.

Z

2 0

Da

2

.1 C 2 cos  / d

2=3 Z 

  1 C 4 cos  C 2.1 C cos 2 / d 2=3 ˇ ˇ ˇ ˇ   ˇ ˇ D3 C 4 sin  ˇ C sin 2 ˇ ˇ ˇ 3 2=3 2=3 p p p 3 3 3 D sq. units. D 2 3C 2 2 D

Da

rD1C2 cos 

15. 1

Z

Z

p a2 C a2  2 d

2 0

p 1 C  2 d

D2

Let  D tan u d D sec2 u d

sec3 u du

D0

ˇ ˇD2 a ˇ sec u tan u C ln j sec u C tan uj ˇ D ˇ 2 D0 ˇD2 ˇ i h p p a ˇ D  1 C  2 C ln j 1 C  2 C  j ˇ ˇ 2 D0 i p ah p 2 D 2 1 C 4 C ln.2 C 1 C 4 2 / units: 2

y 2=3

sD

3 x

r 2 D cos 2 dr D 2 sin 2 2r d s

dr D d

)

sin 2 r

p sin2 2 d D sec 2 d cos 2 Z =4 p sec 2 d: Length D 4

ds D 2=3

cos 2 C 0

y

Fig. 8.6-11

r 2 Dcos 2 x

12.

sD

Z



0

Z



s 

dr d

2

C r 2 d D

p 4 C  2 d

Z

 0

p

4 2 C  4 d

Let u D 4 C  2 0 du D 2 d ˇ4C 2 Z 4C 2 p 1 1 3=2 ˇˇ D u du D u ˇ ˇ 2 4 3 4 h i 1 2 3=2 D .4 C  / 8 units: 3 D



Fig. 8.6-15 16.

If r 2 D cos 2 , then 2r

dr D d

and ds D

dr D ae a . 13. r D e , .     /. dp p ds D e 2a C a2 e 2a d D 1 C a2 e a d . The length of the curve is a

Z

340

 

p 1 C a2 e a d D

p

1C a

a2

.e

a

e

a

2 sin 2 )

s

cos 2 C

dr D d

sin 2 p cos 2

d sin2 2 : d D p cos 2 cos 2

a) Area of the surface generated by rotation about the xaxis is Sx D 2

/ units.

D 2 D

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Z

=4

r sin  ds

0

Z

0

=4 p

cos 2 sin  p

ˇ=4 ˇ ˇ D .2 2 cos  ˇ ˇ 0

p

d cos 2

2/ sq. units:

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 8.6 (PAGE 497)

y

b) Area of the surface generated by rotation about the yaxis is Z =4 Sy D 2 r cos  ds D 4

Z

=4 =4 p

cos 2 cos  p

d

cos 2 ˇ=4 ˇ p ˇ D 2 2 sq. units. D 4 sin  ˇ ˇ 0

x

0

17.

For r D 1 C sin  ,

Fig. 8.6-18 19.

r 1 C sin  D : dr=d cos  p If  D =4, then tan D 2 Cp1 and D 3=8. 2 and D =8. If  D 5=4, then tan D 1 The line y D x meets the cardioid r D 1 C sin  at the origin at an angle of 45ı , and also at first and third quadrant points at angles of 67:5ı and 22:5ı as shown in the figure. tan

rD2 cos 

r 2 D2 sin 2

D

y

The curves r D 1 cos  and r D 1 sin  intersect on the rays  D =4 and  D 5=4, as well as at the origin. At the origin their cusps clearly intersect at right angles. For r D 1 cos  , tan p1 D .1 cos  /= sin  . At  D =4, tan 1 D 2 p 1, so 1 D =8. At  D 5=4, tan 1 D . 2 C 1/, so 1 D 3=8. For r D 1 sin  , tan 2 Dp.1 sin  /=. cos  /. At  D =4, tan 2 D 1p 2, so 2 D =8. At  D 5=4, tan 2 D 2 C 1, so 2 D 3=8. At =4 the curves intersect at angle =8 . =8/ D =4. At 5=4 the curves intersect at angle 3=8 . 3=8/ D 3=4 (or =4 if you use the supplementary angle). y

rD1Csin 

rD1 cos 

 D =4

rD1 sin  x

x

Fig. 8.6-17 18. The two curves r 2 D 2 sin 2 and r D 2 cos  intersect where 2 sin 2 D 4 cos2 

4 sin  cos  D 4 cos2  .sin  cos  / cos  D 0 , sin  D cos  or cos  D 0;   p  and P2 D .0; 0/. 2; i.e., at P1 D 4 dr For r 2 D 2 sin 2 we have 2r D 4 cos 2 . At P1 we d p have r D 2 and dr=d D 0. Thus the angle between the curve and the radial line  D =4 is D =2. For r D 2 cos  we have dr=d D 2 sin  , so the angle between this curve ˇ and the radial line  D =4 satisfies r ˇˇ tan D D 1, and D 3=4. The two dr=d ˇD=4   3 D . curves intersect at P1 at angle 4 2 4 The Figure shows that at the origin, P2 , the circle meets the lemniscate twice, at angles 0 and =2.

Fig. 8.6-19 20.

We have r D cos  C sin  . For horizontal tangents:  d  dy D cos  sin  C sin2  d d D cos2  sin2  C 2 sin  cos  cos 2 D sin 2 , tan 2 D

0D ,

1:

3  or : The tangents are horizontal at Thus  D 8  8 "   #    cos sin ; and 8 8 8 "   #   3 3 3 cos C sin ; . 8 8 8 For vertical tangent:  d  2 dx D cos  C cos  sin  d d D 2 cos  sin  C cos2  sin2  sin 2 D cos 2 , tan 2 D 1:

0D ,

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SECTION 8.6 (PAGE 497)

ADAMS and ESSEX: CALCULUS 9

Thus There are vertical tangents at "  D =8 of 5=8.  #    C sin ; and cos 8 8 8 "   #   5 5 5 cos C sin ; . 8 8 8

There are no points on the curve where cos  D 0. Therefore, horizontal tangents occur only where    1 tan2  D 1=3: There are horizontal tangents at p ; ˙ 6 2   1 5 and p ; ˙ . 6 2 For vertical tangents:

y rDcos Csin 

,

d r cos  D r sin  C cos  d cos 2 sin  D sin 2 cos 

,

sin  D 0 or

0D

, .cos2 

x

Fig. 8.6-20

sin2  / sin  D



sin 2 r



2 sin  cos2 

3 cos2  D sin2 :

There are no points on the curve where tan2  D 3, so the only vertical tangents occur where sin  D 0, that is, at the points with polar coordinates Œ1; 0 and Œ1; . y

21.

r 2 Dcos 2

r D cot  . r D 2 cos  . tan D dr=d For horizontal tangents we want tan D tan  . Thus we want tan  D cot  , and so p  D ˙=4 or ˙3=4. The tangents are horizontal at Œ 2; ˙=4. For vertical tangents we want tan D cot  . Thus we want cot  D cot  , and so  D 0, ˙=2, or . There are vertical tangents at the origin and at Œ2; 0.

x

Fig. 8.6-22

y D=4

23. rD2 cos 

sin 2 D 2 cos 2 For horizontal tangents:

r D sin 2 . tan

D

1 2

tan 2 .

2 x

tan 2 D 2 tan  2 tan  D 2 tan  2 1 tan    tan  1 C .1 tan2  / D 0

D =4

Fig. 8.6-21

tan .2

tan2  / D 0:

p p Thus  D 0, , ˙ tan 1 2,  ˙ tan 1 2. There are horizontal tangents at the origin and the points dr 22. We have r D cos 2 , and 2r D d zontal tangents: 2

d r sin  D r cos  C sin  d cos 2 cos  D sin 2 sin 

0D ,

, .cos2  ,

342

2 sin 2 . For hori-



sin 2 r

sin2  / cos  D 2 sin2  cos 

cos  D 0 or

cos2  D 3 sin2 :



" p 2 2 ; ˙ tan 3

1

p

#

2

and

" p 2 2 ;  ˙ tan 3

1

p

#

2 :

Since the rosette r D sin 2 is symmetric about x D y, there must be vertical tangents at the origin and at the points " p 2 2 ; ˙ tan 3

1

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1 p 2

#

and

" p 2 2 ;  ˙ tan 3

1

# 1 p : 2

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

REVIEW EXERCISES 8 (PAGE 498)

y

y rD2.1 sin / x

x rDsin 2

Fig. 8.6-25

Fig. 8.6-23

24.

We have r D e  and

dr D e  . For horizontal tangents: d

d r sin  D e  cos  C e  sin  d  C k; tan  D 1 ,  D 4

0D ,

where k D 0; ˙1; ˙2; : : :. At the points Œe k =4 ; k =4 the tangents are horizontal. For vertical tangents: d r cos  D e  cos  e  sin  d  tan  D 1 $  D C k: 4

0D ,

At the points Œe cal. 25. r D 2.1

kC=4

sin  /, tan

; k C =4 the tangents are vertiD

For horizontal tangents tan

1

26.

dx dy D f 0 . / cos  f . / sin ; D f 0 . / sin  C f . / cos  d r d  2  2 f 0 . / cos  f . / sin  C f 0 . / sin  C f . / cos  d ds D  2  2 D f 0 . / cos2  2f 0 . /f . / cos  sin  C f . / sin2  1=2  2  2 d C f 0 . / sin2  C 2f 0 . /f . / sin  cos  C f . / cos2  r  2  2 D f 0 . / C f . / d:

Review Exercises 8 (page 498) 1.

sin  . cos  D cot  , so

sin  sin  D cos  cos  cos  D 0; or 2 sin  D 1: 1

The solutions are  D ˙=2, ˙=6, and ˙5=6.  D =2 corresponds to the origin where the cardioid has a cusp, and therefore no tangent. There are horizontal tangents at Œ4; =2, Œ1; =6, and Œ1; 5=6. For vertical tangents tan D cot  , so sin  cos  D cos  sin  sin2  sin  D cos2  D 1 1

sin2 

x D r cos  D f . / cos  , y D r sin  D f . / sin  .

2.

x2 C y2 D 1 2 p Ellipse, semi-major axis a D 2, along the x-axis. Semiminor axis b D 1. c 2 D a2 b 2 D 1. Foci: .˙1; 0/. x 2 C 2y 2 D 2

,

x2 y2 9x 2 4y 2 D 36 , D1 4 9 Hyperbola, transverse axis along the x-axis. Semi-transverse axis a D 2, semi-conjugate axis b D 3. p c 2 D a2 C b 2 D 13. Foci: .˙ 13; 0/. Asymptotes: 3x ˙ 2y D 0.

3.

x C y 2 D 2y C 3 , .y 1/2 D 4 x Parabola, vertex .4; 1/, opening to the left, principal axis y D 1. a D 1=4. Focus: .15=4; 1/.

4.

2x 2 C 8y 2 D 4x 48y 2.x 2 2x C 1/ C 8.y 2 C 6y C 9/ D 74

2

2 sin  sin  1 D 0 .sin  1/.2 sin  C 1/ D 0

.x

The solutions here are  D =2 (the origin again),  D =6 and  D 5=6. There are vertical tangents at Œ3; =6 and Œ3; 5=6.

.y C 3/2 1/2 C D 1: 37 37=4

Ellipse, p 3/, major axis along y D 3. p centre .1; a D 37, bpD 37=2, c 2 D a2 b 2 D 111=4. Foci: .1 ˙ 111=2; 3/.

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ADAMS and ESSEX: CALCULUS 9

y

5. x D t , y D 2 t , .0  t  2/. Straight line segment from .0; 2/ to .2; 0/.

. 2;4/

xDt 3 3t yDt 3 C3t

6. x D 2 sin.3t /, y D 2 cos.3t /, .0  t  2/ Part of a circle of radius 2 centred at the origin from the point .0; 2/ clockwise to .2 sin 6; 2 cos 6/.

x .2; 4/

7.

x D cosh t , y D sinh2 t . Parabola x 2 y D 1, or y D x 2 right.

1, traversed left to

Fig. R-8-12 13.

8. x D e t , y D e 2t , . 1  t  1/. Part of the curve x 2 y D 1 from .1=e; e 2 / to .e; 1=e 2 /. 9. x D cos.t =2/, y D 4 sin.t =2/, .0  t  /. The first quadrant part of the ellipse 16x 2 C y 2 D 16, traversed counterclockwise.

x D t 3 3t dx D 3.t 2 1/ dt Horizontal tangent Vertical tangent at

y D t3 dy D 3t 2 dt at t D 0, i.e., at .0; 0/. t D ˙1, i.e., at .2; 1/ and . 2; 1/.

 t2 dy > 0 if jt j > 1 D 2 < 0 if jt j < 1 dx t 1 Slope ! 1 as t ! ˙1. y

Slope

10. x D cos t C sin t , y D cos t sin t , .0  t  2/ The circle x 2 C y 2 D 2, traversed clockwise, starting and ending at .1; 1/.

tD1

11.

4 xD y D t 3 3t 1 C t2 dy dx 8t D 3.t 2 1/ D dt dt .1 C t 2 /2 Horizontal tangent at t D ˙1, i.e., at .2; ˙2/. Vertical tangent at t D 0, p i.e., at .4; 0/. Self-intersection at t D ˙ 3, i.e., at .1; 0/. y tD 1

p tD˙ 3

tD0

x

Fig. R-8-13 14.

x D t 3 3t dx D 3.t 2 1/ dt Horizontal tangent . 2; 16/. Vertical tangent at

y D t 3 C 3t x D t 3 3t dy dx D 3.t 2 1/ D 3.t 2 C 1/ dt dt Horizontal tangent: none. Vertical tangent at t D ˙1, i.e., at .2; 4/ and . 2; 4/. 

dy t C1 > 0 if jt j > 1 D 2 < 0 if jt j < 1 dx t 1 Slope ! 1 as t ! ˙1.

Slope

344

y D t 3 12t dy D 3.t 2 4/ dt at t D ˙2, i.e., at .2; 16/ and t D ˙1, i.e., at .2; 11/ and . 2; 11/.

Slope

Fig. R-8-11

2

x

 t2 4 dy > 0 if jt j > 2 or jt j < 1 D 2 < 0 if 1 < jt j < 2 dx t 1 Slope ! 1 as t ! ˙1. y . 2;16/

tD1

12.

tD 1

.2;11/

xDt 3 3t yDt 3 12t . 2; 11/

.2; 16/

Fig. R-8-14

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x

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INSTRUCTOR’S SOLUTIONS MANUAL

15.

REVIEW EXERCISES 8 (PAGE 498)

The curve x D t 3 t , y D jt 3 j is symmetric about x D 0 since x is an odd function and y is an even function. Its self-intersection occurs at a nonzero value of t that makes x D 0, namely, t D ˙1. The area of the loop is

19.

r D ;

3 2

 

3 2



y

rD

Z 1 .t 3 t /3t 2 dt . x/ dy D 2 0 tD0  ˇ1 3 4 ˇˇ 1 6 D t C t ˇ D sq. units. ˇ 2 2

AD2

Z

tD1

x

0

y

Fig. R-8-19 x D t3 t y D jt 3 j

20.

r D j j;

. 2    2/ y rDjj

tD˙1

x

tD0

x

Fig. R-8-15 16. The volume of revolution about the y-axis is V D D

Z

.t 6

0

D 3 x D et

Z

1

.t 8

0



Fig. R-8-20

x 2 dy

tD0 Z 1

D 3

17.

tD1

1 9

21.

2t 4 C t 2 /3t 2 dt

r D 1 C cos.2 /

y

2t 6 C t 4 / dt  2 1 8 C cu. units. D 7 5 105

rD1Ccos 2

x

t , y D 4e t=2 , .0  t  2/. Length is Z

2

p .e t

1/2 C 4e t dt Z 2p Z 2 D .e t C 1/2 dt D .e t C 1/ dt 0 0 ˇ2 ˇ t D .e C t /ˇˇ D e 2 C 1 units:

LD

0

Fig. R-8-21 22.

r D 2 C cos.2 /

y rD2Ccos.2/

0

18. Area of revolution about the x-axis is Z S D 2 4e t=2 .e t C 1/ dt ˇˇ2  2 3t=2 t=2 ˇ e C 2e D 8 ˇ ˇ 3

x

Fig. R-8-22

0

16 3 D .e C 3e 3

4/ sq. units.

23.

r D 1 C 2 cos.2 /

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y

27. rD1C2 cos 2

x

Z =4 p 1 AD2 .1 C 2 2 sin  C 2 sin2  / d 2 =2 Z =4 p D .2 C 2 2 sin  cos.2 // d =2

Fig. R-8-23

24.

r D1

 D 2

sin.3 / y

p the origin in the directions for r D 1C 2 sin  approaches p which sin  D 1= 2, that is,  D 3=4 and  D =4. The smaller loop corresponds to values of  between these two values. By symmetry, the area of the loop is

 D 2

rD1 sin.3/

p

2 2 cos 

ˇˇ 1 ˇ sin.2 / ˇ ˇ 2

=4

=2

1  3 2C D sq. units. 2 2

p rD1C 2 sin 

y =6

x

3=4

Fig. R-8-27

Fig. R-8-24 28. 25. Area of a large loop:

AD2 D

Z

1 2

=3

Z

=3 0

D

Z

1 2

=2 =3

=2 =3

346

p Only . 2

1/=2 is between

value of cos  . Let 0 D cos v u u sin 0 D t1

p

1

1

:

1pand 1, so is a possible 2 1 . Then 2

2 1 2

!2

D

p

p 1C2 2 : 2

By symmetry, the area inside r D 1 C cos  to the left of the line x D 1=4 is

.1 C 2 cos.2 //2 d

Œ1 C 4 cos.2 / C 2.1 C cos.4 // d

ˇˇ=2 1 ˇ D 3 C 2 sin.2 / C sin.4 / ˇ ˇ 2 =3 p  3 3 D sq. units. 2 4 

1 4 cos  4 cos2  C 4 cos  1 D 0 p p 4 ˙ 16 C 16 ˙ 2 D cos  D 8 2

.1 C 2 cos.2 //2 d

26. Area of a small loop: AD2

r cos  D x D 1=4 and r D 1 C cos  intersect where 1 C cos  D

Œ1 C 4 cos.2 / C 2.1 C cos.4 // d 0 ˇˇ=3  1 ˇ D 3 C 2 sin.2 / C sin.4 / ˇ ˇ 2 0 p 3 3 sq. units. DC 4

Z

x

=4

  1 C cos.2 / 1 C 2 cos  C d C cos 0 sin 0 2 0 ˇ  ˇ 3 1 ˇ D . 0 / C 2 sin  C sin.2 / ˇ ˇ 2 4 0 p p p . 2 1/ 1 C 2 2 C 4 ! q ! p p p 3 2 1 2 9 1  cos C 1C2 2 sq. units. D 2 2 8

AD2

1 2

Z



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INSTRUCTOR’S SOLUTIONS MANUAL

y

xD1=4

CHALLENGING PROBLEMS 8 (PAGE 498)

rD1Ccos 

0

C1

x

A1 S1

Fig. R-8-28 C

Challenging Problems 8

(page 498)

P

F1

F2 C2 A2

1.

The surface of the water is elliptical (see Problem 2 below) whose semi-minor axis is 4 cm, the radius of the cylinder, and whose semi-major axis is 4 sec  cm because of the tilt of the glass. The surface area is that of the ellipse x D 4 sec  cos t; y D 4 sin t;

S2

Fig. C-8-2 Let P be any point on C . Let A1 A2 be the line through P that lies on the cylinder, with A1 on C1 and A2 on C2 . Then PF1 D PA1 because both lengths are of tangents drawn to the sphere S1 from the same exterior point P . Similarly, PF2 D PA2 . Hence

.0  t  2/:

This area is AD4 D4

Z

Z

tD=2

PF1 C PF2 D PA1 C PA2 D A1 A2 ;

x dy tD0 =2

.4 sec  cos t /.4 cos t / dt Z =2 D 32 sec  .1 C cos.2t // dt D 16 sec  cm2 :

which is constant, the distance between the centres of the two spheres. Thus C must be an ellipse, with foci at F1 and F2 .

0

3.

0



4 cm

Given the foci F1 and F2 , and the point P on the ellipse, construct N1 PN2 , the bisector of the angle F1 PF2 . Then construct T1 P T2 perpendicular to N1 N2 at P . By the reflection property of the ellipse, N1 N2 is normal to the ellipse at P . Therefore T1 T2 is tangent there. N2 T1 P

4 sec  cm

T2   N1 F1

F2

Fig. C-8-1

2. Let S1 and S2 be two spheres inscribed in the cylinder, one on each side of the plane that intersects the cylinder in the curve C that we are trying to show is an ellipse. Let the spheres be tangent to the cylinder around the circles C1 and C2 , and suppose they are also tangent to the plane at the points F1 and F2 , respectively, as shown in the figure.

Fig. C-8-3 4.

Without loss of generality, choose the axes and axis scales so that the parabola has equation y D x 2 . If P is the point .x0 ; x02 / on it, then the tangent to the parabola at P has equation y D x02 C 2x0 .x x0 /;

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347

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CHALLENGING PROBLEMS 8 (PAGE 498)

ADAMS and ESSEX: CALCULUS 9

which intersects the principal axis x D 0 at .0; x02 /. Thus R D .0; x02 / and Q D .0; x02 /. Evidently the vertex V D .0; 0/ bisects RQ. y

y

6.

P D Œr;   Œa; 0  r

Q

P D

.x0 ; x02 /

a 

L

0 x

x

V

Fig. C-8-6 R

a) Let L be a line not passing through the origin, and let Œa; 0  be the polar coordinates of the point on L that is closest to the origin. If P D Œr;   is any point on the line, then, from the triangle in the figure,

Fig. C-8-4 To construct the tangent at a given point P on a parabola with given vertex V and principal axis L, drop a perpendicular from P to L, meeting L at Q. Then find R on L on the side of V opposite Q and such that QV D VR. Then PR is the desired tangent.

a D cos. r

rD

a : cos. 0 /

b) As shown in part (a), any line not passing through the origin has equation of the form r D g. / D

5. y b

or

0 /;

a D a sec. cos. 0 /

0 /;

for some constants a and 0 . We have

c

g 0 . / D a sec.

0 / tan.

g 00 . / D a sec.

2 ft 2 ft

C a sec3 .

a x

D a2 sec2 . 2

2

0 /

0 / tan2 . 0 /  2  2 0 / g. / C 2 g 0 . /

0 / C 2a2 sec2 . 2

g. /g 00 . /

0 / tan2 . 2

0 /

4

a sec . 0 / tan . 0 / a sec . 0 / h   i D a sec2 . 0 / 1 C tan2 . 0 / sec4 . 0 / 2

D 0:

Fig. C-8-5 x2 y2 C 2 D 1, with a D 2 and foci at 2 a b .0; ˙2/ so that c D 2 and b 2 D a2 C c 2 D 8. The volume of the barrel is

c) If r D g. / is the polar equation of the tangent to r D f . / at  D ˛, then g.˛/ D f .˛/ and g 0 .˛/ D f 0 .˛/. Suppose that 

Let the ellipse be

Z

Z

2

2

 4 1

x 2 dy D 2 0 0 ˇ2  3 ˇ 40 3 y ˇ ft : D 8 y ˇ D 24 ˇ 3

V D2

0

348

2

y 8

2  2 f .˛/ C 2 f 0 .˛/

f .˛/f 00 .˛/ > 0:

By part (b) we have 

dy

2  2 g.˛/ C 2 g 0 .˛/

g.˛/g 00 .˛/ D 0:

Subtracting, and using g.˛/ D f .˛/ and g 0 .˛/ D f 0 .˛/, we get f 00 .˛/ < g 00 .˛/. It follows

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INSTRUCTOR’S SOLUTIONS MANUAL

CHALLENGING PROBLEMS 8 (PAGE 498)

that f . / < g. / for values of  near ˛; that is, the graph of r D f . / is curving to the origin side of its tangent at ˛. Similarly, if 

 2 2 f .˛/ C 2 f 0 .˛/

f .˛/f 00 .˛/ < 0;

8.

Take the origin at station O as shown in the figure. Both of the lines L1 and L2 pass at distance 100 cos  from the origin. Therefore, by Problem 6(a), their equations are 100 cos  100 cos    D  sin. C / cos   2 100 cos  100 cos    D : rD  sin. / cos  C 2

L1 W

then the graph is curving to the opposite side of the tangent, away from the origin.

rD

L2 W

The search area A./ is, therefore,

7.

x.t /

0

B

A x





 1002 cos2  1002 cos2  d  sin2 . / sin2 . C / 4  Z  C   4 csc2 . / csc2 . C / d D 5; 000 cos2  

1 A./ D 2

Z

 4 C

r

R





4

  D 5; 000 cos  cot 4 C 2 2 cot 4 C cot 4 2 # "   cos 4 C 2 sin 4 C 2 2   C 2 D 5; 000 cos  sin 4 C 2 cos 4 C 2    D 10; 000 cos2  csc 2 C 4 1 2

D 10; 000 cos2 .sec.4/

1/ mi2 :

For  D 3ı D =60, we have A./  222:8 square miles. Also A0 ./ D

Fig. C-8-7 When the vehicle is at position x, as shown in the figure, the component of the gravitational force on it in the direction of the tunnel is ma.r/ cos  D

20; 000 cos  sin .sec.4/

When  D 3ı , the search area increases at about 8645.=180/  151 square miles per degree increase in . y

mg x: R

mgr cos  D R

 L2 L1

By Newton’s Law of Motion, this force produces an acceleration d 2 x=dt 2 along the tunnel given by d 2x m 2 D dt

1/

C 40; 000 cos2  sec.4/ tan.4/ A0 .=60/  8645:

Area A./

100 mi mg x; R

 =4

that is d 2x C ! 2 x D 0; dt 2

x

O where

g ! D : R 2

Fig. C-8-8

This is the equation ofpsimple harmonic motion, with period T D 2=! D 2 R=g. For R  3960 mi  2:09  107 ft, and g  32 ft/s2 , we have T  5079 s  84:6 minutes. This is a rather short time for a round trip between Atlanta and Baghdad, or any other two points on the surface of the earth.

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349

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CHALLENGING PROBLEMS 8 (PAGE 498)

9. The easiest way to determine which curve is which is to calculate both their areas; the outer curve bounds the larger area. The curve C1 with parametric equations

x D sin t;

1 y D sin.2t /; 2

.0  t  2/

ADAMS and ESSEX: CALCULUS 9

The curve C2 with polar equation r 2 D cos.2 / has area 4 A2 D 2

Z

0

=4

ˇ=4 ˇ ˇ cos.2 / d D sin.2 /ˇ D 1 sq. units. ˇ 0

C1 is the outer curve, and the area between the curves is 1/3 sq. units. y

has area

x

A1 D 4 D4

Z

tD=2

Z

D4

Z

Fig. C-8-9

y dx tD0 =2

0

D4 Let u D cos t du D sin t dt

350

Z

=2

1 sin.2t / cos t dt 2 sin t cos2 t dt

0

0

1

u2 du D

4 sq. units. 3

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 9.1 (PAGE 507)

CHAPTER 9. SEQUENCES, SERIES, AND POWER SERIES Section 9.1 Sequences and Convergence (page 507) 1.

2.

3.

4.

5.

6.

7.

8.

     2 8 9 2n2 D 2 D 1; ; ; : : : is bounded, n2 C 1 n2 C 1 5 5 positive, increasing, and converges to 2. ) (   2n 4 3 8 D 1; ; ; ; : : : is bounded, positive, den2 C 1 5 5 17 creasing, and converges to 0.     . 1/n 7 13 4 D 5; ; ; : : : is bounded, positive, and n 2 3 converges to 4. ( )       1 1 1 D sin 1; sin ; sin ; : : : is bounded, sin n 2 3 positive, decreasing, and converges to 0.  2      n 1 1 3 8 15 D n D 0; ; ; ; : : : is bounded n n 2 3 4 below, positive, increasing, and diverges to infinity. ) (  n e e  e 2  e 3 ; ; ; : : : is bounded, positive, D n    decreasing, and converges to 0, since e < .   n    p e n e p D . Since e=  > 1, the sequence   n=2 is bounded below, positive, increasing, and diverges to infinity. ) (   3 . 1/n n 1 2 ; ; : : : is bounded, alternating, ; D en e e2 e3 and converges to 0.

14.

5 5 2n n D lim lim 3n 7 3

15.

4 n n2 4 n D 1: lim D lim 5 nC5 1C n

16.

n2 lim 3 D lim n C1



n

n

9. f2 =n g is bounded, positive, decreasing, and converges to 0.  n 1 2 3 n 1 .nŠ/2 . D   10. .2n/Š nC1 nC2 nC3 2n 2 2 anC1 .n C 1/ 1 Also, D < . Thus the sequence a .2n C 2/.2n C 1/ 2  n .nŠ/2 is positive, decreasing, bounded, and convergent .2n/Š to 0. fn cos.n=2/g D f0; 2; 0; 4; 0; 6; : : :g is divergent. ) (   sin 2 sin 3 sin n ; ; : : : is bounded and conD sin 1; 12. n 2 3 verges to 0. 11.

13. f1; 1; 2; 3; 3; 4; 5; 5; 6; : : :g is divergent.

17.

lim. 1/n

n2 18. lim 1

19.

20.

21.

22.

23.

24.

25.

lim

2 7 n

1 n 1C

2 : 3

D

D 0:

1 n3

n D 0: n3 C 1 2 1 p 1 p C 2 2 nC1 n n n D lim D 1 1 n 3n2 3 2 n n

en e en C e

n n

D lim

1 e 1Ce

1 : 3

2n 2n

D 1:

sin x cos x 1 D lim D lim D 1: x!0C x!0C n x 1     3 n n 3 n D lim 1 C D e 3 by l’H^opital’s lim n n Rule. x n D lim lim x!1 ln.x C 1/ ln.n C 1/ 1  D lim x C 1 D 1: D lim  x!1 x!1 1 xC1 lim n sin

p lim. n C 1  lim n

p

n/ D lim p

nC1

n p D 0: nC1C n

 n2 .n2 4n/ 4n D lim p n C n2 4n 4 4n r D 2: p D lim D lim 2 4 nC n 4n 1C 1 n p p lim. n2 C n n2 1/ p

n2

n2 C n .n2 1/ D lim p p n2 C n C n2 1 nC1 ! D lim r r 1 1 n 1C C 1 n n2 D lim r

1C

1C 1 C n

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1 n r

1

1 n2

D

1 : 2

351

lOMoARcPSD|6566483

SECTION 9.1 (PAGE 507)

26. If an D



n 1 nC1

n

ADAMS and ESSEX: CALCULUS 9

Thus, fan g is increasing by induction. Observe that a1 < 5 and a2 < 5. If ak < 5 then

, then

n n lim an D lim n nC1  n ,   1 1 n D lim 1 lim 1 C n n 

D

27.

n

1

e

De

e

1

n 

2

akC1 D

(by Theorem 6 of Section 3.4).

.1  2  3    n/.1  2  3    n/ .nŠ/2 D .2n/Š 1  2  3    n  .n C 1/  .n C 2/    2n  n 1 2 3 n 1 D     : nC1 nC2 nC3 nCn 2 Thus lim an D 0.

aD

32.

n2 D 0 since 2n grows much faster than n2 2n

p

15 C 2a ) a2

!

4n lim nŠ

!

D 0:

n ) 0 < an < .=4/n . Since =4 < 1, 1 C 22n therefore .=4/n ! 0 as n ! 1. Thus lim an D 0. p 30. Let a1 D 1 and anC1p D 1 C 2an for n D 1; 2; 3; : : :. Then we have a2 D 3 > a1 . If akC1 > ak for some k, then p

1 C 2akC1 >

p

b) Since ln x  x

p

p p p p 1 C 2ak < 1 C 2.3/ D 7 < 9 D 3:

1 C 2a ) a2

2a

1D0)a D1˙

p

352

25 D 5:

p p 15 C 2akC1 > 15 C 2ak D akC1 :

15 D 0 ) a D

3; or a D 5:

1

1,  1 D1

which implies that ak  e for all k. Since fan g is increasing, e is an upper bound for fan g. 33.

2:

p 2 < 0, p it is not appropriate. Hence, we Since a D 1 must have lim an D 1 C 2. p 31. Let a1 D 3 and anC1pD 15 C 2an for n D 1; 2; 3; : : :. Then we have a2 D 21 > 3 D a1 . If akC1 > ak for some k, then akC2 D

2a

   1 1 ln ak D k ln 1 C k 1C k k

1 C 2ak D akC1 :

Therefore, an < 3 for all n, by induction. Since fan g is increasing and bounded above, it converges. Let lim an D a. Then aD

p

Since f 0 .x/ > 0, f .x/ must be an increasing function. Thus, fan g D fe f .xn / g is increasing.

Thus, fan g is increasing by induction. Observe that a1 < 3 and a2 < 3. If ak < 3 then akC1 D

15 C 2.5/ D

x ln x f 0 .x/ D ln.x C 1/ C x C 1   xC1 1 D ln x xC1 Z xC1 dt 1 D t xC1 x Z xC1 1 1 dt > xC1 x xC1 1 1 D 0: D xC1 xC1

29. an D

akC2 D

p

Since a > a1 , we must have lim an D 5.     1 1 n so ln an D n ln 1 C . Let an D 1 C n n   1 a) If f .x/ D x ln 1 C D x ln.x C 1/ x ln x, then x

4n and lim D 0 by Theorem 3(b). Hence, nŠ n2 22n n2 n2 2n D lim n  D lim n lim nŠ 2 nŠ 2

15 C 2ak
K, and hence aj > K for all j  n. Thus lim an D 1. If fan g is ultimately decreasing, then either it is bounded below, and therefore converges, or else it is unbounded below, and therefore diverges to negative infinity.

34.

If fjan jg is bounded then it is bounded above, and there exists a constant K such that jan j  K for all n. Therefore, K  an  K for all n, and so fan g is bounded above and below, and is therefore bounded.

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 9.2 (PAGE 514)

35. Suppose limn!1 jan j D 0. Given any  > 0, there exists an integer N D N./ such that if n > N , then jjan j 0j < . In this case jan 0j D jan j D jjan j 0j < , so limn!1 an D 0.

3.

nD5

b) “If lim an D 1 and lim bn D 1, then lim.an C bn / D 0” is FALSE. Let an D 1 C n and bn D n; then lim an D 1 and lim bn D 1 but lim.an C bn / D 1.

1 .2 C /10 1 D .2 C /10 1 D .2 C /10

4.

d) “If neither fan g nor fbn g converges, then fan bn g does not converge” is FALSE. Let an D bn D . 1/n ; then lim an and lim bn both diverge. But an bn D . 1/2n D 1 and fan bn g does converge (to 1). e) “If fjan jg converges, then fan g converges” is FALSE. Let an D . 1/n . Then limn!1 jan j D limn!1 1 D 1, but limn!1 an does not exist.

5.

6.

D

1  3

1 1

1 3

D

5 1

7.

(page 514)

2. 3

3 3 C 4 16

3 C D 64

nD1

3

D

i:

5000 : 999

 2 1 X 1 1 1 C  D D 1 C C en e e

1 1

1 e

D

e e

1

:

1  k 1 X X 2 8e 3 2kC3 8e 4 3 D 8e D : D k 3 2 e e 2 e kD0 1 kD0 e

P1

P  j=2 cos.j/ D j1D2 . 1/j  j=2 diverges because limj !1 . 1/j  j=2 does not exist. j D1

P1

nD1

3 C 2n diverges to 1 because 2nC2 3 C1 n 3 C 2n 1 2 lim D lim D > 0: nC2 n!1 2 n!1 4 4

1 : 2

1   1   1 X 1X 1 n 1X 2 n 3 C 2n C D 3nC2 3 3 9 3 nD0

nD0



1

1 X . 5/2 . 5/3 . 5/4 . 5/n D C C C  2n 4 6 8 8 8 88 nD2   52 25 5 C 2  D 4 1 8 64 64 25 1 25 25 D 4  D : D 5 8 64  69 4416 1C 64

!  2 1 C  3

10. 1 X

1 1000

nD0

9.

1.

1 1 C C C  .2 C /12 .2 C /14   1 1 C C    1C .2 C /2 .2 C /4 1 1 h  D 1 8 .2 C / .2 C /2 1 .2 C /2

# "  2 1 1 5 C  D5 1C C 103n 1000 1000 D

8.

1 1 1 1 1 C C C  D 1C C 3 9 27 3 3

1 X

nD0

c) “If lim an D 1 and lim bn D 1, then lim an bn D 1” is TRUE. Let R be an arbitrary, large positive number. Since lim an D p1 R and lim bn D 1, we must have a  n p R, for all sufficiently large n. Thus and bn  an bn  R, and lim an bn D 1.

Section 9.2 Infinite Series

1 .2 C /2n

D

a) “If lim an D 1 and lim bn D L > 0, then lim an bn D 1” is TRUE. Let R be an arbitrary, large positive number. Since lim an D 1, and L > 0, 2R it must be true that an  for n sufficiently large. L L for n Since lim bn D L, it must also be that bn  2 2R L sufficiently large. Therefore an bn  D R for n L 2 sufficiently large. Since R is arbitrary, lim an bn D 1.

36.

1 X

1 4

n

1

D

3 1C

1 4

D

12 : 5

1 D  3

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nD0

1

1

1 1 5 1 1 C  D C D : 1 2 9 2 3 6 1 3 3

353

lOMoARcPSD|6566483

SECTION 9.2 (PAGE 514)

11.

1 1 D n.n C 2/ 2

Since



1 n

ADAMS and ESSEX: CALCULUS 9

 1 , therefore nC2

14.

1 1 1 1 C C C  C 13 24 35 n.n C 2/  1 1 1 1 1 1 1 1 1 D C C C C  2 1 3 2 4 3 5 4 6  1 1 1 1 1 1 C C C n 2 n n 1 nC1 n nC2   1 1 1 1 D 1C : 2 2 nC1 nC2

sn D

Thus lim sn D

Hence,

1 X 1 3 3 , and D . 4 n.n C 2/ 4

nD1

nD1

1 1 1 1 D C C C : 1/.2n C 1/ 13 35 57

1 1 D .2n 1/.2n C 1/ 2 partial sum is Since

 1 sn D 1 2



1 2n

1

 1 , the 2n C 1

  1 1 1 C C  2 3 5   1 1 1 1 1 C C 2 2n 3 2n 1 2 2n 1   1 1 D 1 : 2 2n C 1 1 3 



16.

17.

1 2n C 1

nD1

13. Since

.3n

fore

.2n



1 1 D lim sn D : 1/.2n C 1/ 2

1 1 D 2/.3n C 1/ 3



1 3n

2

 1 , there3n C 1

1 1 1 1 C C C  C 14 47 7  10 .3n 2/.3n C 1/  1 1 1 1 1 1 1 C C C  D 3 1 4 4 7 7 10  1 1 1 1 C C 3n 5 3n 2 3n 2 3n C 1   1 1 1 : D 1 ! 3 3n C 1 3

Thus

354

nD1

.3n

1 1 D . 2/.3n C 1/ 3

1 1 D lim sn D : n.n C 1/.n C 2/ 4

1 1 1 1 > D  , therefore the partial sums 2n 1 2n 2 n of the given series P exceed half those of the divergent harmonic series .1=2n/. Hence the given series diverges to infinity. 1 X

n n diverges to infinity since lim D 1 > 0. nC2 nC2

Since n

1=2

1 1 D p  for n  1, we have n n n X

k

kD1

1=2



n X 1 ! 1; k

kD1

P 1=2 as n ! 1 (harmonic series). Thus n diverges to infinity.   1 X 1 1 1 2 D 2 C C C    diverges to infinity 18. nC1 2 3 4 nD1 since it is just twice the harmonic series with the first term omitted. n 1 if n is odd 19. sn D 1 C 1 1 C    C . 1/n D . P 0 n if n is even Thus lim sn does not exist, and . 1/ diverges.

20.

sn D

P1

 2 1 C ; nC1 nC2

Since

nD1

Hence, 1 X

1 X

nD1

15. .2n

 1 1 1 D n.n C 1/.n C 2/ 2 n

the partial sum is     1 1 1 2 1 1 2 sn D C C 1 C C  2 2 3 2 2 3 4     1 2 1 2 1 1 1 1 C C C C 2 n 1 n nC1 2 n nC1 nC2   1 1 1 1 D C : 2 2 nC1 nC2

12. Let 1 X

Since

21.

n.n C 1/ Since 1 C 2 C 3 C    C n D , the given series 2 P1 2 is nD1 which converges to 2 by the result of n.n C 1/ Example 3 of this section. The total distance is "

#  2 3 3 C  C2 4 4 # "  2 3 3 3 C  1C C D2C2 2 4 4

2C2 2

D2 C

3

1

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3 4

D 14 metres.

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 9.3 (PAGE 524)

29.

“If an  c > 0 for all n, then TRUE. We have

P

an diverges to infinity” is

sn D a1 C a2 C a3 C    C an  c C c C c C    C c D nc; and nc ! 1 as n ! 1.

2 m

30.

Fig. 9.2-21 22. The balance at the end of 8 years is

31.

h i sn D 1000 .1:1/8 C .1:1/7 C    C .1:1/2 C .1:1/   .1:1/8 1 D 1000.1:1/  $12; 579:48: 1:1 1 23. For n > N let sn D

n X

j D1

aj , and Sn D

Then sn D Sn C C , where C D

n X

j DN PN 1 j D1 aj .

P an diverges and fbn g is bounded, then an bn 1 1 and bn D . diverges” is FALSE. Let an D n n C 1 P Then an D 1 and 0  bn  1=2. But P P 1 which converges by Example an bn D n.n C 1/ 3. “If

P

P P 2 “If an > 0 and an converges, then an converges” is TRUE.P Since an converges, therefore lim an D 0. Thus there exists N such that 0 < an  1 for n  N . Thus 0 < an2  an for n  N . n n X X If Sn D ak2 and sn D ak , then fSn g is increasing kDN

aj .

Sn  sn 

We have

lim sn D lim Sn C C W

n!1

n!1

eitherPboth sides exist or neither does. Hence and 1 nDN both converge or neither does.

P1

nD1

Thus an

If fan g is ultimately positive, then the sequence fsn g of partial sums of the series must be ultimately increasing. By Theorem 2, if fsn g is ultimately increasing, then either it is bounded above, and therefore convergent, or else it Pis not boundedPabove and diverges to infinity. Since an D lim sn , an must either converge when fsn g converges and lim sn D s exists, or diverge to infinity when fsn g diverges to infinity. P 25. If fan g is ultimately negative, then the series an must either converge (if its partial sums are bounded below), or diverge to 1 (if its partial sums are not bounded below). P 26. “If an D 0 forPevery n, then an converge” is TRUE n 0 D 0, for every n, and so because s D n kD0 P an D lim sn D 0. P P 27. “If an converges, then 1=a Pn diverges to infinity” is FALSE. A counterexample is . 1/n =2n . P P 28. “If an and bn both diverge, then so does P 1 .an C bn /” is FALSE. Let an D and n P P 1 bn D , then an D 1 and bn D 1 but n P P .an C bn / D .0/ D 0.

24.

kDN

and bounded above:

1 X

1 X

kD1

ak2 converges, and so

kDN

ak < 1: 1 X

ak2 converges.

kD1

Section 9.3 Convergence Tests for Positive Series (page 524)

1.

2.

X 1 1 since converges by comparison with n2 C 1 n2 1 1 0< 2 < 2. n C1 n

X

1 X

nD1

n n4

2

converges by comparison with

nD1



n

4  lim n

3.

1 X 1 since n3

X n2 C 1

1 n3

2



D 1;

and 0 < 1 < 1:

diverges to infinity by comparison with n3 C 1 2 1 n C1 > . since 3 n C1 n

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X1 , n

355

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SECTION 9.3 (PAGE 524)

4.

1 X

nD1

ADAMS and ESSEX: CALCULUS 9

p

n2

since

1 X 1 n converges by comparison with 3=2 CnC1 n nD1

lim



p

n n2 C n C 1   1 n3=2



D 1;

and

0 < 1 < 1:

14.

1 X

1 p diverges to infinity by the integral test, n ln n ln ln n nD3 since Z 1 Z 1 dt du p D p D 1: u t ln t ln ln t 3 ln ln 3 1 X

1 converges by the integral test: n ln n.ln ln n/2

nD2

Z

5. Since sin x  x for x  0, we have ˇ ˇ ˇ ˇ ˇsin 1 ˇ D sin 1  1 ; ˇ n2 ˇ n2 n2

6.

13.

ˇ X ˇˇ X 1 ˇ ˇsin 1 ˇ converges by comparison with so . ˇ n2 ˇ n2 1 X

1 converges by comparison with the geometric n C 5 nD8 1  n X 1 1 1 series since 0 < n < n.   C5 

15.

16.

a

dt D t ln t .ln ln t /2

X

1

n

D lim

1

D 1, the series n n converges by comparison with the geometric

9. Since limn!1

n

n

1

 n n X 1 . series n 1 X 1Cn 1Cn 10. diverges to infinity since lim D 1 > 0. 2Cn 2Cn nD0

11.

X 1 C n4=3 diverges to infinity by comparison with the 2 C n5=3 X 1 divergent p-series , since n1=3 , n1=3 C n5=3 1 1 C n4=3 D lim D 1: lim 5=3 1=3 n!1 2 C n n 2 C n5=3 1 X

D2

du < 1 if ln ln a > 0: u2

1 X

1 p X 1 1 p D 2 p 2k k kD1 kD1

diverges to infinity. X 1 1 1 , the series < con2n .n C 1/ 2n 2n .n C 1/ X 1 . verges by comparison with the geometric series 2n 1 X n4 converges by the ratio test since 18. nŠ 17.

Since

nD1

.n C 1/4   nC1 4 1 .n C 1/Š D 0: D lim lim n nC1 n4 nŠ

19.

X nŠ diverges to infinity by the ratio test, since n2 e n  D lim

20.

.n C 1/Š n2 e n 1 n2  D lim D 1: .n C 1/2 e nC1 nŠ e nC1

1 X .2n/Š6n converges by the ratio test since .3n/Š

nD1

.2n C 2/Š6nC1 lim .3n C 3/Š

n2 p D 1. 1Cn n

356

ln ln a

X 1 . 1/n converges by comparison with , 4 n n4 n 2 1 . 1/ since 0   4. n4 n The series

n2 12. p diverges to infinity since 1Cn n nD1 lim

1

X1

7.

nD1

Z

1 X 2 2 2 1 C . 1/n p D 0 C p C 0 C p C 0 C p C  n 2 4 6 nD1

nD8

X 1 Since .ln n/3 < n for large n, diverges to .ln n/3 X1 . infinity by comparison with n 1 X 1 8. diverges to infinity by comparison with the ln.3n/ nD1 1 X 1 1 1 since > for n  1. harmonic series 3n ln.3n/ 3n

1

D lim

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,

.2n/Š6n .3n/Š

.2n C 2/.2n C 1/6 D 0: .3n C 3/.3n C 2/.3n C 1/

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

21.

SECTION 9.3 (PAGE 524)

p 1 X n converges by the ratio test, since 3n ln n

We use the approximation

nD2

s  sn D sn C

p

3n ln n nC1  p  D lim nC1 3 ln.n C 1/ n r 1 ln n 1 nC1 D lim  lim D < 1: 3 n ln.n C 1/ 3 22.

24.

1 X 1 C nŠ diverges by comparison with the harmonic .1 C n/Š nD1 1 X 1 C nŠ nŠ 1 1 since > D . series nC1 .1 C n/Š .1 C n/Š nC1

25.

2n

3n

n3

 D lim D

26.

  1 1 1 2 3n3 3.n C 1/3 1 .n C 1/3 n3 D 6 n3 .n C 1/3 1 3n2 C 3n C 1 7 D < : 6 n3 .n C 1/3 6n4

  1 X 1 1 1 1 1 1 1 1 1   s C C C C C C D 1 C 6 n4 24 34 44 54 64 6 73 63

nD1

 1:082

2 lim 3

28.

converges by the ratio test since

3nC1

3n n3 2nC1  3 .n C 1/ 2n 3

n

3n

3

n 2 D lim 3 .n C 1/3 1 3

with error less than 0.001 in absolute value:

1 is positive, continuous and decreasing x3 on Œ1; 1/, for any n D 1; 2; 3; : : :, we have Since f .x/ D

sn C AnC1  s  sn C An 1

n3 2 3n D < 1: 3 .n C 1/3 3nC1

where sn D

Z 1 n X 1 dx 1 and A D D . If n 3 2 k3 x 2n n

kD1

1 sn D sn C .AnC1 C An /, then 2

1 X nn converges by the ratio test since  n nŠ

jsn

27.

,

  nn e 1 1 n D D lim 1 C < 1:  n nŠ  n 

f .x/ D 1=x 4 is positive, continuous, and decreasing on Œ1; 1/. Let An D

Z

n

1

 ˇR 1 ˇˇ dx 1 D lim ˇ D 3: R!1 x4 3x 3 ˇ 3n

 AnC1 1 1 D 2 4 n2 1 2n C 1 < 0:001 D 4 n2 .n C 1/2

sn j 

nD1

.n C 1/nC1 lim .nC1/  .n C 1/Š

:

that is, if n4 > 7000=6. Since 64 D 1296 > 7000=6, n D 6 will do. Thus

nD1

X



We have used 3n2 C 3n C 1  7n2 and n3 .n C 1/3 > n6 to obtain the last inequality. We will have js sn j < 0:001 provided 7 < 0:001; 6n4

X .2n/Š converges by the ratio test, since .nŠ/3 .2n C 2/Š .nŠ/3 .2n C 2/.2n C 1/  D lim D 0 < 1: ..n C 1/Š/3 .2n/Š .n C 1/3

1 1 C 3 3.n C 1/3 3n

sn j 

js

1 X n100 2n converges by the ratio test since p nŠ nD0

 D lim



The error satisfies

, .n C 1/100 2nC1 n100 2n lim p p nŠ .n C 1/Š  100 nC1 1 p D 0: D lim 2 n nC1

23.

1 2

An

1 .n C 1/2



if n D 8. Thus, the error in the approximation s  s8 is less than 0.001. 29.

Since f .x/ D

1 x 3=2

is positive, continuous and decreasing

on Œ1; 1/, for any n D 1; 2; 3; : : :, we have

n

sn C AnC1  s  sn C An

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357

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SECTION 9.3 (PAGE 524)

n X

ADAMS and ESSEX: CALCULUS 9

Z

1

2 dx D p . If n x 3=2 n kD1   1 1 1 sn D sn C .AnC1 C An / D sn C p C p , then 2 n nC1

where sn D

sn j 

jsn

D D
: 2 4 6 2n 2 2n 2n

with the harmonic series

44.

nD1

360

1 . 2n

k

2k 2 D 0 1/

For given n, the p upper bound is minimal if n2 C 8 nC2 (for n  2). kD 2.n 1/

diverges to infinity by comparison 1 X

1/k 2

.n C 2/ ˙

an D

nD1

k.n C 1/ C 1

.n C 2/k C 1 D 0 p .n C 2/2 4.n kD 2.n 1/ p n C 2 ˙ n2 C 8 D : 2.n 1/ .n

.2n/Š

k/.n C 1/.1 C k/n .1 C k/nC1 .1 k 2 .1 k/2 2 k /.n C 1/ .1 C k/.1 2k/ D 0

k 2 .n C 1/

42. We have

22n .nŠ/2



Therefore, s D

22nC2 ..n C 1/Š/2 .2n/Š 4.n C 1/2  2n D lim D 1: 2 .2n C 2/Š 2 .nŠ/ .2n C 2/.2n C 1/

1 X

nD0

nD0

1

P Thus 1 nD1 an converges by the ratio test. (Remark: the question contained a typo. It was intended to ask that #33 be repeated, using the ratio test. That is a little harder.)

Therefore

 N  N X 1 X 1Ck n n < 2n k 2

N 1 1 r N C1 1 X n ; r D  D k k 1 r nD0 where r D .1 C k/=n. Thus

anC1 nn 2nC2  nC1 D nC1 an .n C 1/ 2 1 2 2  D  n D  n C 1 n 1 n .n C 1/ 1C nC1 n 1 ! 0  D 0 as n ! 1: e

 D lim

a) If n is a positive integer and k > 0, then 1 .1 C k/n  1 C nk > nk, so n < .1 C k/n . k

If s D

1 X

kD1

ck D

1 X

kD1

1 , then we have k 2 .k C 1/

sn C AnC1  s  sn C An

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2k/

D0

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INSTRUCTOR’S SOLUTIONS MANUAL

where sn D An D

Z

1

n

n X

kD1

SECTION 9.4 (PAGE 531)

1 and C 1/

(b) Let Sn D

k 2 .k

dx D x 2 .x C 1/

Z

1 n



ˇ1 ˇ 1 ˇ C ln.x C 1/ˇ D ln x ˇ x n ˇ1   ˇ 1 1ˇ D ln 1 C ˇ x xˇ  n 1 1 D ln 1 C : n n

1 1 1 C 2 C x x xC1



dx

0
1;000: 2 1;000

2n C 1 2n 1 < n; 2n .2n C 1/ 4

1 X 1 1 D 2n C 1 2n

if n D 8. Thus,

sn D

1 . Since 2n C 1

provided 4n > 1;000=3. Thus n D 5 will P do (but n D 4 is insufficient). S5 approximates 1 nD1 bn to within 0:001. P n (c) Since 1 nD1 1=2 D 1, we have

An

1 X 1 1 D 1 C s8 D 1 C s8 C .A9 C A8 / n2 2 nD1   1 1 1 1 C 2 C 2 C  C 2 C D1C 2 2 .3/ 3 .4/ 8 .9/ "   # 1 1 10 1 9 ln C ln 2 9 9 8 8

1 2n

Sn D bnC1 C bnC2 C bnC3 C   
a1 2 a3 2 > a2 3

where P4 is the 4th degree Taylor polynomial for f .x/ about x D =2, satisfies jerrorj 



The required Fourier series is, therefore,

Observe that 1:5 < =2  1:5708, that csc x  1 and cot x  0, and that both functions are decreasing on that interval. Thus jf .5/ .x/j  24 csc4 .1:5/ cot.1:5/  2

Z

Z  a0 1 D f .t / dt 2 2  Z 0  Z   1 1 dt C t dt D C D 2 2 4  0  Z 0 Z  1 t cos.nt / dt cos.nt / dt C an D  0 Z  1  D .1 C t / cos.nt / dt  0  n . 1/ 1 2=. n2 / if n is odd D D  n2 0 if n is even Z 0  Z  1 bn D sin.nt / dt C t sin.nt / dt  0 Z  1  .t 1/ sin.nt / dt D  0  1 C . 1/n . 1/ . 2=. n/ if n is odd D D .1=n/ if n is even. n

The series satisfies the conditions of the alternating series test, so if we truncate after the term for n D k 1, then the error will satisfy

Z

2 

t on Œ0;  has

nD1

. 1/n : 4nC1 2 .4n C 1/nŠ

jerrorj 

The Fourier sine series of f .t / D  coefficients

) )

a1 2 2a2 a1 a3 > > 3 3 a2 >

:: :

: n 1 an > an 1 n

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)

an >

a1 : n

387

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CHALLENGING PROBLEMS 9 (PAGE 567)

ADAMS and ESSEX: CALCULUS 9

If x ¤ m for any integer m, then sin.x=2/ ¤ 0. Using the addition formulas we obtain   i 1h  sin.nx/ sin.x=2/ D cos .n C 21 /x : cos .n 12 /x 2 Therefore, using the telescoping property of these terms, h    i N N cos .n 12 /x cos .n C 21 /x X X sin.nx/ D 2 sin.x=2/ nD1 nD1   cos.x=2/ cos .N C 21 /x D : 2 sin.x=2/ P Therefore, the partial sums of 1 nD1 sin.nx/ are bounded. Since the sequence f1=ng is positive, decreasing, and has P sin.nx/=n limit 0, part (b) of Problem 2 shows that 1 nD1 converges in this case too. Therefore the series converges for all x.

(This can be P verified by induction.) Therefore 1 nD1 an diverges by comparison with the harP 1 monic series 1 nD1 . n P 2. a) If sn D nkD1 vk for n  1, and s0 D 0, then vk D sk sk 1 for k  1, and n X

kD1

uk vk D

n X

n X

uk sk

uk sk

1:

kD1

kD1

In the second sum on the right replace k with k C 1: n X

kD1

uk vk D D

n X

uk sk

kD1 n X

n X1

ukC1 sk

kD0

.uk

ukC1 /sk

kD1

D unC1 sn C

n X

.uk

u1 s0 C unC1 sn

4.

ukC1 /sk :

kD1

b) If fun g is positive and decreasing, and limn!1 un D 0, then n X

ukC1 / D u1

.uk

kD1

Thus

D u1 n X

u2 C u2

u3 C    C un

ukC1 / is a convergent, positive, tele-

.uk

scoping series. If the partial sums sn of fvn g are bounded, say jsn j  K for all n, then j.un

unC1 /sn j  K.un

uk vk D lim

n!1

D

1 X

.uk

unC1 sn C

n X

.uk

kD1

ukC1 /sk

!

ukC1 /sk

f .x/ dx

k 1=2 1 2;k

f .k/ D C 12 .

3 2

1 2



f 00 .u/ D f 00 .u/

for some u in Œk C 12 ; k C 23 . Similarly,    1 C 23 f 00 .v/ D f 00 .v/ f 0 k 32 D f 0 k 12 2

f0

for some v in Œk 32 ; k 12 . Since f 00 is decreasing and v  c  u, we have f 00 .u/  f 00 .c/  f 00 .v/, and so    k C 23 f 0 k C 12  f 00 .c/  f 0 k 12 f0 k

b) If f 00 is decreasing, 0

R1

1 NC2

f .x/ dx converges, and

f .x/ ! 0 as x ! 1, then Z 1 1 X f .x/ dx f .n/ 1 nDN C1

kD1

f 00 .c/ , for some c in the 24

a) By the Mean-Value Theorem,   f 0 k C 23 f 0 k C 21 D

D

converges. 3. If x DPm for some integer m, then all the terms of the series 1 nD1 .1=n/ sin.nx/ are 0, so the series converges to 0.

388

mD1

kC1=2

unC1 /;

P unC1 /sn is absolutely convergent (and so 1 nD1 .un therefore convergent) by the comparison test. Therefore, by part (a),

kD1

5.

Z

interval Œk

kD1

1 X

nD1

unC1

unC1 ! u1 as n ! 1.

Let an be the nth integer that has no zeros in its decimal representation. The number of such integers that have m digits is 9m . (There are nine possible choices for each of the m digits.) Also, each such m-digit number is greater than 10m 1 (the smallest m-digit number). Therefore the sum of all the terms 1=an for which an has m digits is less than 9m =.10m 1 /. Therefore,  1 1  X X 1 9 m 1 D 90: 2k. If k  i  2k, the only term in the sum for f .i/ .0/ that is not zero is the term for which j D i k. This term is the constant

390



k i

k



mk

iŠ j . n/j : 0Š

.k C 2/IkC1 :

1=t

dt D I0 D x 2 e 1=x 2I1   D x 2 e 1=x 2 x 3 e 1=x 3I2   D e 1=x Œx 2 2Šx 3  C 3Š x 4 e 1=x 4I3  D e 1=x Œx 2 2Šx 3 C 3Šx 4  4Š x 5 e 1=x e

5I4

:: :

N X

1=x

. 1/n .n

nD2

C . 1/N C1 N Š

j Ck i

 .j C k/.j C k 1/    .j C k i C 1/x k   .j C k/Š 1 X k mk j . n/j x j Ck i : D j kŠ .j C k i /Š

1=x

0

. n/j

j D0

1 kŠ

x

De j

dt

Therefore, Z

1  k mk < : kŠ 2

f .x/ sin x dx
1, z < 2. S is neither open nor closed.

39.

S D f.x; y; z/ W .x z/2 C .y z/2 D 0g The boundary of S is S, that is, the line x D y D z. The interior of S is empty. S is closed.

40.

S D f.x; y; z/ W x 2 C y 2 < 1; y C z > 2g Boundary: the part of the cylinder x 2 C y 2 D 1 that lies on or above the plane y C z D 2 together with the part of that plane that lies inside the cylinder. Interior: all points that are inside the cylinder x 2 C y 2 D 1 and above the plane y C z D 2. S is open.



x2 C y2 C z2  1 p represents all points which are inx2 C y2  z side or on the sphere of radius 1 centred at the origin and which are also inside or on the upper half of the circular cone with axis along the z-axis, vertex at the origin, and semi-vertical angle 45ı . z

p

zD

(PAGE 583)

x 2 Cy 2

y

Section 10.2 Vectors

x x 2 Cy 2 Cz 2 D1

1.

Fig. 10.1-32

34. S D f.x; y/ W x  0; y < 0g The boundary of S consists of points .x; 0/ where x  0, and points .0; y/ where y  0. The interior of S consists of all points of S that are not on the y-axis, that is, all points .x; y/ satisfying x > 0 and y < 0. S is neither open nor closed; it contains some, but not all, of its boundary points. S is not bounded; .x; 1/ belongs to S for 0 < x < 1.

A D . 1; 2/; B D .2; 0/; C D .1; 3/; D D .0; 4/. ! ! (a) AB D 3i 2j (b) BA D 3i C 2j ! (c) AC D 2i

33. S D f.x; y/ W 0 < x 2 C y 2 < 1g The boundary of S consists of the origin and all points on the circle x 2 C y 2 D 1. The interior of S is S, which is therefore open. S is bounded; all points in it are at distance less than 1 from the origin.

(page 583)

5j

! (d) BD D

2i C 4j

! ! ! (e) DA D i 2j (f) AB BC D 4i C j ! ! ! (g) AC 2AB C 3CD D 7i C 20j  5 1 ! ! ! j AB C AC C AD D 2i (h) 3 3 2.

uDi j v D j C 2k a)

u C v D i C 2k u v D i 2j 2k 2u 3v D 2i 5j 6k

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395

lOMoARcPSD|6566483

SECTION 10.2 (PAGE 583)

b) juj D jvj D

p

p

1C1D 1C4D

p p

ADAMS and ESSEX: CALCULUS 9

Thus MN is parallel to and half as long as BC .

2

C

5

1 c) uO D p .i j/ 2 1 vO D p .j C 2k/ 5 d) u  v D 0 1 C 0 D

N

1

A

e) The angle between u and v is 1 cos 1 p  108:4ı . 10 f) The scalar projection of u in the direction of v is 1 uv D p . jvj 5

g) The vector projection of v along u is .v  u/u 1 D .i j/. juj2 2 3.

u D 3i C 4j v D 3i 4j

6.

We have ! ! ! ! ! ! PQ D PB C BQ D 21 AB C 12 BC D 21 AC I ! ! ! ! ! ! SR D SD C DR D 12 AD C 12 DC D 21 AC : ! ! Therefore, PQ D SR. Similarly,

u C v D 6i 10k u v D 8j 2u 3v D 3i C 20j C 5k p p b) juj D 9 C 16 C 25 D 5 2 p p jvj D 9 C 16 C 25 D 5 2 a)

! ! ! ! QR D QC C CR D 12 BDI ! ! ! ! PS D PA C AS D 21 BD: ! ! Therefore, QR D PS . Hence, PQRS is a parallelogram.

1 c) uO D p .3i C 4j 5k/ 5 2 1 vO D p .3i 4j 5k/ 5 2 d) u  v D 9 16 C 25 D 18

B

g) The vector projection of v along u is 9 .v  u/u D .3i C 4j 5k/. juj2 25

4. If a D . 1; 1/, B D .2; 5/ and C D .10; 1/, then ! ! ! ! AB D 3i C 4j and BC D 8i 6j. Since AB  BC D 0, ! ! therefore, AB ? BC . Hence, 4ABC has a right angle at B.

A

! AB 2

D

! BC : 2

C

R

S

D

Fig. 10.2-6

7.

Let the parallelogram be ABCO. Take the origin at O. The position vector of the midpoint of OB is ! ! ! ! ! OB C CB OC C OA OB D D : 2 2 2 The position vector of the midpoint of CA is ! ! ! ! CA ! OA OC D OC C OC C 2 2 ! ! OC C OA : D 2

5. Let the triangle be ABC . If M and N are the midpoints ! ! of AB and AC respectively, then AM D 12 AB, and ! ! AN D 12 AC . Thus

396

Q

P

e) The angle between u and v is 18  68:9ı . cos 1 50 f) The scalar projection of u in the direction of v is uv 18 D p . jvj 5 2

! AC ! AM D

B

Fig. 10.2-5

5k 5k

! ! MN D AN

M

Thus the midpoints of the two diagonals coincide, and the diagonals bisect each other.

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 10.2

9. B

C

(PAGE 583)

Let i point east and j point north. Let the wind velocity be vwind D ai C bj: Now vwind D vwind rel car C vcar . When vcar D 50j, the wind appears to come from the west, so vwind rel car D i. Thus ai C bj D i C 50j;

A

O

Fig. 10.2-7 8. Let X be the point of intersection of the medians AQ and BP as shown. We must show that CX meets AB in the ! ! ! ! midpoint of AB. Note that PX D ˛ PB and QX D ˇ QA for certain real numbers ˛ and ˇ. Then   1 ! 1 ! 1 ! ! ! ! CX D CB C ˇ QA D CB C ˇ CB C BA 2 2 2 1Cˇ ! ! D CB C ˇ BAI 2   1 ! 1 ! 1 ! ! ! ! CX D CA C ˛ PB D CA C ˛ CA C AB 2 2 2 1C˛ ! ! CA C ˛ AB: D 2

so a D  and b D 50. When vcar D 100j, the wind appears to come from the northwest, so vwind rel car D .i-j). Thus ai C bj D .i

so a D  and b D 100 . Hence 50 D 100 , so  D 50.pThus a D b D 50. The wind is from the southwest at 50 2 km/h. 10. Let the x-axis point east and the y-axis north. The velocity of the water is vwater D 3i: If you row through the water with speed 5 in the direction making angle  west of north, then your velocity relative to the water will be vboat

Thus, 1Cˇ ! 1C˛ ! ! ! CB C ˇ BA D CA C ˛ AB 2 2 1C˛ ! 1Cˇ ! ! .ˇ C ˛/BA D CA CB 2 2 1C˛ ! 1Cˇ ! ! ! .ˇ C ˛/.CA CB/ D CA CB 2  2   1Cˇ ! 1C˛ ! CA D ˇ C ˛ CB: ˇC˛ 2 2 ! ! Since CA is not parallel to CB, 1C˛ DˇC˛ 2 1 )˛DˇD : 3

ˇC˛

1Cˇ D0 2

j/ C 100j;

rel water

D

5 sin  i C 5 cos  j:

Therefore, your velocity relative to the land will be vboat

rel land

D vboat rel water C vwater D .3 5 sin  /i C 5 cos  j:

To make progress in the direction j, choose  so that 3 D 5 sin  . Thus  D sin 1 .3=5/  36:87ı . In this case, your actual speed relative to the land will be 4 5 cos  D  5 D 4 km/h. 5 To row from A to B, head in the direction 36:87ı west of north. The 1=2 km crossing will take .1=2/=4 D 1=8 of an hour, or about 7 12 minutes. B

Since ˛ D ˇ, x divides AQ and BP in the same ratio. By symmetry, the third median CM must also divide the other two in this ratio, and so must pass through X and MX D 31 M C .

vboat

rel water

A  M

vwater

P

X

B

j i A

Q

C

Fig. 10.2-10

Fig. 10.2-8

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SECTION 10.2 (PAGE 583)

11.

ADAMS and ESSEX: CALCULUS 9

If this velocity is true easterly, then

We use the notations of the solution to Exercise 4. You 1 now want to make progress in the direction ki C j, that 2 is, in the direction making angle  D tan

1

100 750 sin  D p ; 2

1 2k

so   5:41ı . The speed relative to the ground is

with vector i. Head at angle  upstream of this direction. Since your rowing speed is 2, the triangle with angles  and  has sides 2 and 3 as shown in the figure. By the 3 2 Sine Law, D , so sin  sin 

100 p  675:9 km/h: 2

750 cos 

The time for the 1500 km trip is

1500  2:22 hours. 675:9

y

3 1 3 sin  D sin  D q 2 2 2 k2 C

3

1 4

: D p 2 4k 2 C 1

3 This is only possible if p  1, that is, if 2 4k 2 C 1 p 5 . k 4 3 Head in the direction  D sin 1 p upstream of 2 4k 2 C 1 the direction of AC p , as shown in the figure. The trip is not possible if k < 5=4. B

750  x 100

C

k

Fig. 10.2-12



13. 3

2

1 2

The two vectors are perpendicular if their dot product is zero: .2t i C 4j .10 C t /k/  .i C t j C k/ D 0 2t C 4t 10 t D 0 ) t D 2:



3i

The vectors are perpendicular if t D 2. 14.



A Fig. 10.2-11

The cube with edges i, j, and k has diagonal iCjCk. The angle between i and the diagonal is cos

1

12. Let i point east and j point north. If the aircraft heads in a direction  north of east, then its velocity relative to the air is 750 cos  i C 750 sin  j:

i  .i C j C k/ p D cos 3

1

1 p  54:7ı : 3

z

The velocity of the air relative to the ground is 100 p iC 2

100 p j: 2



Thus the velocity of the aircraft relative to the ground is  750 cos 

398

  100 p i C 750 sin  2

 100 p j: 2

x

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iCjCk y

i

Fig. 10.2-14

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

15.

SECTION 10.2

The cube of Exercise 10 has six faces, each with 2 diagonals. The angle between i C j C k and the face diagonal i C j is cos

1

.i C j/  .i C j C k/ D cos p p 2 3

1

2 p  35:26ı : 6

20.

If a ¤ 0, then a  r D 0 implies that the position vector r is perpenducular to a. Thus the equation is satisfied by all points on the plane through the origin that is normal (perpendicular) to a.

21.

If r  a D b, then the vector projection of r along a is the constant vector ra a b D 2 a D r0 ; say. jaj jaj jaj

Six of the face diagonals make this angle with i C j C k. The face diagonal i j (and five others) make angle cos

1

j/  .i C j C k/ D cos p p 2 3

.i

1

0 D 90

Thus r  a D b is satisfied by all points on the plane through r0 that is normal to a.

ı

with the cube diagonal i C j C k.

In Exercises 22–24, u D 2i C j w D 2i 2j C k. 22.

ui u1 16. If u D u1 i C u2 j C u3 k, then cos ˛ D . juj juj u3 u2 and cos D . Similarly, cos ˇ D juj juj Thus, the unit vector in the direction of u is uO D

u D cos ˛i C cos ˇj C cos k; juj

If uO makes equal angles ˛ D ˇ D with p the coordinate axes, then 3 cos2 ˛ D 1, and cos ˛ D 1= 3. Thus uO D

23.

1

†BCA D cos

1

†CAB D cos

1

! ! BA  BC D cos jBAjjBC j ! ! CB  CA D cos jCBjjCAj ! ! AC  AB D cos jAC jjABj

Let x D xi C yj C zk. Then xuD9 xvD4 xw D 6

4 p p  60:26ı 5 13 9 1 p p  37:87ı 10 13 1 1 p p  81:87ı : 10 5

, , ,

2x C y 2z D 9 x C 2y 2z D 4 2x 2y C z D 6:

This system of linear equations has solution x D 2, y D 3, z D 4. Thus x D 2i 3j 4k. 24.

1

19. Since r r1 D r1 C .1 /r2 r1 D .1 /.r1 r2 /, therefore r r1 is parallel to r1 r2 , that is, parallel to the line P1 P2 . Since P1 is on that line, so must P be on it. 1 1 If  D , then r D .r1 C r2 /, so P is midway between 2 2 P1 and P2 . 2 1 2 If  D , then r D r1 C r2 , so P is two-thirds of the 3 3 3 way from P2 towards P1 along the line. If  D 1, the r D r1 C 2r2 D r2 C .r2 r1 /, so P is such that P2 bisects the segment P1 P . If  D 2, then r D 2r1 r2 D r1 C .r1 r2 /, so P is such that P1 bisects the segment P2 P .

2k, and

Vector x D xi C yj C zk is perpendicular to both u and v if u  x D 0 , 2x C y 2z D 0 v  x D 0 , x C 2y 2z D 0:

iCjCk : p 3

18. If A D .1; 0; 0/, B D .0; 2; 0/, and C D .0; 0; 3/, then †ABC D cos

2k, v D i C 2j

Subtracting these equations, we get x y D 0, so x D y. The first equation now gives 3x D 2z. Now x is a unit vector if x 2 C y 2 C z 2 D 1, that is, if x 2 C x 2 C 49 x 2 D 1, p or x D ˙2= 17. The two unit vectors are   2 3 2 xD˙ p iC p jC p k : 17 17 17

O 2 D 1. and so cos2 ˛ C cos2 ˇ C cos2 D juj 17.

(PAGE 583)

Since u, v, and w all have the same length (3), a vector x D xi C yj C zk will make equal angles with all three if it has equal dot products with all three, that is, if 2x C y 2x C y

2z D x C 2y 2z 2z D 2x 2y C z

, ,

xDyD0 3y 3z D 0:

Thus x D y D z. Two unit vectors satisfying this condition are   1 1 1 xD˙ p iC p jC p k : 3 3 3 25.

Let uO D u=juj and vO D v=jvj. Then uO C vO bisects the angle between u and v. A unit vector which bisects this angle is u v C uO C vO juj jvj ˇ D ˇ ˇ u v ˇˇ juO C vO j ˇ C ˇ juj jvj ˇ jvju C jujv ˇ: D ˇ ˇ ˇ ˇjvju C jujvˇ

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SECTION 10.2 (PAGE 583)

ADAMS and ESSEX: CALCULUS 9

Similarly, r  v D b and r  w D c.

u uO

31. uO C vO

vO

Let u D vDw and

v

wa a, (the vector projection of w along a). Let jaj2 u. Then w D u C v. Clearly u is parallel to a, wa aaDwa jaj2

vaDwa

Fig. 10.2-25

w  a D 0;

so v is perpendicular to a. 26. If u and v are not parallel, then neither is the zero vector, and the origin and the two points with position vectors u and v lie on a unique plane. The equation r D u C v (;  real) gives the position vector of an arbitrary point on that plane. 27.

w v

a

2

a) ju C vj D .u C v/  .u C v/ DuuCuvCvuCvv

u

D juj2 C 2u  v C jvj2 :

Fig. 10.2-31

b) If  is the angle between u and v, then cos   1, so u  v D jujjvj cos   jujjvj:

32.

c) ju C vj2 D juj2 C 2u  v C jvj2

 juj2 C 2jujjvj C jvj2

Let nO be a unit vector that is perpendicular to u and lies in the plane containing the origin and the points U , V , and P . Then uO D u=juj and nO constitute a standard basis in that plane, so each of the vectors v and r can be expressed in terms of them:

D .juj C jvj/2 : Thus ju C vj  juj C jvj. 28.

v D s uO C t nO O r D x uO C y n:

a) u, v, and u C v are the sides of a triangle. The triangle inequality says that the length of one side cannot exceed the sum of the lengths of the other two sides.

Since v is not parallel to u, we have t ¤ 0. Thus O and nO D .1=t /.v s u/

b) If u and v are parallel and point in the same direction, (or if at least one of them is the zero vector), then ju C vj D juj C jvj.

29. u D 53 i C 45 j, v D 54 i 35 j, w D k. q q 9 16 a) juj D 25 C 16 D 1, jvj D 25 25 C uv D

12 25

12 25

9 25

D 1, jwj D 1,

D 0, u  w D 0, v  w D 0.

r D x uO C where  D .tx 33.

Let jaj2

30. Suppose juj D jvj D jwj D 1, and uv D uw D vw D 0, and let r D au C bv C ww. Then

ys/=.t juj/ and  D y=t .

4rst D K 2 , where K > 0. Now D r 2 jxj2 C s 2 jyj2 C 2rsx  y

K 2 D jaj2 D jrx

4rsx  y

syj2

(since x  y D t ). O for some unit vector u. O Therefore rx sy D K u, Since rx C sy D a, we have 2rx D a C K uO O 2sy D a K u: Thus

r  u D au  u C bv  u C cw  u D ajuj2 C 0 C 0 D a:

400

O D u C v; s u/

jaj2 D a  a D .rx C sy/  .rx C sy/

b) If r D xi C yj C zk, then .r  u/u C .r  v/v C .r  w/w    4 3 4 3 xC y iC j D 5 5 5 5    4 4 3 3 C x y i j C zk 5 5 5 5 16y C 9y 9x C 16x iC j C zk D 25 25 D xi C yj C zk D r:

y .v t

xD

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a C K uO ; 2r

yD

a

K uO ; 2s

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 10.3

p where K D jaj2 4rst, and uO is any unit vector. (The solution is not unique.)

(PAGE 592)

The length of the cable between x D 0 and x D 10 m is Z 10 q LD 1 C sinh2 .ax/ dx 0 ˇ10 Z 10 ˇ 1 ˇ D cosh.ax/ dx D sinh.ax/ˇ ˇ a 0

34. The derivation of the equation of the hanging cable given in the text needs to be modified by replacing W D ıgsj with W D ıgxj. Thus Tv D ıgx, and the slope of the cable satisfies dy ıgx D D ax dx H

0

1 D sinh.10a/  12:371 m: a

where a D ıg=H . Thus yD

1 2 ax C C I 2

Section 10.3 The Cross Product in 3-Space (page 592)

the cable hangs in a parabola. 1 35. If y D cosh.ax/, then y 0 D sinh.ax/, so a Z

Z x q sD 1 C sinh2 .au/ du D cosh.au/ du 0 0 ˇx sinh.au/ ˇˇ 1 D ˇ D sinh.ax/: ˇ a a

2.

.j C 2k/  . i

3.

If A D .1; 2; 0/, B D .1; 0; 2/, and C D .0; 3; 1/, then ! ! AB D 2j C 2k, AC D i C j C k, and the area of triangle ABC is

jTj D

50 D

45

0

1 cosh.45a/ a

 1  19:07 m:

1 cosh.ax/. a At the point P where x D 10 m, the slope of the cable is sinh.10a/ D tan.55ı /. Thus

37. The equation of the cable is of the form y D

1 sinh 10

1

4i

2j C k

2j 2

2kj

D

p

6 sq. units.

A vector perpendicular to the plane containing the three given points is . ai C bj/  . ai C ck/ D bci C acj C abk: A unit vector in this direction is p

bci C acj C abk

b 2 c 2 C a2 c 2 C a2 b 2

:

1p 2 2 b c C a2 c 2 C a2 b 2 . 2 A vector perpendicular to i C j and j C 2k is

The triangle has area 5.

˙.i C j/  .j C 2k/ D ˙.2i

q 1 1 C sinh2 .ax/ dx D sinh.45a/: a

The equation sinh.45a/ D 50a has approximate solution a  0:0178541. The vertical distance between the lowest point on the cable and the support point is

aD

4.

ıg cosh.ax/ D ıgy: Th2 C Tv2 D a

1 36. The cable hangs along the curve y D cosh.ax/, and its a length from the lowest point at x D 0 to the support tower at x D 45 m is 50 m. Thus Z

j C k/ D 3i

! ! j jAB  AC j D 2

0

q

4k/ D 5i C 13j C 7k

.i

x

As shown in the text, the tension T at P has horizontal ıg and vertical components that satisfy Th D H D and a ıg Tv D ıgs D sinh.ax/. Hence a

2j C 3k/  .3i C j

1.

2j C k/;

which has length 3. A unit vector in that direction is   2 2 1 ˙ i jC k : 3 3 3 6.

A vector perpendicular to u D 2i j 2k and to v D 2i 3j C k is the cross product ˇ ˇ ˇi j k ˇˇ ˇ 1 2 ˇˇ D 7i 6j 4k; u  v D ˇˇ 2 ˇ2 3 1 ˇ

p which has length 101. A unit vector with positive k component that is perpenducular to u and v is

.tan.55ı /  0:115423:

p

1 101

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uv D p

1 101

.7i C 6j C 4k/:

401

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SECTION 10.3 (PAGE 592)

ADAMS and ESSEX: CALCULUS 9

Since u makes zero angle with itself, ju  uj D 0 and u  u D 0. ˇ ˇ ˇ i j k ˇˇ ˇ 8. u  v D ˇˇ u1 u2 u3 ˇˇ ˇ v1 v2 v3 ˇ ˇ ˇ ˇ i j k ˇˇ ˇ D ˇˇ v1 v2 v3 ˇˇ D v  u: ˇ u1 u2 u3 ˇ 7.

9.

10.

Thus u  v C w  v D 0. Thus u  v D w  v D v  w. By symmetry, we also have v  w D w  u. 14.

The base of the tetrahedron is a triangle spanned by v and w, which has area AD

hD

ˇ ˇ u1 u2 ˇˇ v1

ˇ ˇ ˇ u1 u3 ˇˇ ˇ C u 3 ˇ v1 v3 ˇ

D u1 u2 v3 u1 v2 u3 u2 u1 v3 C u2 v1 u3 C u3 u1 v2 u3 v1 u2 D 0; v  .u  v/ D v  .v  u/ D 0:

V D

u h h

ˇ k ˇˇ 0 ˇˇ D .sin ˛ cos ˇ 0ˇ

Fig. 10.3-14 15.

cos ˛ sin ˇ/k:

Because v is displaced counterclockwise from u, the cross product above must be in the positive k direction. Therefore its length is the k component. Therefore sin.˛

ˇ/ D sin ˛ cos ˇ

cos ˛ sin ˇ:

w

v

But j sin ˇ sin ˛

1 1 Ah D ju  .v  w/j 3 6 ˇ ˇ ˇu u2 u3 ˇˇ 1 ˇˇ 1 D j ˇ v1 v2 v3 ˇˇ j: 6 ˇw w w ˇ 1 2 3 uv

ˇ u2 ˇˇ v2 ˇ

12. Both u D cos ˇ i C sin ˇ j and v D cos ˛ i C sin ˛ j are unit vectors. They make angles ˇ and ˛, respectively, with the positive x-axis, so the angle between them is j˛ ˇj D ˛ ˇ, since we are told that 0  ˛ ˇ  . They span a parallelogram (actually a rhombus) having area ju  vj D jujjvj sin.˛ ˇ/ D sin.˛ ˇ/: ˇ ˇ i ˇ u  v D ˇˇ cos ˇ ˇ cos ˛

ju  .v  w/j : jv  wj

The volume of the tetrahedron is

.t v/  u t .v  u/ D t .u  v/:

u  .u  v/ ˇ ˇ ˇ u2 u3 ˇ ˇ D u1 ˇˇ v2 v3 ˇ

1 jv  wj: 2

The altitude h of the tetrahedron (measured perpendicular to the plane of the base) is equal to the length of the projection of u onto the vector v  w (which is perpendicular to the base). Thus

D u  w C v  w: ˇ ˇ ˇ i j k ˇˇ ˇ .t u/  v D ˇˇ t u1 t u2 t u3 ˇˇ ˇ v1 v2 v3 ˇ ˇ ˇ ˇ i j k ˇˇ ˇ D t ˇˇ u1 u2 u3 ˇˇ D t .u  v/; ˇ v1 v2 v3 ˇ

402

Suppose that u C v C w D 0. Then u  v C v  v C w  v D 0  v D 0:

ˇ ˇ ˇ ˇ i j k ˇ ˇ .u C v/  w D ˇˇ u1 C v1 u2 C v2 u3 C v3 ˇˇ ˇ w1 w2 w3 ˇ ˇ ˇ ˇ ˇ ˇ i j k ˇˇ ˇˇ i j k ˇˇ ˇ D ˇˇ u1 u2 u3 ˇˇ C ˇˇ v1 v2 v3 ˇˇ ˇ w1 w2 w3 ˇ ˇ w1 w2 w3 ˇ

u  .t v/ D D 11.

13.

16.

The tetrahedron with vertices .1; 0; 0/, .1; 2; 0/, .2; 2; 2/, and .0; 3; 2/ is spanned by u D 2j, v D i C 2j C 2k, and w D i C 3j C 2k. By Exercise 14, its volume is ˇ ˇ ˇ 0 2 0ˇ ˇ 4 1 ˇˇ V D j ˇ 1 2 2 ˇˇ j D cu. units. 6 ˇ 1 3 2ˇ 3

Let the cube be as shown in the figure. The required parallelepiped is spanned by ai C aj, aj C ak, and ai C ak. Its volume is ˇ ˇ ˇa a 0ˇ ˇ ˇ V D j ˇˇ 0 a a ˇˇ j D 2a3 cu. units. ˇa 0 aˇ

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lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 10.3

(PAGE 592)

z

20. .0;a;a/

If v  w ¤ 0, then .v  w/  .v  w/ ¤ 0. By the previous exercise, there exist constants ,  and  such that

.a;0;a/

u D v C w C .v  w/: But v  w is perpendicular to both v and w, so u  .v  w/ D 0 C 0 C .v  w/  .v  w/: If u  .v  w/ D 0, then  D 0, and

y x

u D v C w:

.a;a;0/

Fig. 10.3-16 17.

The points A D .1; 1; 1/, B D .0; 3; 2/, C D . 2; 1; 0/, ! ! ! and D D .k; 0; 2/ are coplanar if .AB  AC /  AD D 0. Now ˇ ˇ i j ! ! ˇˇ 1 2 AB  AC D ˇ ˇ 3 0

ˇ k ˇˇ 1 ˇˇ D 2i C 4j C 6k: 1 ˇ

Thus the four points are coplanar if 2.k that is, if k D 18.

1/ C 4.0

21.

u D i C 2j C 3k v D 2i 3j wDj k u  .v  w/ D u  .3i C 2j C 2k/ D 2i C 7j 4k .u  v/  w D .9i C 6j 7k/  w D i C 9j C 9k: u  .v  w/ lies in the plane of v and w; .u  v/  w lies in the plane of u and v.

22.

u  v  w makes sense in that it must mean u  .v  w/. (.u  v/  w makes no sense since it is the cross product of a scalar and a vector.)

1/ C 6.2 C 1/ D 0;

uvw makes no sense. It is ambiguous, since .uv/w and u  .v  w/ are not in general equal.

6. 23.

ˇ ˇ ˇ u1 u2 u3 ˇ ˇ ˇ u  .v  w/ D ˇˇ v1 v2 v3 ˇˇ ˇ w1 w2 w3 ˇ ˇ ˇ ˇ v1 v2 v3 ˇ ˇ ˇ D ˇˇ u1 u2 u3 ˇˇ ˇ w1 w2 w3 ˇ ˇ ˇ ˇ v1 v2 v3 ˇ ˇ ˇ D ˇˇ w1 w2 w3 ˇˇ ˇ u1 u2 u3 ˇ D v  .w  u/ D w  .u  v/

v D v1 i;

u  .v  w/ D .u1 i C u2 j C u3 k/  .v1 w2 k/ D u1 v1 w2 i  k C u2 v1 w2 j  k D u1 v1 w2 i u1 v1 w2 j: But

.by symmetry/:

x  .v  w/ D u  .v  w/ C v  .v  w/ C w  .v  w/ D u  .v  w/: D

x  .v  w/ : u  .v  w/

Since u  .v  w/ D v  .w  u/ D w  .u  v/, we have, by symmetry, D

x  .w  u/ ; u  .v  w/

D

w D w1 i C w2 j:

Thus v  w D v1 w2 i  j D v1 w2 k, and

.u  w/v .u  v/w D .u1 w1 C u2 w2 /v1 i u1 v1 .w1 i C w2 j/ D u2 v1 w2 i u1 v1 w2 j:

19. If u  .v  w/ ¤ 0, and x D u C v C w, then

Thus

As suggested in the hint, let the x-axis lie in the direction of v, and let the y-axis be such that w lies in the xyplane. Thus

x  .u  v/ : u  .v  w/

Thus u  .v  w/ D .u  w/v

.u  v/w.

24.

If u, v, and w are mutually perpendicular, then v  w is parallel to u, so u  .v  w/ D 0. In this case, u  .v  w/ D ˙jujjvjjwj; the sign depends on whether u and v  w are in the same or opposite directions.

25.

Applying the result of Exercise 23 three times, we obtain u  .v  w/ C v  .w  u/ C w  .u  v/ D .u  w/v .u  v/w C .v  u/w .v  w/u C .w  v/u .w  u/v D 0:

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403

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SECTION 10.3 (PAGE 592)

26. If a D

ADAMS and ESSEX: CALCULUS 9

i C 2j C 3k and x D xi C yj C zk, then

ˇ ˇ i ˇ a  x D ˇˇ 1 ˇ x

ˇ k ˇˇ 3 ˇˇ zˇ

j 2 y

D .2z 3y/i C .3x C z/y D i C 5j 3k;

.y C 2x/k

provided 2z 3y D 1, 3x C z D 5, and This system is satisfied by x D t , y D 3 for any real number t . Thus x D t i C .3

2t /j C .5

y 2x D 2t , z D 5

The plane through the origin having normal i equation x y C 2z D 0.

4.

The plane passing through .1; 2; 3/, parallel to the plane 3x C y 2z D 15, has equation 3z C y 2z D 3 C 2 6, or 3x C y 2z D 1.

5.

The plane through .1; 1; 0/, .2; 0; 2/, and .0; 3; 3/ has normal .i j C 2k/  .i 2j 3k/ D 7i C 5j k: It therefore has equation

3. 3t ,

or 7x C 5y

3t /k

Let a D i C 2j C 3k and b D i C 5j. If x is a solution of a  x D b, then

0/ D 0;

.z

z D 12.

The plane passing through . 2; 0; 0/, .0; 3; 0/, and .0; 0; 4/ has equation y z x C C D 1; 2 3 4 or 6x 4y 3z D 12.

7.

The normal n to a plane through .1; 1; 1/ and .2; 0; 3/ must be perpendicular to the vector i j C 2k joining these points. If the plane is perpendicular to the plane x C 2y 3z D 0, then n must also be perpendicular to i C 2j 3k, the normal to this latter plane. Hence we can use

However, a  b ¤ 0, so there can be no such solution x. 28. The equation a  x D b can be solved for x if and only if a  b D 0. The “only if” part is demonstrated in the previous solution. For the “if” part, observe that if a  b D 0 and x0 D .b  a/=jaj2 , then by Exercise 23,

n D .i

j C 2k/  .i C 2j

3k/ D

i C 5j C 3k:

The plane has equation

.a  a/b .a  b/a 1 a  .b  a/ D D b: 2 jaj jaj2

The solution x0 is not unique; as suggested by the example in Exercise 26, any multiple of a can be added to it and the result will still be a solution. If x D x0 C t a, then

1/

6.

a  b D a  .a  x/ D 0:

a  x0 D

1/ C 5.y

7.x

gives a solution of a  x D i C 5j 3k for any t . These solutions constitute a line parallel to a. 27.

j C 2k has

3.

1/ C 5.y

.x or x 8.

a  x D a  x0 C t a  a D b C 0 D b:

3z D

5y

1/ C 3.z

1/ D 0;

7.

Since . 2; 0; 1/ does not lie on x 4y C 2z D required plane will have an equation of the form 2x C 3y

z C .x

5, the

4y C 2z C 5/ D 0

for some . Thus

Section 10.4 Planes and Lines 1.

(page 599)

4 C 1 C . 2

a) x 2 Cy 2 Cz 2 D z 2 represents a line in 3-space, namely the z-axis. b) x C y C z D x C y C z is satisfied by every point in 3-space. c) x 2 C y 2 C z 2 D 3-space.

4.x or 4x

404

y

0/

so  D 3. The required plane is 5x 9.

.y

2/

j

2k has

xCy

2 C .y

15.

z

3/ D 0:

This plane will be perpendicular to 2x C 3y C 4z D 5 if .2/.1/ C .1 C /.3/

2.z C 3/ D 0;

9y C 5z D

A plane through the line x Cy D 2, y z D 3 has equation of the form

1 is satisfied by no points in (real)

2. The plane through .0; 2; 3/ normal to 4i equation

2 C 5/ D 0;

./.4/ D 0;

that is, if  D 5. The equation of the required plane is x C 6y

2z D 4.

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5z D 17:

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 10.4

10. Three distinct points will not determine a unique plane through them if they all lie on a straight line. If the points have position vectors r1 , r2 , and r3 , then they will all lie on a straight line if r1 /  .r3

.r2 11.

r1 / D 0:

or in standard form y z 1 xC1 D D : 2 1 7 17.

h r1 /  .r3

.i C 2j

(or if they satisfy any similar such condition that asserts that the tetrahedron whose vertices they are has zero volume).

14.

The distance from the planes x C

p

p

r D .1 C 2t /i C .2

3t /j C .3

6j

5k:

(vector parametric) (scalar parametric)

5t

(standard form).

j C 2k/ D 2.i

j

k/:

Since the line passes through .2; 1; 1/, its equations are, in vector parametric form r D .2 C t /i

4k has

.1 C t /j

.1 C t /k;

or in scalar parametric form

4t /k;

x D 2 C t;

or in scalar parametric form by x D 1 C 2t;

zD

.i C j/  .i

The line through .1; 2; 3/ parallel to 2i 3j equations given in vector parametric form by

j C 4k/ D 7i

18. A line parallel to x C y D 0 and to x y C 2z D 0 is parallel to the cross product of the normal vectors to these two planes, that is, to the vector

to the origin is 1= 2 C 1 2 D 1. Hence the equation represents the family of all vertical planes at distance 1 from the origin. All such planes are tangent to the cylinder x 2 C y 2 D 1. 15.

k/  .2i

r D 7t i 6t j 5t k x D 7t; y D 6t; y z x D D 7 6 5

2 y D 1

1

y C 4z D 5

2x

Since the line passes through the origin, it has equations

12. x C y C z D  is the family of all (parallel) planes normal to the vector i C j C k. 13. x C y C z D  is the family of all planes containing the line of intersection of the planes x D 0 and y C z D 1, except the plane y C z D 1 itself. All these planes pass through the points .0; 1; 0/ and .0; 0; 1/.

z D 2;

is parallel to the vector

i r1 / D 0

r1 /  .r4

A line parallel to the line with equations x C 2y

If the four points have position vectors ri , .1  i  4/, then they are coplanar if, for example, .r2

(PAGE 599)

yD

.1 C t /;

zD

.1 C t /;

or in standard form

yD2

zD3

3t;

4t;

x

2D

.y C 1/ D

.z C 1/:

or in standard form by x

1 2

D

y

2

z

3

19.

3 : 4

16. The line through . 1; 0; 1/ perpendicular to the plane 2x y C 7z D 12 is parallel to the normal vector 2i j C 7k to that plane. The equations of the line are, in vector parametric form, r D . 1 C 2t /i

xD

1 C 2t;

yD

r D .1 C t /i C .2 C t /j C . 1 C t /k (vector parametric) x D 1 C t; y D 2 C t; z D 1 C t (scalar parametric) x 1Dy 2DzC1 (standard form).

t j C .1 C 7t /k; 20.

or in scalar parametric form, t;

A line making equal angles with the positive directions of the coordinate axes is parallel to the vector i C j C k. If the line passes through the point .1; 2; 1/, then it has equations

The line r D .1 form

z D 1 C 7t;

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2t /i C .4 C 3t /j C .9 x

1 2

D

y

4 3

D

z

4t /k has standard 9 : 4

405

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SECTION 10.4 (PAGE 599)

21.

The line

(

x D 4 5t has standard form y D 3t zD7 x

4 5

22. The line .i



ADAMS and ESSEX: CALCULUS 9

D

y ; 3

26.

p

z D 7:

27.

x 2y C 3z D 0 is parallel to the vector 2x C 3y 4z D 4

2j C 3k/  .2i C 3j

4k/ D

2y D 0;

The distance from .1; 2; 0/ to 3x

28.

i C 10j C 7k:

1

8 y 7 D

a D .i C j C k/  .2i

29.

x1 / y1 / z1 /

.r2 .r3

r1 /  .r4 r3 / ¤ 0; and h i r1 /  .r2 r1 /  .r4 r3 / D 0:

1 j: 3



a1 D 4i a2 D 2i

2j C k 3j C k;

we calculate the distance between the two lines by the formula in Section 10.4 as sD D

j.r1 j.2i

r2 /  .a1  a2 /j ja1  a2 j 4j k/  .i 2j ji 2j 8kj

8k/j

18 D p units. 69 30.

y C3 z 1 D passes through the point 2 4 .2; 3; 1/, and is parallel to a D i C 2j C 4k. The plane 2y z D 1 has normal n D 2j k. Since a  n D 0, the line is parallel to the plane. The distance from the line to the plane is equal to the distance from .2; 3; 1/ to the plane 2y z D 1, so is The line x

(Other similar answers are possible.)

406

3k:

x C 2y D 3 contains the points .1; 1; 1/ and y C 2z D 3 1 .3; 0; 3=2/, so is parallel to the vector 2i j C k, or to 2 4i 2j Cnk. xCy Cz D6 The line contains the points . 5; 11; 0/ x 2z D 5 and . 1; 5; 2/, and so is parallel to the vector 4i 6j C 2k, or to 2i 3j C k. Using the values The line

The point on the line corresponding to t D 1 is the point P3 such that P1 is midway between P3 and P2 . The point on the line corresponding to t D 1=2 is the midpoint between P1 and P2 . The point on the line corresponding to t D 2 is the point P4 such that P2 is the midpoint between P1 and P4 .

25. Let ri be the position vector of Pi (1  i  4). The line P1 P2 intersects the line P3 P4 in a unique point if the four points are coplanar, and P1 P2 is not parallel to P3 P4 . It is therefore sufficient that

1 i 3

r1 D i C j C k r2 D i C 5j C 2k

certainly represent a straight line. Since .x; y; z/ D .x1 ; y1 ; z1 / if t D 0, and .x; y; z/ D .x2 ; y2 ; z2 / if t D 1, the line must pass through P1 and P2 . 24.

4i C 7j

The distance from the origin to the line is r jr1  aj ji C j C kj 3 D sD D units. p jaj 74 74

23. The equations

x D x1 C t .x2 ˆ ˆ ˆ y D y1 C t .y2 ˆ ˆ : z D z1 C t .z2

5k/ D

j

r1 D

4 7 D z; 10 7

8 ˆ ˆ ˆ ˆ ˆ
0 are ellipses with semi-axes k and k=2. z

zDx 2 C2y 2

y0 /2 ;

so the given equations specify all straight lines lying on that cone. 33. The equation .A1 x C B1 y C C1 z C D1 /.A2 x C B2 y C C2 z C D2 / D 0 is satisfied if either A1 x C B1 y C C1 z C D1 D 0 or A2 x C B2 y C C2 z C D2 D 0, that is, if .a; y; z/ lies on either of these planes. It is not necessary that the point lie on both planes, so the given equation represents all the points on each of the planes, not just those on the line of intersection of the planes.

Fig. 10.5-5

6.

Section 10.5 Quadric Surfaces 1.

y

x

(page 603)

z D x2

2y 2 represents a hyperbolic paraboloid. z zDx 2 2y 2

x 2 C 4y 2 C 9z 2 D 36

x2 y2 z2 C 2 C 2 D1 2 6 3 2 This is an ellipsoid with centre at the origin and semi-axes 6, 3, and 2. 2. x 2 Cy 2 C4z 2 D 4 represents an oblate spheroid, that is, an ellipsoid with its two longer semi-axes equal. In this case the longer semi-axes have length 2, and the shorter one (in the z direction) has length 1. Cross-sections in planes perpendicular to the z-axis between z D 1 and z D 1 are circles. 3.

2x 2 C 2y 2 C 2z 2

4x C 8y

y x

Fig. 10.5-6

12z C 27 D 0

2.x 2 2x C 1/ C 2.y 2 C 4y C 4/ C 2.z 2 6z C 9/ D 27 C 2 C 8 C 18 1 .x 1/2 C .y C 2/2 C .z 3/2 D 2 p This is a sphere with radius 1= 2 and centre .1; 2; 3/.

7.

x 2 y 2 z 2 D 4 represents a hyperboloid of two sheets with vertices at .˙2; 0; 0/ and circular cross-sections in planes x D k, where jkj > 2.

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407

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SECTION 10.5 (PAGE 603)

ADAMS and ESSEX: CALCULUS 9

z

z x2

y2

z 2 D4 x 2 C4z 2 D4

x

y y

x

Fig. 10.5-10

Fig. 10.5-7 8.

x 2 C y 2 C z 2 D 4 represents a hyperboloid of one sheet, with circular cross-sections in all planes perpendicular to the x-axis.

11.

x 2 4z 2 D 4 represents a hyperbolic cylinder with axis along the y-axis. z

z x 2 Cy 2 Cz 2 D4

y

y

x

x

x

y

x 2 4z 2 D4

Fig. 10.5-11 Fig. 10.5-8 9. z D xy represents a hyperbolic paraboloid containing the x- and y-axes.

12. y D z 2 represents a parabolic cylinder with vertex line along the x-axis. z

z

yDz 2 y y x

zDxy x

Fig. 10.5-12 Fig. 10.5-9 10. x 2 C4z 2 D 4 represents an elliptic cylinder with axis along the y-axis.

408

13.

  1 2 1 represents a parabolic cylinder x D z Cz D z C 2 4 with vertex line along the line z D 1=2, x D 1=4. 2

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lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 10.5

(PAGE 603)

z z

.z 1/2 D.x 2/2 C.y 3/2 C4

xDz 2 Cz

.2;3;1/ y

y x x

Fig. 10.5-16

Fig. 10.5-13 14.

x 2 D y 2 C 2z 2 represents an elliptic cone with vertex at the origin and axis along the x-axis. 17.

z

x 2 Dy 2 C2z 2



x2 C y2 C z2 D 4 represents the circle of intersection of xCy Cz D1 a sphere and a plane. The circle lies in the plane x pC y C z D 1,pand has centre .1=3; 1=3; 1=3/ and radius 4 .3=9/ D 11=3. z



xCyCzD1

x

1 1 1 3;3;3



y x 2 Cy 2 Cz 2 D4

x

y

Fig. 10.5-14 15.

.z 1/2 D .x 2/2 C .y 3/2 represents a circular cone with axis along the line x D 2, y D 3, and vertex at .2; 3; 1/

Fig. 10.5-17

z .z

1/2 D.x

2/2 C.y

3/2

18.



x2 C y2 D 1 is the ellipse of intersection of the plane z DxCy z D x C y and the circular cylinder x 2 C y 2 D 1. The centre of the ellipse p is at the p origin, p and the ends of the major axis are ˙.1= 2; 1= 2; 2/. z

.2;3;1/ y

zDxCy

x

y x 2 Cy 2 D1

Fig. 10.5-15 x

16. .z 1/2 D .x 2/2 C .y 3/2 C 4 represents a hyperboloid of two sheets with centre at .2; 3; 1/, axis along the line x D 2, y D 3, and vertices at .2; 3; 1/ and .2; 3; 3/.

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Fig. 10.5-18

409

lOMoARcPSD|6566483

SECTION 10.5 (PAGE 603)

19.

ADAMS and ESSEX: CALCULUS 9



z 2 D x 2 C y 2 is the parabola in which the plane z D1Cx z D 1 C x intersects the circular cone z 2 D x 2 C y 2 . (It is a parabola because the plane is parallel to a generator of the cone, namely the line z D x, y D 0.) The vertex of the parabola is . 1=2; 0; 1=2/, and its axis is along the line y D 0, z D 1 C x. z

Family 2:

The cylinder 2x 2 C y 2 D 1 intersects horizontal planes p in ellipses with semi-axes 1 in the y direction and 1= 2 in the x direction. Tilting the plane in the x direction will cause the shorter semi-axis to increase in length. The plane z D cx intersects the cylinder in an ellipse with principal axes p p through the points .0; ˙1; 0/ and .˙1= 2; 0; ˙c= 2/. The semi-axes will be equal (and the ellipse will be a circle) if .1=2/ C .c 2 =2/ D 1, that is, if c D ˙1. Thus cross-sections of the cylinder perpendicular to the vectors a D i ˙ k are circular.

24.

The plane z D cx C k intersects the elliptic cone z 2 D 2x 2 C y 2 on the cylinder

zD1Cx

c 2 x 2 C 2ckx C k 2 D 2x 2 C y 2

c 2 /x 2 2ckx C y 2 D k 2  2 ck 2k 2 c2k2 2 2 D .2 c 2 / x C y D k C 2 c2 2 c2 2 c2 2 2 y .x x0 / C 2 D 1; a2 b

y

.2

Fig. 10.5-19 20.



x 2 C 2y 2 C 3z 2 D 6 is an ellipse in the plane yD1 y D 1. Its projection onto the xz-plane is the ellipse x 2 C 3z 2 D 4. One quarter of the ellipse is shown in the figure.

where x0 D

z p

2

yD1

p

3

a; 0; c.x0 a/ C k/ and .x0 ; b; cx0 C k/

x 2 C2y 2 C3z 2 D6

a2 C c 2 a2 D b 2 ;

Fig. 10.5-20 21.

x2 y2 z2 C 2 2 a b c2 x2 z2 D1 2 2 a  x cz   x C a c a

that is,

Family 1:

410

2k 2 2k 2 D ; 2 2 .2 c / 2 c2 p or 1 C c 2 D 2 c 2 . Thus p c D ˙1= 2. Apvector normal to the plane z D ˙.x= 2/ C k is a D i ˙ 2k.

D1

y2 b 2  z y y D 1C 1 c b b  8 x z y < C D 1C a c  b Family 1: :  x z D 1 y. a c b  8 x z y < C D 1 a c  b : Family 2: :  x z D 1C y. a c b

22. z D xy

to .x0 C a; 0; c.x0 C a/ C k/; to .x0 ; b; cx0 C k/:

The centre of this ellipse is .x0 ; 0; cx0 C k/. The ellipse is a circle if its two semi-axes have equal lengths, that is, if

y p 6

2k 2 2k 2 ck , a2 D , and b 2 D . 2 2 2 2 c .2 c / 2 c2

As in the previous exercise, z D cx C k intersects the cylinder (and hence the cone) in an ellipse with principal axes joining the points .x0

x

z D y  D x:

23.

z 2 Dx 2 Cy 2

x

n



z D x  D y:

.1 C c 2 /

Section 10.6 Cylindrical and Spherical Coordinates (page 607) 1.

Cartesian: .2; p2; 1/; Cylindrical: Œ2 2; =4; 1; Spherical: Œ3; cos 1 .1=3/; =4.

2.

Cylindrical: p Œ2; =6; 2; p Cartesian: . 3; 1; 2; Spherical: Œ2 2; 3=4; =6.

3.

Spherical: Œ4;p =3; 2=3; p 3; 3; 2/; Cylindrical: Œ2 3; 2=3; 2. Cartesian: .

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lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 10.7

4. Spherical: Œ1; ;  ; Cylindrical: Œr; =4; r.

4.

p x D sin  cos  D r cos =4 D r= 2 p y D sin  sin  D r sin =4 D r= 2 z D cos  D r: Thus x D y,  D =4,pand r D sin  D cos . Hence  D =4, p so r D 1= 2. Finally: x D y D 1=2, z D 1= 2. p Cartesian: .1=2; 1=2; 1= 2/.

5.

5.  D =2 represents the half-plane x D 0, y > 0. 6.  D 2=3 represents the lower half of the right-circular cone with vertex at the origin, axis along the z-axis, and semi-vertical angle =3. Its Cartesian equation is p zD .x 2 C y 2 /=3. 7.

 D =2 represents the xy-plane.

8. R D 4 represents the sphere of radius 4 centred at the origin. 9. r D 4 represents the circular cylinder of radius 4 with axis along the z-axis. 10. R D z represents the positive half of the z-axis. 11.

w y

x z



a c

b d

1 B 0 AAT D B @0 0 0 4 B3 DB @2 1 0 1 B 0 A2 D B @0 0 0 1 B0 DB @0 0

1 1 0 0 3 3 2 1 1 1 0 0 2 1 0 0

0



D

1 1 1 0 2 2 2 1 1 1 1 0 3 2 1 0



aw C cx ay C cz

10 1 1 B1 1C CB 1A@1 1 1 1 1 1C C 1A 1 10 1 1 B0 1C CB 1A@0 0 1 1 4 3C C 2A 1

bw C dx by C dz

0 1 1 1

0 0 1 1

1 0 0C C 0A 1

1 1 0 0

1 1 1 0

1 1 1C C 1A 1



R D r represents the xy-plane.

12. R D 2x represents the half-cone with vertex at the origin, axis along the positive x-axis, and p semi-vertical angle =3. Its Cartesian equation is x D .y 2 C z 2 /=3.

6.

13. If R D 2 cos , then R2 D 2R cos , so

x 2 C y 2 C z 2 D 2z

x2 C y2 C z2

2z C 1 D 1

x 2 C y 2 C .z

1/2 D 1:

Thus R D 2 cos  represents the sphere of radius 1 centred at .0; 0; 1/. 14.



(PAGE 617)

r D 2 cos  ) x 2 C y 2 D r 2 D 2r cos  D 2x, or .x 1/2 C y 2 D 1. Thus the given equation represents the circular cylinder of radius 1 with axis along the vertical line x D 1, y D 0.

D ax 2 C by 2 C cz 2 C 2pxy C 2qxz C 2ryz

Section 10.7 A Little Linear Algebra (page 617) 0

10 1 0 3 0 2 2 1 6 1. @ 1 1 2 A @ 3 0 A D @ 5 1 1 1 0 2 1 0 10 1 0 1 1 1 1 1 1 1 2. @ 0 1 1 A @ 0 1 1 A D @ 0 0 0 1 0 0 1 0     a b w x aw C by 3. D c d y z cw C dy

1 7 3A 1 1 2 3 1 2A 0 1

7.

ax C bz cx C dz



0 1 0 1 x a p q x D @y A; A D @p b r A z q r c 0 1 0 2 1 x x xy xz T 2 yz A xx D @ y A .x; y; z/ D @ xy y z xz yz z 2 0 1 x T x x D .x; y; z/ @ y A D .x 2 C y 2 C z 2 / z 0 10 1 a p q x T x Ax D .x; y; z/ @ p b r A @ y A q r c z 0 1 ax C py C qz D .x; y; z/ @ px C by C rz A qx C ry C cz

ˇ ˇ ˇ ˇ ˇ ˇ ˇ ˇ

2 4 1 2

D

3

3 0 0 0 

ˇ 1 0 ˇˇ 2 1 ˇˇ D 1 1 ˇˇ 0 1ˇ ˇ ˇ ˇ 1 1ˇ ˇ 2 ˇˇ 2 1ˇ

D 6.3/ C 3.6/ D 36

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ˇ ˇ 4 ˇ 3 ˇˇ 1 ˇ 2 ˇ ˇ 4 1 ˇˇ 2

ˇ 2 1 ˇˇ 1 1 ˇˇ 0 1ˇ ˇ 1 ˇˇ 1ˇ

411

lOMoARcPSD|6566483

SECTION 10.7 (PAGE 617)

8.

ˇ ˇ ˇ ˇ ˇ ˇ ˇ ˇ

1 1 2 3

D

D

D

9.

1 2 0 3 ˇ ˇ 1 ˇ 2 ˇˇ 2 ˇ 3 ˇ ˇ1 ˇ 2 ˇˇ 0 ˇ0 ˇ ˇ1 2 ˇˇ 5

ˇ 1 1 ˇˇ 3 4 ˇˇ 2 4 ˇˇ 2 2ˇ ˇ ˇ ˇ1 1 1 ˇˇ ˇ 3 4 ˇˇ C 2 ˇˇ 1 ˇ3 2 2ˇ ˇ ˇ ˇ1 1 1ˇ ˇ ˇ 4 ˇˇ 1 2 3 ˇˇ ˇ3 3 2ˇ ˇ ˇ ˇ1 1 1 1 ˇˇ ˇ 1 2 ˇˇ C 2 ˇˇ 0 1 ˇ0 5 1ˇ 6 ˇ ˇ ˇ ˇ1 1 1 ˇ ˇ 2 ˇˇ 4 ˇˇ 0 1 ˇ0 6 1ˇ ˇ ˇ ˇ ˇ 1 2 ˇˇ 3 ˇˇ ˇ C 2ˇ 1ˇ 6 5ˇ

ADAMS and ESSEX: CALCULUS 9

Generalization: ˇ ˇ 1 ˇ ˇ x1 ˇ 2 ˇ x1 ˇ ˇ :: ˇ : ˇ ˇ xn 1

ˇ 1 ˇˇ 4 ˇˇ 2ˇ

1 2 3

1

ˇ 1 ˇˇ 3 ˇˇ 5ˇ

11.

ˇ ˇ 1 4 ˇˇ 6

D 2. 9/ C 2.13/ 4.11/ D 0 ˇ ˇ ˇ a11 a12 a13    a1n ˇ ˇ ˇ ˇ 0 a22 a23    a2n ˇ ˇ ˇ ˇ 0 0 a33    a3n ˇˇ ˇ :: :: :: ˇ ˇ :: :: ˇ : : : : : ˇˇ ˇ ˇ 0 0 0    ann ˇ ˇ ˇ ˇ a22 a23    a2n ˇ ˇ ˇ ˇ 0 a33    a3n ˇ ˇ ˇ :: :: ˇ D a11 ˇ :: :: ˇ : ˇ : : : ˇ ˇ ˇ 0 0    ann ˇ ˇ ˇ ˇ a33    a3n ˇ ˇ ˇ :: ˇ ˇ : :: D a11 a22 ˇ :: ˇ : : ˇ ˇ ˇ 0    ann ˇ

ˇ ˇ 1 ˇ f .x; y; z/ D ˇˇ x ˇ x2

ˇ 2 ˇˇ 1ˇ

a c

    b ` m w , CD , BD d n p y

12. If A D



  b a , then AT D d b

a c

x/.z

xi /:

 x . Then z

 c , and d

bc D det.AT /:

det.A/ D ad

We generalize this by induction. Suppose det(BT )=det(B) for any .n where n  3. Let 0

1 y y2

a11 B a21 B A D B :: @ : an1

ˇ 1 ˇˇ z ˇˇ ; z2 ˇ

x/.z

a12 a22 :: :

  :: :

an2



1/  .n

1/ matrix,

1 a1n a2n C C :: C : A

ann

be an n  n matrix. If det(A) is expanded in minors about the first row, and det(AT ) is expanded in minors about the first column, the corresponding terms in these expansions are equal by the induction hypothesis. (The .n 1/.n 1/ matrices whose determinants appear in one expansion are the transposes of those in the other expansion.) Therefore det(AT )=det(A) for any square matrix A.

13.

Let A D



a c

b d



and B D

x and

f .x; y; z/ D .y

412



ˇ 1 ˇ ˇ xn ˇ Y 2 ˇˇ xn .xj ˇD :: ˇ : ˇˇ 1i 0;

26. ˇ 1 ˇˇ D 1ˇ



G ı F .x1 ; x2 / D G.y1 ; y2 /    ax1 C bx2 p q D cx1 C dx2 r s   pax1 C pbx2 C qcx1 C qdx2 D rax1 C rbx2 C scx1 C sdx2

1

ˇ 2 0 ˇˇ 1 0 ˇˇ D 0 1ˇ

ˇ 2 ˇˇ D 1ˇ

indefinite. 1 1 1 2 1 A. Use Theorem 8. 1 2

ˇ ˇ2 ˇ D3 D ˇˇ 1 ˇ1

   a b x1 . , where F D c d x    2 p q y1 , where G D . Let G.y1 ; y2 / D G y2 r s If y1 D ax1 C bx2 and y2 D cx1 C dx2 , then

414

Thus, G ı F is represented by the matrix GF.   1 1 A D . Use Theorem 8. D1 D 1 < 0, 1 2 ˇ ˇ ˇ 1 1 ˇ ˇ D 1 > 0. Thus A is negative definite. D2 D ˇˇ 1 2ˇ 0 1 1 2 0 A D @ 2 1 0 A. Use Theorem 8. 0 0 1 D1 D 1 > 0;

ˇ ˇ ˇ1 1 0 1 ˇ ˇ ˇ 1 ˇˇ 1 1 4 1 ˇˇ 1 ˇˇ 8 ˇˇ 1 1 6 ˇ1 1 2 1ˇ ˇ ˇ ˇ0 2 0 1 ˇ ˇ ˇ 1 ˇˇ 1 ˇˇ 0 0 4 1 ˇˇ 8 ˇˇ 0 0 6 ˇ2 2 2 1ˇ ˇ ˇ ˇ2 0 1 ˇ ˇ ˇ ˇ 2 ˇˇ ˇ D 4 ˇ4 0 4 1 ˇ6 ˇ 8 ˇˇ 0 6 8 1ˇ .x1 C x2 C x3 / D 2:

22. Let F .x1 ; x2 / D F

24.



ˇ ˇ2 D2 D ˇˇ 1

3 < 0;

3 < 0:

ˇ 1 ˇˇ D 3 > 0; 2ˇ

ˇ 1 1 ˇˇ 2 1 ˇˇ D 4 > 0: 1 2ˇ

Thus A is positive definite. 1 0 ˇ ˇ 1 1 0 ˇ1 1ˇ ˇ D 0, we cannot A D @ 1 1 0 A. Since D2 D ˇˇ 1 1ˇ 0 0 1 use Theorem 8. The corresponding quadratic form is Q.x; y; z/ D x 2 C y 2 C 2xy C z 2 D .x C y/2 C z 2 ;

27.

which is positive semidefinite. (Q.1; 1; 0/ D 0.). Thus A is positive semidefinite. 0 1 1 0 1 1 A. Use Theorem 8. A D @0 1 1 1 1 D1 D 1 > 0; ˇ ˇ1 ˇ D3 D ˇˇ 0 ˇ1

Thus A is indefinite.

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ˇ ˇ1 D2 D ˇˇ 0 0 1 1

ˇ 1 ˇˇ 1 ˇˇ D 1 ˇ

ˇ 0 ˇˇ D 1 > 0; 1ˇ 1 < 0:

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INSTRUCTOR’S SOLUTIONS MANUAL

0

2 28. A D @ 0 1

0 4 1

SECTION 10.8

1 1 11 A. Use Theorem 8. 1

D1 D 2 > 0; ˇ ˇ2 ˇ D3 D ˇˇ 0 ˇ1

ˇ ˇ ˇ2 0ˇ ˇ D 8 > 0; D2 D ˇˇ 0 4ˇ 0 4 1

Thus A is positive definite.

ˇ 1 ˇˇ 11 ˇˇ D 2 > 0: 1 ˇ

Section 10.8 Using Maple for Vector and Matrix Calculations (page 626)

> a := DotProduct(U,(V W),conjugate=false):

&x

> b := DotProduct(V,(W U),conjugate=false):

&x

> c := DotProduct(W,(U V),conjugate=false):

&x

(PAGE 626)

> simplify(a-b); simplify(a-c); 0 0 4.

These calculations verify the identity: > U := Vector[row](3,symbol=u): V := Vector[row](3,symbol=v):

It is assumed that the Maple package LinearAlgebra has been loaded for all the calculations in this section.

> W := Vector[row](3,symbol=w): 1.

We use the result of Example 9 of Section 10.4. > LHS := (U &x V) &x (U &x W): > RHS := (DotProduct(U,(V &x W),conjugate=false))*U:

> r1 := : v1 := : > r2 := : v2 := : > v1xv2 := v1 &x v2: > dist := abs((r2-r1).v1xv2)/Norm(v1xv2,2); d i st WD 2

> simplify(LHS-RHS); Œ0; 0; 0

The distance between the two lines is 2 units. 2. The plane P through the origin containing the vectors v1 D i 2j 3k and v2 D 2i C 3j C 4k has normal n D v1  v2 . >

n := &x ; n WD Œ1; 10; 7

The angle between v D i

sp := (U,V) -> DotProduct(U,Normalize(V,2),conjugate=false)

6.

vp := (U,V) -> DotProduct(U,Normalize(V,2), conjugate=false)*Normalize(V,2)

7.

ang := (u,v) -> evalf((180/Pi)*VectorAngle(U,V))

8.

unitn := (U,V)->Normalize((U &x V),2)

9.

VolT := (U,V,W)->(1/6)*abs(DotProduct(U,(V &x W), conjugate=false))

j C 2k and n (in degrees) is

> angle := evalf((180/Pi)*VectorAngle(n,)); angvn WD 33:55730975 Since this angle is acute, the angle between v and the plane P is its complement. >

5.

angle := 90 - angvn; angle WD 56:44269025

10. dist:=(A,B)->Norm(A-B,2)

3. These calculations verify the identity:

> dist(,); 5

> U := Vector[row](3,symbol=u): V := Vector[row](3,symbol=v): >

W := Vector[row](3,symbol=w): 11.

We use LinearSolve.

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ADAMS and ESSEX: CALCULUS 9

> A := Matrix([[1,2,3,4,5], > [6,-1,6,2,-3],[2,8,-8,-2,1], > [1,1,1,1,1],[10,-3,3,-2,2]]): > X := LinearSolve(A,,free=t); 2 3 1 6 0 7 6 7 7 X WD 6 6 17 4 3 5 2 The solution is u D 1, v D 0, x D

16.

> A := Matrix([[1,1/2,1/3], > [1/2,1/3,1/4],[1/3,1/4,1/5]]): > Ainv := MatrixInverse(A): > Digits := 10: evalf(Eigenvalues(A)); 2 3 1:408318927 4 10 11 I 4 0:00268734034 5:673502694 10 10 I 5 0:1223270659 C 5:873502694 10 10 I > evalf(Eigenvalues(Ainv)); 3 2 372:1151279 2 10 9 I 4 0:710066409 5:096152424 10 8 I 5 8:174805711 C 5:296152424 10 8 I

1, y D 3, z D 2.

12. We use LinearSolve. > B := Matrix([[1,1,1,1,0], > [1,0,0,1,1],[1,0,1,1,0], > [1,1,1,0,1],[0,1,0,1,-1]]): > X := LinearSolve(B,,free=t); 2 3 11 2t5 6 7 2 6 7 7 2 C t X WD 6 5 6 7 4 1 C t5 5 t5

The small imaginary parts are due to round-off errors in the solution process. The eigenvalues are real since the matrix and its inverse are real and symmetric. Although they appear in different orders, each eigenvalue of A 1 is the reciprocal of an eigenvalue of A. This is to be expected since A

1

x D x



.1=/x D Ax:

There is a one-parameter family of solutions: u D 11 2t , v D 2, x D 2 C t , y D 1 C t , z D t , for arbitrary t .

13.

14.

15.

> A := Matrix([[1,2,3,4,5], > [6,-1,6,2,-3],[2,8,-8,-2,1], > [1,1,1,1,1],[10,-3,3,-2,2]]): > Determinant(A); 935

> B := Matrix([[1,1,1,1,0], > [1,0,0,1,1],[1,0,1,1,0], > [1,1,1,0,1],[0,1,0,1,-1]]): > Digits := 5: evalf(Eigenvalues(B)); 2 3 0 6 3:3133 0:0000053418I 7 6 7 6 0:8693 C 0:0000073520I 7 6 7 4 1:2728 0:0000025143I 5 7 1:9098 C 5:041 10 I

Review Exercises 10 (page 627) 1.

x C 3z D 3 represents a plane parallel to the y-axis and passing through the points .3; 0; 0/ and .0; 0; 1/.

2.

y z  1 represents all points on or below the plane parallel to the x-axis that passes through the points .0; 1; 0/ and .0; 0; 1/.

3.

x C y C z  0 represents all points on or above the plane through the origin having normal vector i C j C k.

4.

x 2y 4z D 8 represents all points on the plane passing through the three points .8; 0; 0/, .0; 4; 0/, and .0; 0; 2/.

5.

y D 1 C x 2 C z 2 represents the circular paraboloid obtained by rotating about the y-axis the parabola in the xy-plane having equation y D 1 C x 2 . y D z 2 represents the parabolic cylinder parallel to the x-axis containing the curve y D z 2 in the yz-plane.

The tiny imaginary parts are due to roundoff error in the calculations. They should all be 0. Since B is a real, symmetric matrix, its eigenvalues are all real. The eigenvalues, rounded to 5 decimal places are 0, 3.3133, 0.8693, 1:2728, and 1:9098.

6. 7.

x D y 2 z 2 represents the hyperbolic paraboloid whose intersections with the xy- and xz-planes are the parabolas x D y 2 and x D z 2 , respectively.

> A := Matrix([[1,1/2,1/3], > [1/2,1/3,1/4],[1/3,1/4,1/5]]): > Ainv := MatrixInverse(A); 2 3 9 36 30 180 5 Ai nv WD 4 36 192 30 180 180

8.

z D xy is the hyperbolic paraboloid containing the x- and y-axes that results from rotating the hyperbolic paraboloid z D .x 2 y 2 /=2 through 45ı about the z-axis.

416

9.

x 2 C y 2 C 4z 2 < 4 represents the interior of the circular ellipsoid (oblate spheroid) centred at the origin with semiaxes 2, 2, and 1 in the x, y, and z directions, respectively.

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REVIEW EXERCISES 10

10. x 2 C y 2 4z 2 D 4 represents a hyperboloid of one sheet with circular cross-sections in planes perpendicular to the z-axis, and asymptotic to the cone obtained by rotating the line x D 2z about the z-axis. 11.

21.

x 2 y 2 4z 2 D 0 represents an elliptic cone with axis along the x-axis whose cross-sections in planes x D k are ellipses with semi-axes jkj and jkj=2 in the y and z directions, respectively.

14.

15.

.x z/2 C y 2 D z 2 represents an elliptic cone with oblique axis along the line z D x in the xz-plane, having circular cross-sections of radius jkj in horizontal planes z D k. The z-axis lies on the cone.

17.

or 2x C 5y C 3z D 2. 22.

23.

19. The given line is parallel to the vector a D 2i jC3k. The plane through the origin perpendicular to a has equation 2x y C 3z D 0. 20. A plane through .2; 1; 1/ and .1; 0; 1/ is parallel to b D .2 1/i C . 1 0/j C .1 . 1//k D i j C 2k. If it is also parallel to the vector a in the previous solution, then it is normal to ˇ ˇi ˇ a  b D ˇˇ 2 ˇ1

The plane has equation .x x y z D 2.

j 1 1 1/

ˇ k ˇˇ 3 ˇˇ D i 2ˇ .y

j

0/

24.

0/ D 0:

A plane containing the line of intersection of the planes x C y C z D 0 and 2x C y 3z D 2 has equation 2x C y

2 C .x C y C z

3z

This plane is perpendicular to x 2y normals are perpendicular, that is, if 1.2 C / or 9x C 7y 25.

2.1 C /

26.

0/ D 0: 5z D 17 if their

5. 3 C / D 0;

z D 4.

The line through .2; 1; 1/ and . 1; 0; 1/ is parallel to the vector 3i C j 2k, and has vector parametric equation r D .2 C 3t /i C .1 C t /j

.1 C 2t /k:

A vector parallel to the planes x y D 3 and x C 2y C z D 1 is .i j/  .i C 2j C k/ D i j C 3k. A line through .1; 0; 1/ parallel to this vector is x

1 1

D

y zC1 D : 1 3

27.

The line through the origin perpendicular to the plane 3x 2y C 4z D 5 has equations x D 3t , y D 2t , z D 4t .

28.

The vector

k:

.z C 1/ D 0, or

2 C .x C y C z

3z

This plane passes through .2; 0; 1/ if 1 C 3 D 0. In this case, the equation is 7x C 4y 8z D 6.

2

18. x C z  1, x y  0 together represent all points that lie inside or on the circular cylinder of radius 1 and axis along the y-axis and also either on the vertical plane x y D 0 or on the side of that plane containing the positive x-axis.

A plane containing the line of intersection of the planes x C y C z D 0 and 2x C y 3z D 2 has equation 2x C y

x 2 C y 2 C z 2 D 4, x C y C z D 3 together represent the circle in which the sphere of radius 2 centred at the origin intersects the plane through .1; 1;p1/ with normal i C j C k. Since this plane lies p at distance 3 from the origin, the circle has radius 4 3 D 1. 2

The plane through A D . 1; 1; 0/, B D .0; 4; 1/ and C D .2; 0; 0/ has normal ˇ ˇ ˇi j k ˇˇ ! ! ˇˇ 3 1 0 ˇˇ D i C 3j C 10k: AC  AB D ˇ ˇ1 3 1ˇ

Its equation is .x 2/C3y C10z D 0, or x C3y C10z D 2.

x C2y D 0, z D 3 together represent the horizontal straight line through the point .0; 0; 3/ parallel to the vector 2i j.

16. x C y C 2z D 1, x C y C z D 0 together represent the straight line through the points . 1; 0; 1/ and .0; 1; 1/.

A plane perpendicular to x y Cz D 0 and 2x Cy 3z D 2 has normal given by the cross product of the normals of these two planes, that is, by ˇ ˇ ˇi j k ˇˇ ˇ ˇ1 1 1 ˇˇ D 2i C 5j C 3k: ˇ ˇ2 1 3ˇ If the plane also passes through .2; 1; 1/, then its equation is 2.x 2/ C 5.y C 1/ C 3.z 1/ D 0;

12. x 2 y 2 4z 2 D 4 represents a hyperboloid of two sheets asymptotic to the cone of the previous exercise. 13. .x z/2 C y 2 D 1 represents an elliptic cylinder with oblique axis along the line z D x in the xz-plane, having circular cross-sections of radius 1 in horizontal planes z D k.

(PAGE 627)

a D .1 C t /i

tj

D .1 C t

2s/i

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.2 C 2t /k .t C s

2/j

 2si C .s

.1 C 2t

2/j 3s/k

 .1 C 3s/k

417

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REVIEW EXERCISES 10 (PAGE 627)

ADAMS and ESSEX: CALCULUS 9

joins points on the two lines and is perpendicular to both lines if a  .i j 2k/ D 0 and a  .2i C j 3k/ D 0, that is, if 1Ct 2 C 2t

2s C t C s 2 C 2 C 4t 4s t s C 2 C 3 C 6t

32.

The tetrahedron with vertices A D .1; 2; 1/, B D .4; 1; 1/, C D .3; 4; 2/, and D D .2; 2; 2/ has volume 1 1 ! ! ! j.AB  AC /  ADj D j.9i C 9j C 12k/  .i C k/j 6 6 7 9 C 12 D cu. units: D 6 2

6s D 0 9s D 0;

or, on simplification, 33. 6t 7s D 7t 14s D

1 7:

This system has solution t D 1, s D 1. We would expect to use a as a vector perpendicular to both lines, but, as it happens, a D 0 if t D s D 1, because the two given lines intersect at .2; 1; 4/. A nonzero vector perpendicular to both lines is ˇ ˇ ˇi j k ˇˇ ˇ ˇ1 1 2 ˇˇ D 5i j C 3k: ˇ ˇ2 1 3ˇ

Thus the required line is parallel to this vector and passes through .2; 1; 4/, so its equation is r D .2 C 5t /i

The inverse of A satisfies 10 0 1 0 0 0 a b B2 1 0 0CB e f B CB @3 2 1 0A@ i j 4 3 2 1 m n

a D 1; b D 0; c D 0; d D 0;

2a C e D 0; 3a C 2e C i 2b C f D 1; 3b C 2f C j 2c C g D 0; 3c C 2g C k 2d C h D 0; 3d C 2h C l

a D 1; e D 2; b D 0; f D 1; c D 0; g D 0; d D 0; h D 0; Thus A

r1 / D 0:

(Any permutation of the subscripts 1, 2, and 3 in the above equation will do as well.) 30. The points with position vectors r1 , r2 , r3 , and r4 are coplanar if the tetrahedron having these points as vertices has zero volume, that is, if h

.r2

r1 /  .r3

i r1 /  .r4

r1 / D 0:

(Any permutation of the subscripts 1, 2, 3, and 4 in the above equation will do as well.) 31. The triangle with vertices A D .1; 2; 1/, B D .4; 1; 1/, and C D .3; 4; 2/ has area ˇ ˇi ˇ 1 1 ! ! jAB  AC j D j ˇˇ 3 2 2 ˇ2

j 3 2

ˇ k ˇˇ 0 ˇˇ j 3ˇ

p 1 3 34 D j9i C 9j C 12kj D sq. units: 2 2

34.

0

1

0

1 B 2 DB @ 1 0

1 0 0C C: 0A 1

D 0; D 0; D 1; D 0;

4a C 3e C 2i C m D 0: 4b C 3f C 2j C n D 0: 4c C 3g C 2k C o D 0: 4d C 3h C 2l C p D 1:

i j k l

D 1; D 2; D 1; D 0;

0 1 2 1

0 0 1 2

m D 0; n D 1; o D 2; p D 1: 1 0 0C C: 0A 1

1 0 1 0 1 1 1 1 x1 b1 Let A D @ 2 1 0 A, x D @ x2 A, and b D @ b2 A. 1 0 1 x3 b3 Then Ax D b , x1 C x2 C x3 D b1 2x1 C x2 D b2 x1 x3 D b3 : The sum of the first and third equations is 2x1 C x2 D b1 C b3 , which is incompatible with the second equation unless b2 D b1 C b3 , that is, unless b  .i

j C k/ D 0:

If b satisfies this condition then there will be a line of solutions; if x1 D t , then x2 D b2 2t , and x3 D t b3 , so 0 1 t x D @ b2 2t A t b3

is a solution for any t .

418

0 0 1 0

These systems have solutions

.1 C t /j C . 4 C 3t /k:

r1 /  .r3

0 1 0 0

Expanding the product on the left we get four systems of equations:

29. The points with position vectors r1 , r2 , and r3 are collinear if the triangle having these points as vertices has zero area, that is, if .r2

1 0 d 1 B0 hC CDB l A @0 p 0

c g k o

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INSTRUCTOR’S SOLUTIONS MANUAL

0

3 35. A D @ 1 1

CHALLENGING PROBLEMS 10

1 1 1 A. We use Theorem 8. 2

1 1 1

D1 D 3 > 0;

ˇ ˇ 3 ˇ D3 D ˇˇ 1 ˇ 1

1 1 1

Thus A is positive definite.

1 jx2 y3 x2 y1 x1 y3 2 ˇ ˇ ˇ x y1 1 ˇ ˇ 1 ˇˇ 1 D j ˇ x2 y2 1 ˇˇ j: 2 ˇx y 1ˇ 3 3

D

ˇ 1 ˇˇ D 2 > 0; 3 ˇ

ˇ ˇ 3 D2 D ˇˇ 1

ˇ 1 ˇˇ 1 ˇˇ D 2 > 0: 2 ˇ

4.

Challenging Problems 10 (page 628) 1.

If d is the distance from P to the line AB, then d is the altitude of the triangle APB measured perpendicular to the base AB. Thus the area of the triangle is ! .1=2/d jBAj D .1=2/d jrA

rB j:

On the other hand, the area is also given by ! ! .1=2/jPA  PBj D .1=2/j.rA

rP /  .rB

j.rA

rP /  .rB jrA rB j

rP /j

a) Let Q1 and Q2 be the points on lines L1 and L2 , respectively, that are closest together. As observed in ! Example 9 of Section 1.4, Q1 Q2 is perpendicular to both lines. Therefore, the plane P1 through Q1 having normal ! Q1 Q2 contains the line L1 . Similarly, the plane P2 ! through Q2 having normal Q1 Q2 contains the line L2 . These planes are parallel since they have the same normal. They are different planes because Q1 ¤ Q2 (because the lines are skew).

r1 D .1 C t /i C .1

r2 D si C .1 C s/j C .1 C s/k: Now r2

.u  v/  .w  x/ D Œ.u  v/  xw Œ.u  v/  wx .u  v/  .w  x/ D .w  x/  .u  v/ D Œ.w  x/  vu C Œ.w  x/  uv:

.s .s

.u  v/  .u  x/ D Œ.u  v/  xu;

.u  v/  .u  w/ D Œ.u  v/  wu:

x1 /.y3

y1 /

.x3

x1 /.y2

t

1/i C .s C t /j C .1 C s

t /k.

t t

1/ .s C t / C .1 C s 1/ C .s C t / C .1 C s

t/ D 0 t / D 0:

Subtracting these equations gives s C t D 0, so t D s. Then substituting into either equation gives 2s 1 C 1 C 2s D 0, so s D t D 0. Thus Q1 D .1; 1; 0/ and Q2 D .0; 1; 1/, and ! Q1 Q2 D i C k. The required planes are x z D 1 (containing L1 ) and x z D 1 (containing L2 ).

or, replacing x with w,

3. The triangle with vertices .x1 ; y1 ; 0/, .x2 ; y2 ; 0/, and .x3 ; y3 ; 0/, has two sides corresponding to the vectors .x2 x1 /i C .y2 y1 /j and .x3 x1 /i C .y3 y1 /j. Thus the triangle has area given by ˇ ˇ ˇ i j k ˇˇ 1 ˇˇ A D j ˇ x2 x1 y2 y1 0 ˇˇ j 2 ˇx x1 y3 y1 0 ˇ 3

r1 D .s

To find the points Q1 on L1 and Q2 on L2 for ! which Q1 Q2 is perpendicular to both lines, we solve

In particular, if w D u, then, since .u  v/  u D 0, we have

1 jŒ.x2 2

t /j C t k:

Line L2 through .0; 1; 1/ and .1; 2; 2/ is parallel to i C j C k, and has parametric equation

:

2. By the formula for the vector triple product given in Exercise 23 of Section 1.3,

D

x3 y2 C x3 y1 C x1 y2 j

b) Line L1 through .1; 1; 0/ and .2; 0; 1/ is parallel to i j C k, and has parametric equation

rP /j:

Equating these two expressions for the area of the triangle and solving for d we get dD

(PAGE 628)

5.

This problem is similar to Exercise 28 of Section 1.3. The equation a  x D b has no solution x unless a  b D 0. If this condition is satisfied, then x D x0 C t a is a solution for any scalar t , where x0 D .b  a/=jaj2 .

y1 /kj

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ADAMS and ESSEX: CALCULUS 9

CHAPTER 11. VECTOR FUNCTIONS AND CURVES

9.

Section 11.1 Vector Functions of One Variable (page 635) 1.

10. Position: r D 3 cos t i C 4 sin t j C t k Velocity: v D p 3 sin t i C 4 cos t j C k p Speed: v D 9 sin2 t C 16 cos2 t C 1 D 10 C 7 cos2 t Acceleration : a D 3 cos t i 4 sin t j D t k r Path: a helix (spiral) wound around the elliptic cylinder .x 2 =9/ C .y 2 =16/ D 1.

Position: r D i C t j Velocity: v D j Speed: v D 1 Acceleration : a D 0 Path: the line x D 1 in the xy-plane.

Position: r D ae t i C be t j C ce t k Velocity and acceleration: vDaDr p Speed: v D e t a2 C b 2 C c 2 x y z Path: the half-line D D > 0. a b c 12. Position: r D at cos !t i C at sin !t j C b ln t k Velocity: v D a.cos !t !t sin !t /i C a.sin !t C !t cos !t /j C .b=t /k p Speed: v D a2 .1 C ! 2 t 2 / C .b 2 =t 2 / Acceleration: a D a!.2 sin !t C ! cos !t /i 11.

2. Position: r D t 2 i C k Velocity: v D 2t i Speed: v D 2jt j Acceleration : a D 2i Path: the line z D 1, y D 0. 3. Position: r D t 2 j C t k Velocity: v D p2t j C k Speed: v D 4t 2 C 1 Acceleration : a D 2j Path: the parabola y D z 2 in the plane x D 0.

C a!.2 cos !t ! sin !t /j .b=t 2 /k Path: a spiral on the surface x 2 C y 2 D a2 e z=b .

13.

4. Position: r D i C t j C t k Velocity: v D pj C k Speed: v D 2 Acceleration : a D 0 Path: the straight line x D 1, y D z. 5. Position: r D t 2 i t 2 j C k Velocity: v Dp 2t i 2t j Speed: v D 2 2t Acceleration: a D 2i 2j Path: the half-line x D y  0, z D 1.

Position: r D a cos t i C a sin t j C ct k Velocity: v D p a sin t i C a cos t j C ck Speed: v D a2 C c 2 Acceleration: a D a cos t i a sin t j Path: a circular helix.

et k

Position: r D a cos t sin t i C a sin2 t j C a cos t k  a a 1 cos 2t j C a cos t k D sin 2t i C 2 2 Velocity: v Dp a cos 2t i C a sin 2t j a sin t k Speed: v D a 1 C sin2 t Acceleration: a D 2a sin 2t i C 2a cos 2t j a cos t k Path: the path lies on the sphere x 2 C y 2 C z 2 D a2 , on the surface defined in terms of spherical polar coordinates by  D  , on the circular cylinder x 2 C y 2 D ay, and on the parabolic cylinder ay C z 2 D a2 . Any two of these surfaces serve to pin down the shape of the path.

15.

The position of the particle is given by r D 5 cos.!t /i C 5 sin.!t /j;

8. Position: r D a cos !t i C bj C a sin !t k Velocity: v D a! sin !t i C a! cos !t k Speed: v D ja!j Acceleration: a D a! 2 cos !t i a! 2 sin !t k Path: the circle x 2 C z 2 D a2 , y D b.

420

t t Position: r D e  cos.e t /i C e t sin.e t /j  e k Velocity: v D e t cos.e t / C sin.e t / i   e t sin.e t / cos.e t / j e t k p Speed: v D 1 C e 2t C e 2t  Acceleration: a D .e t e t / cos.e t / C sin.e t / i   C .e t e t / sin.e t / cos.e t / j p Path: a spiral on the surface z x 2 C y 2 D 1.

14.

6. Position: r D t i C t 2 j C t 2 k Velocity: v D pi C 2t j C 2t k Speed: v D 1 C 8t 2 Acceleration: a D 2j C 2k Path: the parabola y D z D x 2 . 7.

Position: r D 3 cos t i C 4 cos t j C 5 sin t k Velocity: v D p 3 sin t i 4 sin t j C 5 cos t k Speed: v D 9 sin2 t C 16 sin2 t C 25 cos2 t D 5 Acceleration : a D 3 cos t i 4 cos t j 5 sin t k D r Path: the circle of intersection of the sphere x 2 C y 2 C z 2 D 25 and the plane 4x D 3y.

where ! D  to ensure that r has period 2=! D 2 s. Thus d 2r a D 2 D ! 2 r D  2 r: dt At .3; 4/, the acceleration is 3 2 i 4 2 j.

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 11.1

16. When its x-coordinate is x, the particle is at position r D xi C .3=x/j, and its velocity and speed are

Thus

The particle is at .3; 3; 2/ when u D 1. At this point du=dt D 2=3 and d 2 u=dt 2 D 16=27, and so

We know that dx=dt > 0 since the particle is moving to the right. When x D p2, we have 10 D v D .dx=dt / 1 C .9=16/ D .5=4/.dx=dt /. Thus dx=dt D 8. The velocity at that time is v D 8i 6j.

2 .3i C 6uj C 6u2 k/ D 2i C 4j C 4k 3  2 2 16 .6j C 12k/ .3i C 6j C 6k/ C aD 27 3 8 D . 2i j C 2k/: 9 vD

The particle moves along the curve z D x 2 , x C y D 2, in the direction of increasing y. Thus its position at time t is r D .2

y/2 k;

y/i C yj C .2

where y is an increasing function of time t . Thus

20.

i dy h i C j 2.2 y/k dt dy p vD 1 C 1 C 4.2 y/2 D 3 dt vD

since the speed p When y D 1, we have p is 3. dy=dt D 3= 6 D 3=2. Thus vD

r

3 . iCj 2

2k/:

i dx h i C 2xj C 3x 2 k . Since dt dz=dt D 3x 2 dx=dt D 3, when x D 2 we have 12 dx=dt D 3, so dx=dt D 1=4. Thus

so its velocity is v D

Since u is increasing and the speed of the particle is 6, 6 D jvj D 3

aD

21.

r D 3ui C 3u2 j C 2u3 k du vD .3i C 6uj C 6u2 k/ dt  2 d 2u du 2 aD .6j C 12uk/: .3i C 6uj C 6u k/ C dt 2 dt du p du 1 C 4u2 C 4u4 D 3.1 C 2u2 / : dt dt



dx dt

2

:

The left side is 3 when x D 1, so 3.d 2 x=dt 2 / C 48 D 3, and d 2 x=dt 2 D 15 at that point, and the acceleration there is

r D xi C x 2 j C x 3 k;

1 v D i C j C 3k: 4

r D xi x 2 j C Cx 2 k dx vD .i 2xj C 2xk/ dt  2 d 2x dx aD . 2j C 2k/: .i 2xj C 2xk/ C 2 dt dt ˇ ˇ p ˇ dx ˇ p dx Thus jvj D ˇˇ ˇˇ 1 C 4x 4 C 4x 4 D 1 C 8x 4 , dt dt since x is increasing. At .1; 1; 1/, x D 1 and jvj D 9, so dx=dt D 3, and the velocity at that point is v D 3i 6j C 6k. Now p 16x 3 d 2x d jvj D 1 C 8x 4 2 C p dt dt 1 C 8x 4

18. The position of the object when its x-coordinate is x is

19.

2 du , and D dt 1 C 2u2 2 du 16u d 2u D 4u : D dt 2 .1 C 2u2 /2 dt .1 C 2u2 /3

dr dx 3 dx D i j dt rdt x 2 dt ˇ ˇ ˇ dx ˇ 9 v D ˇˇ ˇˇ 1 C 4 : dt x vD

17.

(PAGE 635)

22.

15.i

2j C 2k/ C 9. 2j C 2k/ D

15i C 12j

12k:

d 2 d jvj D v  v D 2v  a. dt dt If v  a > 0 then the speed v D jvj is increasing. If v  a < 0 then the speed is decreasing. If u.t / D u1 .t /i C u2 .t /j C u3 .t /k v.t / D v1 .t /i C v2 .t /j C v3 .t /k then u  v D u1 v2 C u2 v2 C u3 v3 , so du1 dv1 du2 dv2 d uvD v1 C u1 C v2 C u2 dt dt dt dt dt dv3 du3 v3 C u3 C dt dt dv du vCu : D dt dt

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421

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SECTION 11.1 (PAGE 635)

23.

24.

25.

ADAMS and ESSEX: CALCULUS 9

ˇ ˇ ˇ a11 a12 a13 ˇ ˇ ˇ ˇ a21 a22 a23 ˇ ˇ ˇ ˇ a31 a32 a33 ˇ d h D a11 a22 a33 C a12 a23 a31 C a13 a21 a32 dt i a11 a23 a32 a12 a21 a33 a13 a22 a31

d dt

0 0 0 D a11 a22 a33 C a11 a22 a33 C a11 a22 a33 0 0 0 C a12 a23 a31 C a12 a23 a31 C a12 a23 a31 0 0 0 C a13 a21 a32 C a13 a21 a32 C a13 a21 a32 0 0 0 a11 a23 a32 a11 a23 a32 a11 a23 a32 0 0 0 a12 a21 a33 a12 a21 a33 a12 a21 a33 0 0 0 a13 a22 a31 a13 a22 a31 a13 a22 a31 ˇ 0 ˇ ˇ ˇ 0 0 ˇ ˇ a11 a12 ˇ a13 a12 a13 ˇˇ ˇ ˇ ˇ a11 0 0 0 ˇ a22 a23 D ˇˇ a21 a22 a23 ˇˇ C ˇˇ a21 ˇ ˇ a31 a32 a33 ˇ ˇ a31 a32 a33 ˇ ˇ ˇ ˇ a11 a12 a13 ˇ ˇ ˇ C ˇˇ a21 a22 a23 ˇˇ 0 0 0 ˇ a31 a32 a33 ˇ

r0 j2 D

d .r dt

r0 /  .r

32.

33.

34.

r0 /

dr D0 dt implies that jr r0 j is constant. Thus r.t / lies on a sphere centred at the point P0 with position vector r0 . D 2.r

r0 / 

30.

 d  u  .v  w/ dt D u0  .v  w/ C u  .v0  w/ C u  .v  w0 /:    d d u d 2u  2 u dt dt dt   2   du d u d 2u d u d 2u D   2 Cu  dt dt dt dt 2 dt 2  3  du d u  3 Cu dt dt     d u d 2u d u d 3u du   2 Cu  3 : D dt dt dt dt dt

422

Since

dr D v.t / D 2r.t / and r.0/ D r0 , we have dt

The path is the half-line from the origin in the direction of r0 . v  0 r D r0 cos !t C sin !t ! dr D !r0 sin !t C v0 cos !t dt d 2r D ! 2 r0 cos !t !v0 sin !t D ! 2 r dt 2 ˇ d r ˇˇ D v0 : r.0/ D r0 ; ˇ dt ˇ tD0

Observe that r  .r0  v0 / D 0 for all t . Therefore the path lies in a plane through the origin having normal N D r0  v0 . Let us choose our coordinate system so that r0 D ai (a > 0) and v0 D !bi C !cj (c > 0). Therefore, N is in the direction of k. The path has parametric equations

26. If r  v > 0 then jrj is increasing. (See Exercise 16 above.) Thus r is moving farther away from the origin. If r v < 0 then r is moving closer to the origin.   d 2u d 2u d u d 3u d d u d 2u 27.  2 D  2 C  3 2 dt dt dt dt dt dt dt d u d 3u  3: D dt dt   d 28. u  .v  w/ dt D u0  .v  w/ C u  .v0  w/ C u  .v  w0 /: 29.

i d h .u C u00 /  .u  u0 / dt D .u0 C u000 /  .u  u0 / C .u C u00 /  .u0  u0 / C .u C u00 /  .u  u00 / D u000  .u  u0 /: i d h .u  u0 /  .u0  u00 / dt D .u0  u0 /  .u0  u00 / C .u  u00 /  .u0  u00 / C .u  u0 /  .u00  u00 / C .u  u0 /  .u0  u000 / D .u  u00 /  .u0  u00 / C .u  u0 /  .u0  u000 /:

r.t / D r.0/e 2t D r0 e 2t ; dv dr a.t / D D2 D 4r0 e 2t : dt dt

d d 2 jrj D r  r D 2r  v D 0 implies that jrj is constant. dt dt Thus r.t / lies on a sphere centred at the origin. d jr dt

31.

x D a cos !t C b sin !t y D c sin !t: The curve is a conic section since it has a quadratic equation:   by 2 y 2 1 C 2 D 1: x a2 c c Since the path is bounded (jr.t /j  jr0 j C .jv0 j=!/), it must be an ellipse. If r0 is perpendicular to v0 , then b D 0 and the path is the ellipse .x=a/2 C .y=c/2 D 1 having semi-axes a D jr0 j and c D jv0 j=!. 35.

d 2r D dt 2

gk

r.0/ D r0 ;

dr dtˇ d r ˇˇ ˇ dt ˇ

c

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tD0

D v0 :

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INSTRUCTOR’S SOLUTIONS MANUAL

Let w D e ct

SECTION 11.2

dr . Then dt

2.

dr d 2r dw D ce ct C e ct 2 dt dt dt dr ct ct d r e gk ce ct D ce dt dt D e ct gk Z e ct w.t / D e ct gk dt D gk C C: c

e ct

Let v.t / be the speed of the tank car at time t seconds. The mass of the car at time t is m.t / D M k t kg. At full power, the force applied to the car is F D Ma (since the motor can accelerate the full car at a m/s2 ). By Newton’s Law, this force is the rate of change of the momentum of the car. Thus d h .M dt

.M

g k C C, so c

Put t D 0 and get v0 D

1

e c

ct

g .ct C e c2

v0

kv D

c!0

c!0

D r0 C v0 t D r0 C v0 t

ct

te

gk lim

1

t 2e gk lim c!0 2 1 2 gt k; 2

t

te 2c

c!0 ct

Ma D

Mak t : M kt

Mat m/s: M kt

3.

dr D k  r, r.0/ D i C k. dt Let r.t / D x.t /i C y.t /j C z.t /k. Then x.0/ D z.0/ D 1 and y.0/ D 0. Since k  .d r=dt / D k  .k  r/ D 0, the velocity is always perpendicular to k, so z.t / is constant: z.t / D z.0/ D 1 for all t . Thus

Given:

dx dy dr iC jD D k  r D xj dt dt dt

yi:

Separating this equation into components, ln



 m.0/ ve : m.T /

dx D dt

If v.0/ D 0 and v.T / D ve then ln.m.0/=m.T // D 1 and m.T / D .1=e/m.0/. The rocket must therefore burn e 1 fraction of its initial mass to accelerate to the speed e of its exhaust gases. Similarly, if v.T / D

1 ln C k

ct

It was shown in the text that v.0/ D

M 2a M kt

v.t / D

Section 11.2 Some Applications of Vector Differentiation (page 642)

v.T /

kt/ C

1/k:

which is the solution obtained in Example 4.

1.

kv D Ma

The speed of the tank car at time t (before it is empty) is

ct

The limit of this solution, as c ! 0, is calculated via l’H^opital’s Rule: lim r.t / D r0 C v0 lim

dv dt

At t D 0 we have v D 0, so Ma D C =M . Thus C D M 2 a and

Thus we have r D r0 C

kt/

i k t /v D Ma

dv dt D Ma C kv M kt 1 1 ln.Ma C kv/ D ln.M k k C Ma C kv D : M kt

g dr D w D v0 C .1 e ct /k dt c dr g ct D e v0 .1 e ct /k dt c   e ct g e ct rD v0 tC kCD c c c g 1 k C D: v0 r0 D r.0/ D c c2

(PAGE 642)

2

2ve , then m.T / D .1=e /m.0/, so e2 1 the rocket must burn fraction of its initial mass to e2 accelerate to twice the speed of its exhaust gases.

y;

dy D x: dt

Therefore, d 2x D dt 2

dy D x; dt

and x D A cos t C B sin t . Since x.0/ D 1 and y.0/ D 0, we have A D 1 and B D 0. Thus x.t / D cos t and y.t / D sin t . The path has equation

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r D cos t i C sin t j C k:

423

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SECTION 11.2 (PAGE 642)

ADAMS and ESSEX: CALCULUS 9

Remark: This result also follows from comparing the given differential equation with that obtained for circular motion in the text. This shows that the motion is a rotation with angular velocity k, that is, rotation about the z-axis with angular speed 1. The initial value given for r then forces r D cos t i C sin t j C k:

6.

4. First observe that d jr dt

bj2 D 2.r

b/ 

dr D 2.r dt

 b/  a  .r

 b/ D 0;

I K V D R p : 2 The angular velocity of the earth is  D .=12/K.

so jr bj is constant; for all t the object lies on the sphere centred at the point with position vector b having radius r0 b. Next, observe that d .r dt

 r0 /  a D a  .r

We use the fixed and rotating frames as described in the text. Assume the satellite is in an orbit in the plane spanned by the fixed basis vectors I and K. When the satellite passes overhead an observer at latitude 45ı , its position is ICK RDR p ; 2 where R is the radius of the earth, and since it circles the earth in 2 hours, its velocity at that point is

The rotating frame with origin at the observer’s position has, at the instant in question, its basis vectors satisfying ID

 b/  a D 0;

JDi

1 1 K D p j C p k: 2 2

so r r0 ? a; for all t the object lies on the plane through r0 having normal a. Hence the path of the object lies on the circle in which this plane intersects the sphere described above. The angle between r b and a must therefore also be constant, and so the object’s speed jd r=dt j is constant. Hence the path must be the whole circle.

As shown in the text, the velocity v of the satellite as it appears to the observer is given by V D v C   R. Thus vD V R R pi R K  p .I C K/ D p .I K/ 12 2 2 R R p J D p .I K/ 2 12 2 R p i: D Rj 12 2

5. Use a coordinate system with origin at the observer, i pointing east, and j pointing north. The angular velocity of the earth is 2=24 radians per hour northward:

D

 j: 12

Because the earth is rotating west to east, the true north to south velocity of the satellite will appear to the observer to be shifted to the west by R=12 km/h, where R is the radius of the earth in kilometres. Since the satellite circles the earth at a rate of  radians/h, its velocity, as observed at the moving origin, is vR D

Rj

v makes angle p ! p 1 R=12 2 tan D tan 1 .1=.12 2/  3:37ı with R the southward direction. Thus the satellite appears to the observer to be moving in a direction 3:37ı west of south. The apparent Coriolis force is   R R  p J 2  v D 2 K  p .I K 12 2 12 2    2R 1 D p JC I 12 6 2   1  2R p i C p . j C k/ : D 6 2 12 2

R i: 12

 R=12 D tan 1 .1=12/  4:76ı R with the southward direction. Thus the satellite appears to the observer to be moving in a direction 4:76ı west of south. vR makes angle tan

1



The apparent Coriolis force is 2  vR D

2 j 12



7. Rj

 R i D 12

which is pointing towards the ground.

424

2R k; 72

1 1 p jC p k 2 2

The angular velocity of the earth is , pointing due north. For a particle moving with horizontal velocity v, the tangential and normal components of the Coriolis force C, and of , are related by CT D

2N  v;

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CN D

2T  v:

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 11.3

At the north or south pole, T D 0 and N D . Thus CN D 0 and CT D 2  v. The Coriolis force is horizontal. It is 90ı east of v at the north pole and 90ı west of v at the south pole.

Section 11.3 Curves and Parametrizations (page 649) 1.

At the equator, N D 0 and T D . Thus CT D 0 and CN D 2  v. The Coriolis force is vertical. 8. We continue with the same notation as in Example 4. Since j points northward at the observer’s position, the angle  between the direction vector of the sun, S D cos I C sin J and north satisfies cos  D S  j D

On the first quadrant part of the circle x 2 C y 2 D a2 p we have x D a2 y 2 , 0  y  a. The required parametrization is p r D r.y/ D a2 y 2 i C yj; .0  y  a/:

2.

On the first quadrant part of the circle x 2 C y 2 D a2 p we have y D a2 x 2 , 0  x  a. The required parametrization is p r D r.x/ D xi C a2 x 2 j; .0  x  a/:

3.

From the figure we see that

cos  cos  cos  C sin  sin :

For the sun,  D 0 and at sunrise and sunset we have, by Example 4, cos  D tan = tan , so that

  ; 0  2 2   D a sin  x D a cos  D a cos  2   y D a sin  D a sin  D a cos : 2 DC

tan  C sin  sin  tan  2 cos  C sin  sin  D sin  sin  sin  : D sin 

cos  D cos  cos 

The required parametrization is r D a sin i

1



tan 23:3ı tan 40:8ı



cos

1

ı

sin 23:3 sin 40:8ı

.x;y/

 16 



a

4.

tan 23:3ı tan 26:5ı



s s s  x D a sin ; y D a cos ; 0  a a  a 2 s a s 0s r D a sin i C a cos j; : a a 2 y

1



sin 23:3ı sin 26:5ı



s

a

 20

hours between sunrise and sunset. By Exercise 8, the sun will rise and set at an angle cos

x

Fig. 11.3-3

10. At Umea,  D 90ı 63:5ı D 26:5ı . On June 21st,  D 23:3ı . By Example 4 there will be 1



 52:7ı

to the east and west of north.

24 cos 

2

  :

a

hours between sunrise and sunset. By Exercise 8, the sun will rise and set at an angle 



a cos j;

y

9. At Vancouver,  D 90ı 49:2ı D 40:8ı . On June 21st,  D 23:3ı . Ignoring the mountains and the rain, by Example 4 there will be 24 cos 

(PAGE 649)

.x;y/

s a

 27:6ı

a

x

Fig. 11.3-4

to the east and west of north.

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425

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SECTION 11.3 (PAGE 649)

ADAMS and ESSEX: CALCULUS 9

5. z D x 2 , z D 4y 2 . If t D y, then z D 4t 2 , so x D ˙2t . The curve passes through .2; 1; 4/ when t D 1, so x D 2t . The parametrization is r D 2t i C t j C 4t 2 k. 6. z D x 2 , x C y C z D 1. If t D x, then z D t 2 and y D 1 t t 2 . The parametrization is r D t i C .1 t t 2 /j C t 2 k.

12. By symmetry, the centre of the circle C of intersection of the plane x C y C z D 1 and the sphere x 2 C y 2 C z 2 D 1 must lie on the plane and must have its three coordinates equal. Thus the centre has position vector r0 D

z D x C y, x 2 C y 2 D 9. One possible parametrization is r D 3 cos t i C 3 sin t j C 3.cos t C sin t /k. p 8. x C y D 1, z D 1 x 2 y 2 . If x D t , then y D 1 t and p p z D 1 t 2 .1 t /2 D 2.t t 2 /. One possible parametrization is 7.

p t /j C 2.t

r D t i C .1 9. z D x 2 C y 2 , 2x 4y z on the vertical cylinder

.x

Since C passes through the point .0; 0; 1/, its radius is s 

4y

2

0

2

 C 0

1 3

2

 C 1

v2 D .i C j C k/  .i

1 3

2

D

r

2 : 3

j/ D i C j

2k:

Two perpendicular unit vectors that are parallel to the plane of C are

that is

1;

1 3

Any vector v that satisfies v  .i C j C k/ D 0 is parallel to the plane x C y C z D 1 containing C. One such vector is v1 D i j. A second one, perpendicular to v1 , is

t 2 /k:

1 D 0. These surfaces intersect

x 2 C y 2 D 2x

1 .i C j C k/: 3

2

i j vO 1 D p ; 2

1/ C .y C 2/ D 4:

vO 2 D

i C j 2k : p 6

One possible parametrization is Thus one possible parametrization of C is x D 1 C 2 cos t y D 2 C 2 sin t z D 1 C 2.1 C 2 cos t / 4. 2 C 2 sin t / D 9 C 4 cos t 8 sin t r D .1 C 2 cos t /i 2.1 sin t /j C .9 C 4 cos t 8 sin t /k: 10. yz C x D 1, xz x D 1. One possible parametrization is x D t , z D .1 C t /=t , and y D .1 t /=z D .1 t /t =.1 C t /, that is, 1Ct t t2 jC k: r D ti C 1Ct t 11.

2 .cos t vO 1 C sin t vO 2 / 3 cos t iCjCk sin t C p .i j/ C .i C j D 3 3 3

r D r0 C

13.

z 2 D x 2 C y 2 , z D 1 C x.

2 2 2 a) If t D x, then p z D 1 C t , so 1 C 2t C t D t C y , and y D ˙ 1 C 2t . Two parametrizations are needed to get the whole parabola, one for y  0 and one for y  0.

t2

1 2

i C tj C

14.

2

r D t i C t j C t k; .0  t  T / p p v D 1 C .2t /2 C 9t 4 D .1 C 3t 2 /2 p if 42 D 6, that is, if  D ˙ 3=2. In this case, the length of the curve is

t2 C 1 k: 2

2 2 c) If t D z, then 2t C 1 C y 2 , p x D t 1 and t D t so y D ˙ 2t 1. Again two parametrizations are needed to get the whole parabola.

3

s.T / D

15.

426

r D t 2 i C t 2 j C t 3 k; .0  t  1/ p p v D .2t /2 C .2t /2 C .3t 2 /2 D t 8 C 9t 2 Z 1 p t 8 C 9t 2 dt Let u D 8 C 9t 2 Length D 0 du D 18t dt ˇ17 p p ˇ 17 17 16 2 1 2 3=2 ˇ u ˇ D units. D ˇ 18 3 27

2k/:

8

b) If t D y, then x 2 C t 2 D z 2 D 1 C 2x C x 2 , so 2x C 1 D t 2 , and x D .t 2 1/=2. Thus z D 1 C x D .t 2 C 1/=2. The whole parabola is parametrized by rD

r

Length D D

Z

Z

T 1 T 1

Z

T 0

ˇ ˇ ˇdrˇ ˇ ˇ dt ˇ dt ˇ s

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.1 C 3t 2 / dt D T C T 3 :

4a2 t 2 C b 2 C

c2 dt units. t2

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 11.3

If b 2 D rthen Z T4ac c 2 Length D dt 2at C t 1 Z T c D dt 2at C t 1 D a.T 2 1/ C c ln T units.

Since the first octant part of C lies in the plane y D z, it must be a quarter of a circle of radius 1. Thus the length of all of C is 8  .=2/ D 4 units. If you wish to use an integral, the length is Z =2 r 1 1 sin2 t C cos2 t C cos2 t dt 8 2 2 0 Z =2 dt D 4 units. D8

a 16. x D a cos t sin t D sin 2t , 2 a y D a sin2 t D .1 cos 2t /, 2 z D bt . The curve is a circular helix lying on the cylinder 2



x C y

(PAGE 649)

0

z

x2 C y2 C z2 D 1 x 2 C 2z 2 D 1

a 2 a2 : D 2 4

C

Its length, from t D 0 to t D T , is LD

Z

T 0

p a2 cos2 2t C a2 sin2 2t C b 2 dt

y x

p D T a2 C b 2 units.

Fig. 11.3-18 19.

17.

r D t cos t i C t sin t j C t k; 0  t  2 v D .cos t t sin t /i C .sin t C t cos t /j C k p p v D jvj D .1 C t 2 / C 1 D 2 C t 2 : The length of the curve is LD

Z

D2

2

0

Z

p 2 C t 2 dt

tD2

x D e t cos t;

p Let t D 2 tan  p dt D 2 sec2  d

sec3  d

tD0

 ˇˇtD2 D sec  tan  C ln j sec  C tan  j ˇˇ tD0

!ˇ2 p p 2 C t2 t 2 C t2 t ˇˇ p D C ln Cp ˇ 2 2 2 ˇ0 p p p  D  2 C 4 2 C ln 1 C 2 2 C 2 units. The curve is called a conical helix because it is a spiral lying on the cone x 2 C y 2 D z 2 . 18. One-eighth of the curve C lies in the first octant. That part can be parametrized x D cos t; r yD

1

If C is the curve

1 z D p sin t; .0  t  =2/ 2 1 2 1 cos2 t sin t D p sin t: 2 2

y D e t sin t;

z D t;

.0  t  2/;

then the length of C is s Z 2  2  2  2 dy dz dx C C dt LD dt dt dt 0 Z 2 p e 2t .cos t sin t /2 C e 2t .sin t C cos t /2 C 1 dt D 0 Z 2 p D 2e 2t C 1 dt Let 2e 2t C 1 D v 2 0 2e 2t dt D v dv  Z tD2 2 Z tD2  v dv 1 D D dv 1 C v2 1 v2 1 tD0 tD0 ˇ ˇˇtD2  1 ˇ v 1 ˇˇ ˇˇ D v C ln ˇˇ ˇ 2 v C 1ˇ ˇ tD0 ˇ2 p p p 1 2e 2t C 1 1 ˇˇ 3 C ln p D 2e 4 C 1 ˇ 2 2e 2t C 1 C 1 ˇ0 ˇ2 p p p 2e 2t C 1 1 ˇˇ 3 C ln p D 2e 4 C 1 ˇ ˇ 2e t 0   p p p 4 4 D 2e C 1 3 C ln 2e C 1 1 p 2 ln. 3 1/ units. Remark: This answer appears somewhat different from that given in the answers section of the text. The two are, however, equal. Somewhat different simplifications were used in the two.

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SECTION 11.3 (PAGE 649)

20.

ADAMS and ESSEX: CALCULUS 9

r D t 3i C t 2j

v D 3t 2 i C 2t j p p v D jvj D 9t 4 C 4t 2 D jt j 9t 2 C 4

The length L between t D LD

Z

0 1

2a cos 

L

1 and t D 2 is

Z p 2 . t / 9t C 4 dt C

2

t

0

p

a a

9t 2 C 4 dt:

 2.a C b/ one revolution

Making the substitution u D 9t 2 C 4 in each integral, we obtain Z

Z

13

40

1 u1=2 du C 18 4 4  1  3=2 3=2 D 13 C 40 16 27

LD

21.

Fig. 11.3-22 Observe that tan  D

 u1=2 du

sin  D

units.

cos  D

2a 1  . Therefore cos  2.a C b/

a .a C b/ s

a2 D 2  .a C b/2

1

p  2 .a C b/2 .a C b/

a2

:

The total length of spool required is

r1 D t i C t j, .0  t  1/ represents the straight line segment from the origin to .1; 1/ in the xy-plane.

H D L sin  C 2a cos   p a L C 2  2 .a C b/2 D .a C b/

r2 D .1 t /i C .1 C t /j, .0  t  1/ represents the straight line segment from .1; 1/ to .0; 2/. Thus C D C1 C C2 is the 2-segment polygonal line from the origin to .1; 1/ and then to .0; 2/.

L sin 

2a cos 

23.

22. (Solution due to Roland Urbanek, a student at Okanagan College.) Suppose the spool is vertical and the cable windings make angle  with the horizontal at each point.

a2



units.

r D At i C Bt j C C t k. The arc length from the point where t D 0 to the point corresponding to arbitrary t is s D s.t / D

Z tp p A2 C B 2 C C 2 du D A2 C B 2 C C 2 t: 0

p Thus t D s= A2 C B 2 C C 2 : The required parametrization is Asi C Bsj C C sk : rD p A2 C B 2 C C 2

24. H  2a b

p r D e t i C p2t j e t k t v D e i C p2j C e t k v D jvj D e 2t C 2 C e 2t D e t C e t : The arc length from the point where t D 0 to the point corresponding to arbitrary t is s D s.t / D

a

Z

t 0

.e u C e

Fig. 11.3-22 The centreline of the cable is wound around a cylinder of 2a in radius a C b and must rise a vertical distance cos  one revolution. The figure below shows the cable unwound from the spool and inclined at angle  . The total length of spool required is the total height H of the cable as shown in that figure.

428

Thus t D sinh

1

p

.s=2/ D ln

u

/ du D e t sC

e

t

D 2 sinh t:

! s2 C 4 , 2

p

s2 C 4 . The required parametrization is 2 ! p p s C s2 C 4 p 2k s C s2 C 4 iC 2 ln rD j p : 2 2 s C s2 C 4 and e t D

sC

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INSTRUCTOR’S SOLUTIONS MANUAL

25.

r D a cos3 t i C a sin3 t j C b cos 2t k;

 2 4b sin t cos t k

ds D g 0 .t / D jv.t /j > 0 dt on Œa; b, by the Fundamental Theorem of Calculus. Hence g is invertible, and defines t as a function of arc length s: t D g 1 .s/ , s D g.t /:

0

1p 2 9a C 16b 2 sin2 t D K sin2 t D 2 1p 2 where K D 9a C 16b 2 2 r r s s , cos t D 1 , Therefore sin t D K K 2s . cos 2t D 1 2 sin2 t D 1 K The required parametrization is  rDa 1

Then

27.

  s 3=2 s 3=2 iCa Cb 1 K K

2s K



k

p p t sin t /i C 3.sin t C t cos t /j C 3 2 t k

p v D jvj D 3 1 C t 2 C 2t D 3.1 C t /   Z t t2 3.1 C u/ du D 3 t C sD 2 0 r 2s 2s 2 , so t D 1 C 1 C since t  0. Thus t C 2t D 3 3 The required parametrization is the given one with t rep placed by 1 C 1 C .2s/=3.

As claimed in the statement of the problem, r1 .t / D r2 u.t / , where u is a function from Œa; b to Œc; d , having u.a/ D c and u.b/ D d . We assume u is differentiable. Since u is one-to-one and orientationpreserving, du=dt  0 on Œa; b. By the Chain Rule:

1.

a

ˇ Z d  ˇˇ bˇ ˇ d r2 u.t / ˇ du dt D ˇ dt ˇ du a c

ˇ ˇ ˇ ˇ d ˇ r2 .u/ˇ du: ˇ ˇ du

28. If r D r.t / has nonvanishing velocity v D d r=dt on Œa; b, then for any t0 in Œa; b, the function s D g.t / D

Z

t t0

jv.u/j du;

 .s/

r D ti

2t 2 j C 3t 3 k

v D i 4t j C 9t 2 k p v D 1 C 16t 2 C 81t 4

i 4t j C 9t 2 k v TO D D p : v 1 C 16t 2 C 81t 4 2.

3.

4.

and so ˇ ˇ Z bˇ ˇ ˇ d r1 .t /ˇ dt D ˇ ˇ dt

1

Section 11.4 Curvature, Torsion, and the Frenet Frame (page 658)

d du d r1 .t / D r2 .u/ ; dt du dt

Z

 r D r2 .s/ D r g

is a parametrization of the curve r D r.t / in terms of arc length.

1p 2 9a C 16b 2 . for 0  s  K, where K D 2 p 26. r D 3t cos t i C 3t sin t j C 2 2t 3=2 k; .t  0/ v D 3.cos t

(PAGE 658)

which gives the (signed) arc length s measured from r.t0 / along the curve, is an increasing function:

0t 

3a cos2 t sin t i C 3a sin2 t cos t j p v D 9a2 C 16b 2 sin t cos t Z tp sD 9a2 C 16b 2 sin u cos u du vD

SECTION 11.4

5.

6.

r D a sin !t i C a cos !t k v D a! cos !t i a! sin !t k; v D ja!j h i TO D sgn.a!/ cos !t i sin !t k :

r D cos t sin t i C sin2 t C cos t k 1 1 D sin 2t i C .1 cos 2t /j C cos t k 2 2 v D cos 2t i C sin 2t j sin t k p v D jvj D 1 C sin2 t   1 TO D p cos 2t i C sin 2t j sin t k : 1 C sin2 t r D a cos t i C b sin t j C t k v D a sin t i C b cos t j C k p v D a2 sin2 t C b 2 cos2 t C 1 a sin t i C b cos t j C k v : TO D D p v a2 sin2 t C b 2 cos2 t C 1

d TO O D 0, so D N ds dr O O O T.s/ D T.0/ is constant. This says that D T.0/, so ds O r D T.0/s C r.0/, which is the vector parametric equation of a straight line. If .s/ D 0 for all s, then

If .s/ D 0 for all s, then O dB O D 0, so B.s/ O O D N D B.0/ is constant. Therefore, ds  dr O d  O O O  B.s/ D T.s/  B.s/ D 0: r.s/ r.0/  B.s/ D ds ds

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ADAMS and ESSEX: CALCULUS 9

It follows that    O r.s/ r.0/  B.0/ D r.s/

for all s. This says that r.s/ lies in the plane through r.0/ O having normal B.0/. 7.

Hence .0/ D 1 and .=2/ D 0. The radius of curvature at x D 0 is 1. The radius of curvature at x D =2 is infinite.

 O r.0/  B.s/ D0 3.

The circle C1 given by

r D 2t i C .1=t /j

v D 2i

.1=t 2 /j

2t k 2k

a D .2=t 3 /j

1 1 rD cos C si C sin C sj C C

v  a D .4=t 3 /i C .4=t 3 /k At .2; 1; 2/, that is, at t D 1, we have

is parametrized in terms of arc length, and has curvature C and torsion 0. (See Examples 2 and 3.) If curve C has constant curvature .s/ D C and constant torsion .s/ D 0, then C is congruent to C1 by Theorem 3. Thus C must itself be a circle (with radius 1=C ).

 D .1/ D

p jv  aj 4 2 D : v3 27

p Thus the radius of curvature is 27=.4 2/.

8. The circular helix C1 given by r D a cos t i C a sin t j C bt k

4.

has curvature and torsion given by .s/ D

a ; a2 C b 2

.s/ D

v D 3t 2 i C 2t j C k a D 6t i C 2j v.1/ D 3i C 2j C k; a.1/ D 6i C 2j v.1/  a.1/ D 2i C 6j 6k p p 2 19 4 C 36 C 36 D 3=2 .1/ D .9 C 4 C 1/3=2 14 p At t D 1 the radius of curvature is 143=2 =.2 19/.

b ; a2 C b 2

by Example 3. if a curve C has constant curvature .s/ D C > 0, and constant torsion .s/ D T ¤ 0, then we can choose a and b so that a D C; a2 C b 2

b D T: a2 C b 2

5.

r D t i C t 2 j C 2k v D i C 2t j a D 2j v  a D 2k At .1; 1; 2/, where t D 1, we have p TO D v=jvj D .i C 2j/= 5 BO D .v  a/=jv  aj D k p O D BO  TO D . 2i C j/= 5: N

6.

r D t i C t 2j C t k v D i C 2t j C k a D 2j v  a D 2i C 2k At .1; 1; 1/, where t D 1, we have p TO D v=jvj D .i C 2j C k/= 6 p BO D .v  a/=jv  aj D .i k/= 2 p O D BO  TO D .i j C k/= 3: N

T C , and b D 2 .) By C2 C T 2 C CT2 Theorem 3, C is itself a circular helix, congruent to C1 .

(Specifically, a D

Section 11.5 Curvature and Torsion for General Parametrizations (page 664) 1.

For y D x 2 we have .x/ D

jd 2 y=dx 2 j 2 D : .1 C .dy=dx/2 /3=2 .1 C 4x 2 /3=2

p Hence .0/ D 2 and . 2/ p D 2=27. The radii of curvature at x D 0 and x D 2 are 1=2 and 27=2, respectively. 2. For y D cos we have .x/ D

430

jd 2 y=dx 2 j j cos xj : D .1 C .dy=dx/2 /3=2 .1 C sin2 x/3=2

r D t 3i C t 2j C t k

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INSTRUCTOR’S SOLUTIONS MANUAL

7.

t3 t2 jC k 2 3 v D i C t j C t 2k da D 2k a D j C 2t k; dt 2 v  a D t i 2t j C k p v D jvj D 1 C t 2 C t 4 ; da .v  a/  D2 dt

SECTION 11.5

9.

r D ti C

jv  aj D

p

1 C 4t 2 C t 4

i C t j C t 2k O D v D p T v 1 C t2 C t4 v  a t 2 i 2t j C k O D B D p jv  aj 1 C 4t 2 C t 4 3 C t /i C .1 t 4 /j C .t 3 C 2t /k O DB O  TO D .2t N p .1 C t 2 C t 4 /.1 C 4t 2 C t 4 / p 1 C 4t 2 C t 4 jv  aj D D 3 v .1 C t 2 C t 4 /3=2 da .v  a/  2 dt D D : jv  aj2 1 C 4t 2 C t 4

8.

r D e t cos t i C e t sin t j C e t k v D e t .cos t sin t /i C e t .sin t C cos t /j C e t k a D 2e t sin t i C 2e t cos t j C e t k da D 2e t .cos t C sin t /i C 2e t .cos t sin t /j C e t k dt v  a D e 2t .sin t cos t /i e 2t .cos t C sin t /j C 2e 2t k p p jv  aj D 6e 2t v D jvj D 3e t ; da .v  a/  D 2e 3t dt v .cos t sin t /i C .cos t C sin t /j C k p TO D D v 3 .sin t cos t /i .cos t C sin t /j C 2k v  a p D BO D jv  aj 6 .cos t C sin t /i .cos t sin t /j O D BO  T O D p N 2 p 2 jv  aj D t D v3 3e da .v  a/  dt D 1 : D 2 jv  aj 3e t

10.

p r D .2 C 2 cos t /i C .1 sin t /j C .3 C sin t /k p 2 sin t i cos t j C cos t k vD p p v D 2 sin2 t C cos2 t C cos2 t D 2 p aD 2 cos t i C sin t j sin t k p da D 2 sin t i C cos t j cos t k dt p p 2j 2k va D 1 jv  aj 2 D D p D p v3 2 2 2 p p da .v  a/  2 cos t C 2 cos t D 0 D dt  D 0: p Since  D 1= 2 is constant, and  D 0, thepcurve is a circle. Its centre is .2; 1; 3/ andpits radius is 2. It lies in O 2B/. a plane with normal j C k.D

r D xi C sin xj dx dx vD i C cos x j D k.i C cos xj/ dt dt p v D k 1 C cos2 x dx a D k sin x j D k 2 sin xj dt v  a D k 3 sin xk j sin xj jv  aj D : D v3 .1 C cos2 x/3=2 The tangential and normal components of acceleration are k dx dv D p 2 cos x/. sin x/ D 2 dt dt 2 1 C cos x k 2 j sin xj : v2 D p 1 C cos2 x

11.

(PAGE 664)

k 2 cos x sin x p 1 C cos2 x

r D sin t cos t i C sin2 t j C cos t k v D cos 2t i C sin 2t j sin t k a D 2 sin 2t i C 2 cos 2t j cos t k da D 4 cos 2t i 4 sin 2t j C sin t k: dt At t D 0 we have v D i, a D 2j

k,

da D dt

da v  a D j C 2k, .v  a/  D 0. dtp O D .2j O O ThuspT D i, B D .j C 2k/= 5, N  D 5, and  D 0.

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4i,

p k/= 5,

431

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SECTION 11.5 (PAGE 664)

ADAMS and ESSEX: CALCULUS 9

1 1 p k, a D 2i p k, 2 2 p 1 1 da D 4j C p k, v  a D p i C 2j C 2k, dt 2 2 p da .v  a/  D 3 2. dt Thus p O D p1 . 2j k/ T 3 p 1 O D p . i C 2j C 2 2k/ B 13 p O D p1 .6i C j C 2k/ N 39 p p 2 39 6 2 D ; D : 9 13

The rate of change of the speed, dv=dt , is the tangential component of the acceleration, and is due entirely to the tangential component of the gravitational force since there is no friction:

At t D =4 we have v D j

12.

dv O D g cos  D g. j/  T; dt O and j. (See the figwhere  is the angle between T ure.) Since the p slope of y D x 2 at .1; 1/ is 2, p we have O D .i C 2j/= 5, and therefore dv=dt D 2g= 5. T y

r D a cos t i C b sin t j v D a sin t i C b cos t j a D a cos t i b sin t j v  a D abk p v D a2 sin2 t C b 2 cos2 t :

.1; 1/  gj dv O T dt

The tangential component of acceleration is .a2 b 2 / sin t cos t dv D p ; dt a2 sin2 t C b 2 cos2 t

15.

Curve: r D xi C e x j. p Velocity: v D i C e x j. Speed: v D 1 C e 2x . Acceleration: a D e x j. We have v  a D e x k;

jv  aj ab D p : 2 v3 2 a sin t C b 2 cos2 t

ex . Therefore, the radius .1 C e 2x /3=2 2x 3=2 .1 C e / . of curvature is  D ex The unit normal is

ab .a2 sin2 t C b 2 cos2 t /3=2 ab D  3=2 : .a2 b 2 / sin2 t C b 2

D

x O DB O  TO D .v  a/  v D p e i C j : N j.v  a/  vj 1 C e 2x

The centre of curvature is

If a > b > 0, then the maximum curvature occurs when sin t D 0, and is a=b 2 . The minimum curvature occurs when sin t D ˙1, and is b=a2 .

O rc D r C N

xD1

2 D p : 5 5

1

iC



This is the equation of the evolute. 16.

Thus the magnitude of the normal p acceleration of the bead at that point is v 2  D 2v 2 =.5 5/.

432

D .x



1 j ex e 2x /i C .2e x C e x /j:

D xi C e x j C .1 C e 2x /

By Example 2, the curvature of y D x 2 at .1; 1/ is ˇ ˇ 2 ˇ D ˇ 2 3=2 .1 C 4x / ˇ

jv  aj D e x :

The curvature is  D

13. The ellipse is the same one considered in Exercise 16, so its curvature is

14.

x

Fig. 11.5-14

which is zero if t is an integer multiple of =2, that is, at the ends of the major and minor axes of the ellipse. The normal component of acceleration is v2 D v2

y D x2

O v2 N

The curve with polar equation r D f . / is given parametrically by r D f . / cos  i C f . / sin  j:

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 11.5

Thus we have   v D f 0 . / cos  f . / sin  i   C f 0 . / sin  C f . / cos  j   a D f 00 . / cos  2f 0 . / sin  f . / cos  i   C f 00 . / sin  C 2f 0 . / cos  f . / sin  j r  2  2 f 0 . / C f . / v D jvj D h  2  2 i v  a D 2 f 0 . / C f . / f . /f 00 . / k: The curvature is, therefore,  2  2 j2 f 0 . / C f . / f . /f 00 . /j : h 2  2 i3=2 f 0 . / C f . /

17.

Therefore r.t / D

3a2 .1

2a2 .1

cos  / 3 : 3=2 D p 2 2ar cos  /

r.t / D

19.

Given that

20.

 1 t C sin t p C1 iC 2 2

t sin t cos t p k: jC 2 2 2

dr D c  r.t /, we have dt

For r D a cos t i C a sin t j C bt k, we have, by Example 3 of Section 2.4, O D N

cos t i

sin t j;

D

a : a2 C b 2

The centre of curvature rc is given by

for some right-handed basis fi1 ; j1 ; k1 g, and some constant vector r0 . Example 3 of Section 2.4 provides values for O O O T.0/, N.0/, and B.0/, which we can equate to the given values of these vectors:

O O D r C 1 N: rc D r C N  Thus the evolute has equation

1 1 O i D T.0/ D p j1 C p k1 2 2 O j D N.0/ D i1 1 1 O k D B.0/ D p j1 C p k1 : 2 2

r D a cos t i C a sin t j C bt k

D

Solving these equations for i1 , j1 , and k1 in terms of the given basis vectors, we obtain j 1 1 j1 D p i p k 2 2 1 1 k1 D p i C p k: 2 2



  Thus jr.t /j D jr.0/j is constant, and r.t / r.0/ c D 0 is constant. Thus r.t / lies on the sphere centred at the origin with radius jr.0/j, and also on the plane through r.0/ with normal c. The curve is the circle of intersection of this sphere and this plane.

1 1 1 cos t i1 C sin t j1 C t k1 C r0 2 2 2

i1 D

cos t t sin t p k C r0 : jC 2 2 2

d 2 d jrj D r  r D 2r  .c  r/ D 0 dt dt   d dr  c D .c  r/  c D 0: r.t / r.0/  c D dt dt

18. By Exercise 8 of Section 2.4, the required curve must be a circular helix with parameters a D 1=2 (radius), and b D 1=2. Its equation will be rD

t C sin t p i 2 2

1 We also require that r.0/ D i, so r0 D iC j. The required 2 equation is, therefore,

If r D a.1 cos  /, then r 0 D a sin  , and r 00 D a cos  . By the result of Exercise 20, the curvature of this cardioid is ˇ 1 ˇ 2 2 D  3=2  ˇ2a sin  2 a2 sin  C a2 .1 cos  /2 ˇ ˇ C a2 .1 cos  /2 a2 .cos  cos2  /ˇ D 

(PAGE 664)

a2 C b 2 .cos t i C sin t j/ a 2 b b2 cos t i sin t j C bt k: a a

The evolute is also a circular helix. 21.

The parabola y D x 2 has curvature D

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2 ; .1 C 4x 2 /3=2

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SECTION 11.5 (PAGE 664)

ADAMS and ESSEX: CALCULUS 9

by Exercise 18. The normal at .x; x 2 / is perpendicular to the tangent, so has slope 1=.2x/. Since the unit normal points upward (the concave side of the parabola), we have

The conditions at x D 1 become A C A C

O D p 2xi C j : N 1 C 4x 2

.1 C 4x 2 /3=2 2



p

2xi C j

1 C 4x 2 1 C 4x 2 D xi C x 2 j .1 C 4x 2 /xi C j 2   1 D 4x 3 i C 3x 2 C j: 2

C C C



15 x 8

f .x/ D

y

.1;1/

2 , so the radius of .3 sin2 t C 1/3=2 2 3=2 .3 sin t C 1/ curvature is  D . We have 2

x

yD 1 . 1; 1/

O Dk B

Fig. 11.5-23 24.

We require f .0/ D 1; f . 1/ D 1;

d2 p 1 dx 2

2

D

3 cos3 i 2

3 sin t C 1 .cos t i C 2 sin t j/ 2

As in Example 5, we try

f 00 .0/ D 1; f 00 . 1/ D 0:

1 follows from the fact that ˇ ˇ ˇ x2 ˇ ˇ

xD0

D

1:

3 sin3 t j: f .x/ D A C Bx C C x 2 C Dx 3 C Ex 4 C F x 5

f 0 .x/ D B C 2C x C 3Dx 2 C 4Ex 3 C 5F x 4

23. We require that f .1/ D 1; f . 1/ D 1;

0

f .1/ D 0; f 0 . 1/ D 0;

00

f .1/ D 0; f 00 . 1/ D 0:

f 00 D 2C C 6Dx C 12Ex 2 C 20F x 3 :

The required conditions force the coefficients to satisfy the system of equations

As in Example 5, we try a polynomial of degree 5. However, here it is clear that an odd function will do, and we need only impose the conditions at x D 1. Thus we try f .x/ D Ax C Bx 3 C C x 5

f 0 .x/ D A C 3Bx 2 C 5C x 4

f 00 .x/ D 6Bx C 20C x 3 :

434

f 0 .0/ D 0; f 0 . 1/ D 0;

The condition f 00 .0/ D

Therefore the evolute has equation r D 2 cos t i C sin t j

yD1

yDf .x/

The curvature is  D

O D N

5=4, and

is one possible solution.

v D 2 sin t i C cos t j a D 2 cos t i sin t j v  a D 2k p p v D 4 sin2 t C cos2 t D 3 sin2 t C 1:

2 sin t i C cos t j p ; 3 sin2 t C 1 cos t i C 2 sin t j p : 3 sin2 t C 1

1 0 0:

5 3 3 5 x C x 4 8

22. For the ellipse r D 2 cos t i C sin t j, we have

TO D

D D D

C 5C 20C

This system has solution A D 15=8, B D C D 3=8. Thus

Thus the evolute of the parabola has equation r D xi C x 2 j C

B 3B 6B

A B CC DCE F D1 B 2C C 3D 4E C 5F D 0 2C 6D C 12E 20F D 0 AD1 BD0 2C D 1

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 11.5

which has solution A D 1, B D 0, C D 1=2, D D 3=2, E D 3=2, F D 1=2. Thus we can use a track section in the shape of the graph of f .x/ D 1

1 2 x 2

3 3 x 2

3 4 x 2

1 5 x D1 2

This leads to the values p

.cos.t /2

1 2 x .1 C x/3 : 2

2 p C 1/ 2 cos.t /2 C 2

and

0

for the curvature and torsion, respectively. Maple doesn’t seem to recognize that the curvature simplifies to 1=.cos2 t C 1/3=2 . The torsion is zero because the curve is lies in the plane z D x. It is the ellipse in which this plane intersects the ellipsoid 2x 2 C y 2 C 2z 2 D 4. The maximum and minimum values of the curvature are 1 and 1=23=2 , respectively, at the ends of the major and minor axes of the ellipse.

y . 1;1/ yD1

(PAGE 664)

yDf .x/

x

27.

> > > > > > > > > > > > > >

x 2 Cy 2 D1

Fig. 11.5-24 25. Given: a.t / D .t /r.t / C .t /v.t /, v  a ¤ 0. We have v  a D v  r C v  v D v  r da D 0 r C v C 0 v C a dt D 0 r C . C 0 /v C .r C v/ D .0 C /r C . C 0 C 2 /v:

Since v  r is perpendicular to both v and r, we have .v  a/ 

da D 0: dt

R := t -> ; assume(t::real): interface(showassumed=0): V := t -> diff(R(t),t): A := t -> diff(V(t),t): v := t -> Norm(V(t),2): VxA := t -> V(t) &x A(t): vxa := t -> Norm(VxA(t),2): Ap := t -> diff(A(t),t): Curv := t -> simplify(vxa(t)/(v(t))^3): Tors := t -> simplify( (VxA(t).Ap(t))/(vxa(t))^2): Curv(t); Tors(t);

This leads to the values p cos.t /2 C 2 2 cos.t / .3 2 cos.t //3=2

Thus the torsion .t / of the curve is identically zero. It remains zero when expressed in terms of arc length: .s/ D 0. By Exercise 6 of Section 2.4, r.t / must be a plane curve.

and

26. After loading the LinearAlgebra and VectorCalculus packages, issue the following commands: > > > > > > > > > > > > > >

After loading the LinearAlgebra and VectorCalculus packages, issue the following commands:

R := t -> ; assume(t::real): interface(showassumed=0): V := t -> diff(R(t),t): A := t -> diff(V(t),t): v := t -> Norm(V(t),2): VxA := t -> V(t) &x A(t): vxa := t -> Norm(VxA(t),2): Ap := t -> diff(A(t),t): Curv := t -> simplify(vxa(t)/(v(t))^3): Tors := t -> simplify( (VxA(t).Ap(t))/(vxa(t))^2): Curv(t); Tors(t);

1 2 cos.t /2 C sin.t /2

2 cos.t / C 1

for the curvature and torsion, respectively. Each of these formulas can be simplified somewhat: p

2 2 cos t C cos2 t .3 2 cos t /3=2 1 Tors.t / D : 2 2 cos t C cos2 t

Curv.t / D

Since 3 2 cos t > 0 and 2 2 cos t C cos2 t D 1 C .1 cos t /2 > 0 for all t , the curvature and torsion are both continuous for all t . The curve appears to be some sort of helix (but not a circular one) with central axis along the line x D z, y D 1. 28.

After loading the LinearAlgebra and VectorCalculus packages, issue the following commands:

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SECTION 11.5 (PAGE 664)

ADAMS and ESSEX: CALCULUS 9

> R := t -> ; > assume(t::real): > interface(showassumed=0): > V := t -> diff(R(t),t): > A := t -> diff(V(t),t): > v := t -> Norm(V(t),2): > VxA := t -> V(t) &x A(t): > vxa := t -> Norm(VxA(t),2): > Ap := t -> diff(A(t),t): > Curv := t -> > simplify(vxa(t)/(v(t))^3): > Tors := t -> simplify( > (VxA(t).Ap(t))/(vxa(t))^2): > Curv(t); Tors(t); > simplify(%,trig);

This leads to the values p 2 cos.t /2 C cos t C 1 3=2 5 cos.t /2 C 2 cos t 1 Tors.t / D 2.cos.t /2 / C cos t C 1

Curv.t / D

This appears to be an elliptical helix with central axis along the line x D y D z 1. 30.

evolute := R -> (t -> R(t)+TNBFrame(R)[2](t) *(1/Curvature(R)(t)));

31.

tanline := R -> ((t,u) -> R(t)+TNBFrame(R)[1](t)*u);

The last line simplifies the rather complicated expression that Tors(t) returns by applying some trigonometric identities. The values for the curvature and torsion are p 17 C 60 cos.t /2 C 48 cos.t /4 Curv.t / D 3=2 4 cos.t /2 C 1 12 cos t .2 cos.t /2 C 3/ : Tors.t / D 17 C 60 cos.t /2 C 48 cos.t /4

Section 11.6 Kepler’s Laws of Planetary Motion (page 673)

1.

436

r C x D `

2`x C  2 x 2

 2 /x 2 C 2`x C y 2 D `2 2  `2 `2  2 ` 2 2 D C y D ` C .1  2 / x C 1 2 1 2 1 2  2 ` xC y2 1 2 2 D 1: 2 C   ` ` p 1 2 1 2

.1

The command simplify(Norm(R(t),2)); gives output 1, indicating that the curve lies on the sphere x 2 C y 2 C z 2 D 1.

> R := t -> ; > assume(t::real): > interface(showassumed=0): > V := t -> diff(R(t),t): > A := t -> diff(V(t),t): > v := t -> Norm(V(t),2): > VxA := t -> V(t) &x A(t): > vxa := t -> Norm(VxA(t),2): > Ap := t -> diff(A(t),t): > Curv := t -> > simplify(vxa(t)/(v(t))^3): > Tors := t -> simplify( > (VxA(t).Ap(t))/(vxa(t))^2): > Curv(t); Tors(t);

÷

x 2 C y 2 D r 2 D `2

Plotting the curvature as a function of t , (plot(Curv(t),t=-2*Pi..2*Pi)), shows that the minimum curvature occurs at t D 0 (and p any integer multiple of ). The minimum curvature is 125=53=2 D 1.

29. After loading the LinearAlgebra and VectorCalculus packages, issue the following commands:

` 1 C  cos  r D ` x

rD

2.

Position: r D r rO D k rO . Velocity: v D k rPO D k P O ; speed: v D k P . P Acceleration: k R O C k P O D k P 2 rO C k R O . Radial component of acceleration: k P 2 . Transverse component of acceleration: k R D vP (the rate of change of the speed).

3.

Position: on the curve r D e  . Radial velocity: rP D e  P . Transverse velocity: r P D e  P . p p  P Speed v D 2ep D 1 ÷ P D .1= 2/e  . Thus R D .1= 2/e  P D e 2 =2. p Radial velocity = transverse velocity D 1= 2. Radial acceleration: rR r P 2 D e  P 2 C e  R e  P 2 D e  R D e  =2. Transverse acceleration: r R C 2rP P D .e  /=2 C e  D e  =2.

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 11.6

4. Path: r D  .qThus rP D P , rR D R . p Speed: v D .Pr/2 C .r P /2 D P 1 C r 2 . Transverse acceleration = 0 (central force). Thus r R C 2rP P D 0, or R D 2P 2 =r. Radial acceleration: rR

r P 2 D R D



The satellite has a circular orbit of radius aS and period TS D 1 day. (If the orbit is in the plane of the equator, the satellite will remain above the same point on the earth.) By Kepler’s third law, TS2 aS3

r P 2

 2 C r P 2 D r

8.

r P 2 j:

For r D 

2

rP D Thus rR D

3

2

2hP D

P D 2

2

3

h D r2

2h:

:

The period T (in years) and radius R (in km) of the asteroid’s orbit satisfies

If R is the radius and T is the period of the asteroid’s circular orbit, then almost stopping the asteroid causes it to drop into a very eccentric elliptical orbit with major axis approximately R. (Thus, a D R=2.) The period Te of the new elliptical orbit satisfies Te2 .R=2/3 1 D D : T2 R3 8

2

2h =r . The speed v is given by

v 2 D rP 2 C r 2 P 2 D 4h2  2 C .h2 =r 2 /:

3 aM

Thus the radius of the asteroid’s orbit is R  150  106 T 2=3 km. 9.

, we have

2 TM

T2 T2 12 D D earth : 3 3 R .150  106 /3 Rearth

5. For a central force, r 2 P D h (constant), and the acceleration is wholly radial, so jaj D jRr

D

Thus aS D 385; 000  .1=27/2=3  42; 788. The satellite’s orbit should have radius about 42,788 km, and should lie in the equatorial plane.

.2 C r 2 /v 2 : r.1 C r 2 /

The magnitude of the acceleration is, therefore, .2 C r 2 /v 2 . r.1 C r 2 /

(PAGE 673)

p Thus Te D T =.2 2/. The time the asteroid will p take to fall into the sun is half of Te . Thus it is T =.4 2/.

Since the speed is v0 when pD 1 (and so r D 1), we have v02 D 5h2 , and h D v0 = 5. Hence the magnitude of the acceleration at any point on the path is ˇ ˇ h2 jaj D ˇˇ 2 2 r

r

6. Let the period and the semi-major axis of the orbit of Halley’s comet be TH D 76 years and aH km respectively. Similar parameters for the earth’s orbit are TE D 1 year and aE D 150  106 km. By Kepler’s third law TH2 3 aH

D

TE2 3 aE

:

Thus aH D 150  106  762=3  2:69  109 : The major axis of Halley’s comet’s orbit is 2aH  5:38  109 km. 7.

R

ˇ   v02 2 h2 ˇˇ 1 D C : r4 ˇ 5 r2 r3

Fig. 11.6-9 10. At perihelion, r D a c D .1 /a. At aphelion r D a C c D .1 C /a. Since rP D 0 at perihelion and aphelion, the speed is v D r P at each point. Since r 2 P D h is constant over the orbit, v D h=r. Therefore vperihelion D

/

vaphelion D

;

h : a.1 C /

If vperihelion D 2vaphelion then h

The period and semi-major axis of the moon’s orbit around the earth are TM  27 days,

h a.1

aM  385; 000 km.

a.1 Hence 1 C  D 2.1 the orbit is 1/3.

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/

D

2h : a.1 C /

/, and  D 1=3. The eccentricity of

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SECTION 11.6 (PAGE 673)

11.

ADAMS and ESSEX: CALCULUS 9

The orbital speed v of a planet satisfies (by conservation of energy) v2 2

k DK r

14.

(total energy).

If v is constant so must be r, and the orbit will therefore be circular.

As in Exercise 12, rP vP D rA vA , where rA D `=.1 / and rP D `=.1 C /,  being the eccentricity of the orbit. Thus rA 1C vP D D : vA rP 1  Solving this equation for  in terms of vP and vA , we get

12. Since r P D h D constant for the planet’s orbit, and since the speed is v D r P at perihelion and at aphelion (the radial velocity is zero at these points), we have 2

rp vp D ra va ;

By conservation of energy the speed v at the ends of the minor axis of the orbit (where r D a) satisfies

where the subscripts p and a refer to perihelion and aphelion, respectively. Since rp =ra D 8=10, we must have vp =va D 10=8 D 1:25. Also, rp D

` ` D ; 1 C  cos 0 1C

ra D

` ` D : 1 C  cos  1 

aD

k.1

vP2

v 2 D vP2 C 2k D vP2 C

H2 R D D : 2/ 4k.1  2 / 4.1  2 /

D vP2 D vP2

.1 C /R R D : 4.1  2 / 4.1 /

D vP2

It follows that 1 D 4 4, so  D 3=4. The new elliptical orbit has eccentricity  D 3=4.

R

Thus v D

15. c S

a

vA2 D 2k

p



D

4k : `



1 a

1 rP



 2k  1  2 .1 C / ` 2k .1 C / `   2 vP vA2 vP vA 1C 2 vP C vA vP vA .2vP / D vP vA : 2

Since the radial line from the sun to the planet sweeps out equal areas in equal times, the fraction of the planet’s period spend on the same side of the minor axis as the sun is equal to the shaded area in the figure to the total area of the ellipse, that is, 1 2 .2bc/

ab

438

1 rA

1 rP

vP vA .

1 2 ab

Fig. 11.6-13



Using this result and the parameters of the orbit given in the text, we obtain

R , so Similarly, c D a D 4.1  2 / R DcCa D

k : rA

The latter equality shows that

13. Let the radius of the circular orbit be R, and let the parameters of the new elliptical orbit be a and c, as shown in the figure. Then R D a C c. At the moment of the collision, r does not change (r D R), but the speed r P is cut in half. Therefore P is cut in half, and so h D r 2 P is cut in half. Let H be the value of r 2 P for the circular orbit, and let h be the value for the new elliptical orbit. Thus h D H=2. We have h2

v2 k D A rP 2

v2 k D P a 2

v2 2

Thus `=.1C/ D .8=10/`=.1 /, and so 10 10 D 8C8. Hence 2 D 18. The eccentricity of the orbit is  D 1=9.

H2 RD ; k

vP vA : vP C vA

D

D

1 2 ab

ab

ab

D

1 2

where  D c=a is the eccentricity of the orbit.

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 ; 

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 11.6

2 Thus T D p k



v02 k

2 r0



3=2

: y

a

b

(PAGE 673)

A c

a

b a

c

S

P x

Fig. 11.6-15

Fig. 11.6-16 17.

16. By conservation of energy, we have   1 2 h2 rP C 2 D 2 r

k r

K

where K is a constant for the orbit (the total energy). The term in the parentheses is v 2 , the square of the speed. Thus k 1 2 k 1 2 v D KD v ; r 2 r0 2 0 where r0 and v0 are the given distance and speed. We evaluate K at perihelion. The parameters of the orbit are `D

h2 ; k

aD

h2 k.1

2/

;

bD

p

h2

k 1

2

;

Let r1 .s/ and r2 .s/ be the distances from the point P D r.s/ on the ellipse E to the two foci. (Here s denotes arc length on E, measured from any convenient point.) By symmetry Z Z E

r1 .s/ ds D

E

r2 .s/ ds:

But r1 .s/ C r2 .s/ D 2a for any s. Therefore, Z

E

r1 .s/ ds C

Z

E

r2 .s/ ds D

Z

E

2a ds D 2ac.E/:

R Hence E r1 .s/ ds D ac.E/, and

Z 1 r1 .s/ ds D a: c.E/ E

c D a:

y P

At perihelion P we have r Da

c D .1

/a D

Since rP D 0 at perihelion, the speed there is v D r P . By Kepler’s second law, r 2 P D h, so v D h=r D k.1 C /= h. Thus k v2 KD r 2 k2 1 k2 D 2 .1 C / .1 C /2 h 2 h2 h i k2 D 2 .1 C / 2 .1 C / 2h k2 k D 2 .1  2 / D : 2h 2a Thus a D

k . By Kepler’s third law, 2K

T2 D

4 2 4 2 3 a D k k



r2

h2 : k.1 C /

k 2K

3

F2

F1

x

E

Fig. 11.6-17 18. Start with rR

h2 D r3

k : r2

1 , where  D .t /. Since r 2 P D h u. / (constant), we have

Let r.t / D

rP D :

r1

rR D

du h du 1 du P  D r2 D h u2 d d r 2 d 2 d 2u P h2 d 2 u 2 2d u h 2 D D h u : 2 2 d r d d 2

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SECTION 11.6 (PAGE 673)

Thus

h2 u2

d 2u d 2

ADAMS and ESSEX: CALCULUS 9

ku2 , or

Such orbits are bounded away from zero and infinity only if A D 0, in which case they are circular.

k d 2u Cu D 2: d 2 h

Thus, the only possible orbits which are bounded away from zero and infinity (i.e., which do not escape to infinity or plunge into the sun) in a universe with an inverse cube gravitational attraction are some circular orbits for which h2 D k. Such orbits cannot be considered “stable” since even slight loss of energy would result in decreased h and the condition h2 D k would no longer be satisfied. Now aren’t you glad you live in an inverse square universe?

h2 u3 D

This is the DE for simple harmonic motion with a constant forcing term (nonhomogeneous term) on the righthand side. It is easily verified that uD

k  1 C  cos. h2

 0 /

is a solution for any choice of the constants  and 0 . Expressing the solution in terms of r, we have h2 =k 1 C  cos.

rD

0 /

20.

h D r3

k ; r3

where r 2 P D h is constant, since the force is central. Making the same change of variables used in Exercise 18, we obtain d 2u h2 u2 2 h2 u3 D ku3 ; d or d 2 u k h2 u D 0: d 2 h2 There are three cases to consider. d 2u C ! 2 u D 0, where d 2 k/= h2 . This has solution u D A cos !. 0 /.

CASE I. If k < h2 the DE is ! 2 D .h2 Thus

k  K > 0; r

k . The orbit is, therefore, bounded. K ` rD , . > 1/. 1 C  cos  See the following figure. Vertices: At V1 ,  D 0 and r D `=.1 C /. At V2 ,  D  and r D `=.1 / D `=. 1/. Semi-focal separation:   ` ` ` 1 C D 2 : cD 2 1C 1   1 The centre is .c; 0/. Semi-transverse axis: ` ` ` D 2 : aD 2  1 C1  1 Semi-conjugate axis: p ` : b D c 2 a2 D p 2 1 Direction of asymptotes (see figure): b a 1  D tan 1 D cos 1 D cos 1 : a c  so r 

19. For inverse cube attraction, the equation of motion is rR

K by conservation of energy, if K < 0,

;

which is an ellipse if jj < 1. 2

1 k D v2 Since r 2 then

1 : A cos !. 0 /  . There are no bounded Note that r ! 1 as  ! 0 C 2! orbits in this case. rD

21.

d 2u ! 2 u D 0, where d 2 ! 2 D .k h2 /= h2 . This has solution u D Ae ! C Be ! . Since u ! 0 or 1 as  ! 1, the corresponding solution r D 1=u cannot be both bounded and bounded away from zero. (Note that P D h=r 2  K > 0 for any orbit which is bounded away from zero, so we can be sure  ! 1 on such an orbit.)

y

CASE II. If k > h2 the DE is

c

F1

V1

b F2



 C

a

d 2u D 0, which has d 2 solutions u D A C B, corresponding to CASE III. If k D h2 the DE is

rD

440

1 : A C B

Fig. 11.6-21

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V2

x

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INSTRUCTOR’S SOLUTIONS MANUAL

REVIEW EXERCISES 11

22. By Exercise 17, the asymptotes make angle  D cos 1 .1=/ with the transverse axis, as shown in the figure. The angle of deviation ı satisfies 2 C ı D , so  ı D , and 2 2 ı cos  D sin ; 2

(PAGE 675)

Therefore 2 v2 a ı ı Dv1 D 1 cot D cot : k k 2 2

ı sin  D cos : 2

Review Exercises 11 (page 675)

y

1.

Given that a  r D 0 and a  v D 0, we have d jr.t / t v.t /j2 dt     D 2 r.t / t v.t /  v.t / v.t / t a.t /   D 2 r.t / t v.t /  a.t / D 0 0 D 0:

.c;0/ D 2

 rp

S

a

x ı

2.

Fig. 11.6-22

r D t cos t i C t sin t j C .2 t /k, .0  t p  2/ is a conical helix wound around the cone z D 2 x 2 C y 2 starting at the vertex .0; 0; 2/, and completing one revolution to end up at .2; 0; 0/. Since

By conservation of energy,

v D .cos t

k v2 D constant D 1 r 2

v2 2

LD

` ; C1 h. C 1/ h D : v D vp D rp P D rp ` a D .

1/a D

Since h2 D k`, we have 2 v1

D

vp2 2

Z

0

2

! p p p 2 C 2 C 4 2 2 2 2 C t dt D  2 C 4 Cln p 2

units. 3.

The position of the particle at time t is

2k rp

h . C 1/2 `2 kh . C 1/2 D ` k D . 2 1/ D ` D

k;

the length of the curve is

for all points on the orbit. At perihelion, r D rp D c

t sin t /i C .sin t C t cos t /j

2k . C 1/ ` i 2. C 1/

r D xi C x 2 j C 32 x 3 k; where x is an increasing function of t . Thie velocity is vD

k : a

 dx  i C 2xj C 2x 2 k : dt

Since the speed is 6, we have

2 Thus av1 D k.

If D is the perpendicular distance from the sun S to an asymptote of the orbit (see the figure) then D D c sin  D a sin  D a Da

cos.ı=2/ ı D a cot : sin.ı=2/ 2

sin  cos 

6D

dx dx p 1 C 4x 2 C 4x 4 D .2x 2 C 1/ ; dt dt

so that dx=dt D 6=.2x 2 C 1/. The particle is at .1; 1; 32 / when x D 1. At this time its velocity is v.1/ D 2.i C 2j C 2k/:

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REVIEW EXERCISES 11 (PAGE 675)

ADAMS and ESSEX: CALCULUS 9

Also

5. 6 dx 144x .4x/ D .2x 2 C 1/2 dt .2x 2 C 1/3 d 2x .i C 2xj C 2x 2 k/ aD dt 2   dx dx dx C k : 2 j C 4x dt dt dt

At x D 1, we have

D

16 .i C 2j C 2k/ C 2.4j C 8k/ 3 8 . 2i 3

j C 2k/: 6.

4. The position, velocity, speed, and acceleration of the particle are given by

7.

ˇ ˇp ˇ dx ˇ v D ˇˇ ˇˇ 1 C 4x 2 dt  2 2 d x dx aD j: .i C 2xj/ C 2 dt 2 dt

ks 2 ks 2 i C sin j 2 2 ks 2 ks 2 a D ks sin i C ks cos j 2 2 v  a D ksk: v D cos

dx t D p dt 1 C 4x 2 p 4tx dx 1 C 4x 2 p 2 d 2x 1 C 4x dt D : 2 dt 1 C 4x 2

Therefore the curvature at position s is  D jv  aj=v 3 D ks. 8.

p p 4 2 .i C 2 2j/ C 2j: 9

If the particle is moving to the left, so that dx=dt < 0, a similar calculation shows that at t D 3 its acceleration is aD

442

p p 3C4 2 .i C 2 2j/ C 2j: 9

If r D e  , and P D k, then rP D e rR D k 2 r. Since r D r rO , we have v D rP rO C r P O D kr rO C kr O a D .Rr

Hence the acceleration is 3

t Tangential acceleration: dv=dt e t. pD e 2 Normal acceleration: v  D 2. Since v D 2 cosh t , the minimum speed is 2 at time t D 0. Z s Z s kt2 kt2 For x.s/ D dt , y.s/ D dt , we have cos sin 2 2 0 0

Since x.0/ D y.0/ D 0, the arc length along the curve, measured from the origin, is s. Also,

Let us assume that the particle is moving to the right, so that dx=dt > 0. Since the speed is t , we have

aD

2t j C e t k

dx ks 2 dy ks 2 D cos ; D sin ; ds 2 ds 2 so that the speed is unity: s  2  2 dy dx C D 1: vD ds ds

r D xi C x 2 j dx vD .i C 2xj/; dt

p If the particle is at . 2; 2/ at t D 3, then dx=dt D 1 at that time, and p d 2x 3 4 2 D : dt 2 9

p

v D e t i C 2j e t k a D et i C e t k da D et i e t k dt p p t v  a D 2e t i 2j 2e k p 2t 2t D et C e t v D e C2Ce p t jv  aj D 2.e C e t / p jv  aj 2 D D 3 t v .e C e t /2 da p .v  a/  2 dt D D t D : jv  aj2 .e C e t /2

d 2x D dt 2

a.1/ D

p

r D et i C

D .k 2 r

9.

r P 2 /Or C .r R C 2rP P /O k 2 r/Or C .0



P D

2k 2 r/O D

kr, and

2k 2 r O :

r D a.t sin t /i C a.1 cos t /j v D a.1 cos t /i C a sin t j p v D a 1 2 cos t C cos2 t C sin2 t p p t D a 2 1 cos t D 2a sin if 0  t  2. 2 The length of the cycloid from t D 0 to t D T  2 is   Z T T t units. s.T / D 2a sin dt D 4a 1 cos 2 2 0

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INSTRUCTOR’S SOLUTIONS MANUAL

 10. s D 4a 1

cos

t 2



) t D 2cos

1

 1

REVIEW EXERCISES 11

s  D t .s/. 4a

Thus rQ .t / represents the same cycloid as r.t /, but translated a units to the left and 2a units upward. From Exercise 11, the given cycloid is the evolute of its involute. y

The required arc length parametrization of the cycloid is  r D a t .s/ 11.

  sin t .s/ i C a 1

(PAGE 675)

 cos t .s/ j:

Q A

From Exercise 9 we have

P

O / D v D .1 cos t /i C sin t j T.t v 2 sin.t =2/ t t D sin i C cos j 2 2 1 t 1 t cos i sin j O O dT 1 dT 2 2 2 D D 2 t ds v dt 2a sin 2   t 1 cot i j D 4a 2 ˇ ˇ ˇ d TO ˇ 1 ˇ ˇ .t / D ˇ ˇD ˇ ds ˇ 4a sin.t =2/

O

x

Fig. R-11-12 13.

The position vector of P is given by r D R sin  cos  i C R sin  sin  j C R cos k: Mutually perpendicular unit vectors in the directions of increasing R,  and  can be found by differentiating r with respect to each of these coordinates and dividing the resulting vectors by their lengths. They are

O 1 dT O / D r.t / C rC .t / D r.t / C .t /N.t ..t //2 ds   t 16a2 sin2 .t =2/ cot i j D r.t / C 4a 2 t t t D r.t / C 4a cos sin i 4a sin2 j 2 2 2 D a.t sin t /i C a.1 cos t /j C 2a sin t i 2a.1 cos t /j D a.t C sin t /i a.1 cos t /j (let t D u D a.u sin u /i C a.1 cos u 2/j:

O D d r D sin  cos  i C sin  sin  j C cos k R dR 1 dr O D D cos  cos  i C cos  sin  j sin k R d dr 1 D sin  i C cos  j: O D R sin  d The triad fOr; O ; O g is right-handed. This is the reason for ordering the spherical polar coordinates .R; ;  / rather than .R; ; /.

) 14.

This is the same cycloid as given by r.t / but translated a units to the right and 2a units downward. 12. Let P be the point with position vector r.t / on the cycloid. By Exercise 9, the arc OP has length 4a 4a cos.t =2/, and so PQ has length 4a - arc OP D 4a cos.t =2/ units. Thus t O ! PQ D 4a cos T.t / 2  t t t sin i C cos j D 4a cos 2 2 2 D 2a sin t i C 2a.1 C cos t /j:

By Kepler’s Second Law the position vector r from the origin (the sun) to the planet sweeps out area at a constant rate, say h=2: dA h D : dt 2 As observed in the text, dA=dt D r 2 P =2, so r 2 P D h, and r  v D .r rO /  .Pr rO C r P O / D r 2 P rO  O D hk D h is a constant vector.

15.

By Exercise 14, r  rP D r  v D h is constant, so, by Newton’s second law of motion, r  F.r/ D mr  rR D m

It follows that Q has position vector ! rQ D r C PQ D a.t sin t /i C a.1 cos t /j C 2a sin t i C 2a.1 C cos t /j D a.t C sin t /i C a.1 C cos t C 2/j (let t D u C ) D a.u sin u C /i C a.1 cos u C 2/j:

d .r  rP / D 0: dt

Thus F.r/ is parallel to r, and therefore has zero transverse component: F.r/ D f .r/Or for some scalar function f .r/.

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REVIEW EXERCISES 11 (PAGE 675)

16. By Exercise 15, F.r/ D m.Rr r P 2 /Or D given that r D `=.1 C  cos  /. Thus

ADAMS and ESSEX: CALCULUS 9

which is appropriate since  is much smaller than g, then p dz dr 2   2 i: dt dt Breaking the DE into its components, we get

f .r/Or. We are

` .  sin  /P .1 C  cos  /2 ` sin  P D .1 C  cos  /2 h  sin  2 P r D sin  D ` ` h h2  cos  rR D : .cos  /P D ` `r 2 rP D

p dz d 2x D 2 ; dt 2 dt

z.t / D 100 h2 h2  cos  2 `r r3  h2 ` D 2  cos  D `r r

h2 ; `r 2

mh : `r 2

x

This says that the magnitude of the force on the planet is inversely proportional to the square of its distance from the sun. Thus Newton’s law of gravitation follows from Kepler’s laws and the second law of motion.

Challenging Problems 11 (page 676) a) The angular velocity  of the earth points northward in the direction of the earth’s axis; in terms of the basis vectors defined at a point P at 45ı north latitude, it points in the direction of j C k: jCk 2

b) If v D

D

2 rad/s: 24  3;600

vk, then 2v p .j C k/  k D 2

aC D 2  v D

p

gk C 2 

dr dt

and the initial conditions r.0/ D 100k, r0 .0/ D 0. If we use the approximation dz dr  k; dt dt

444

x.t / D

gt 3 p : 3 2

s

200  4:52; g

2.

2 9:8 p .4:52/3  24  3;600 3 2

0:0155 m:

The object strikes the ground about 15.5 cm west of P. 8 < d v D k  v 32k dt : v.0/ D 70i

a) If v D v1 i C v2 j C v3 k, then k  v D v1 j v2 i. Thus the initial-value problem breaks down into component equations as 8 8 8 < dv1 D v < dv2 D v < dv3 D 32 2 1 dt dt dt : : : v1 .0/ D 70 v2 .0/ D 0 v3 .0/ D 0:

b) If r D xiCyjCzk denotes the position of the baseball t s after it is thrown, then x.0/ D y.0/ D z.0/ D 0 and we have dz D v3 D dt

2vi:

c) If r.t / D x.t /i C y.t /j C z.t /k is the position of the falling object at time t , then r.t / satisfies the DE d 2r D dt 2

y.t / D 0;

at which time we have

2

D p ;

gt 2 ; 2

tD

(because .`=r/ D 1 C  cos  ). Hence

1.

g:

Since g  9:8 m/s2 , the time of fall is

r P 2 D

f .r/ D

d 2z D dt 2

Solving these equations (beginning with the last one), using the initial conditions, we get

It follows that rR

d 2y D 0; dt 2

32t ) z D

dv2 d 2 v1 D Also, D dt 2 dt harmonic motion), so v1 .t / D A cos t C B sin t;

16t 2 :

v1 (the equation of simple

v2 .t / D A sin t

B cos t:

Since v1 .0/ D 70, v2 .0/ D 0, x.0/ D 0, and y.0/ D 0, we have dx D v1 D 70 cos t dt x.t / D 70 sin t

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dy D v2 D 70 sin t dt y.t / D 70.1 cos t /:

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

CHALLENGING PROBLEMS 11

d) If d r=dt D v and r.0/ D 0, then v0 .v0  k/k sin.!t / r.t / D !   v0  k C 1 cos.!t / C .v0  k/t k: ! Since the three constant vectors v0  k v0 .v0  k/k ; ; and .v0  k/k ! ! are mutually perpendicular, and the first two have the same length because

At time t seconds after it is thrown, the ball is at position r D 70 sin t i C 70.1

cos t /j

16t 2 k:

c) At t D 1=5 s, the ball is at about .13:9; 1:40; 0:64/. If it had been thrown without the vertical spin, its position at time t would have been r D 70t i

16t 2 k;

jv0

a)

!D

qB m

4.

d dv .v  k/ D  k D !.v  k/  k D 0: dt dt Thus v  k D constant D v0  k.

dv d jvj2 D 2  v D 2!.v  k/  v D 0, Also, dt dt so jvj D constant D jv0 j for all t . b) If w.t / D v.t / .v0  k/k, then w  k D 0 by part (a). Also, using the result of Exercise 23 of Section 1.3, we have d 2v dv d 2w D D!  k D ! 2 .v  k/  k dt 2 dt 2 h dt i D ! 2 .k  k/v .k  v/k h i D ! 2 v .v0  k/k D ! 2 w; the equation of simple harmonic motion. Also, w.0/ D v0 .v0  k/k w0 .0/ D !v0  k: c) Solving the above initial-value problem for w, we get w D A cos.!t / C B sin.!t /; A D w.0/ D v0 .v0  k/k; !B D w0 .0/ D !  k:

where and

Therefore, v.t / D w.t / C .v0  k/k h i D v0 .v0  k/k cos.!t / C .v0  k/ sin.!t / C .v0  k/k:

.v0  k/kj D jv0 j sin  D jv0  kj;

where  is the angle between v0 and k, the curve r.t / is generally a circular helix with axis in the z direction. However, it will be a circle if v0  k D 0, that is, if v0 is horizontal, and it will be a straight line if v0  k D 0, that is, if v0 is vertical.

so its position at t D 1=5 s would have been .14; 0; 0:64/. Thus the spin has deflected the ball approximately 1.4 ft to the left (as seen from above) of what would have been its parabolic path had it not been given the spin. 8 < d v D !v  k; 3. dt : v.0/ D v0

(PAGE 676)

The arc length element on x D a. sin  /, y D a.cos  1/ is (for   ) q ds D a .1 cos  /2 C sin2  d p D a 2.1 cos  / d D 2a sin.=2/ d:

If the bead slides downward from rest at height y.0 / to height y. /, its gravitational potential energy has decreased by h i mg y.0 / y. / D mga.cos 0 cos  /:

Since there is no friction, all this potential energy is converted to kinetic energy, so its speed v at height y. / is given by 1 2 mv D mga.cos 0 cos  /; 2 p and so v D 2ga.cos 0 cos  /. The time required for the bead to travel distance ds at speed v is dt D ds=v, so the time T required for the bead to slide from its starting position at  D 0 to the lowest point on the wire,  D , is Z  Z D ds 1 ds T D D d 0 v d D0 v s Z sin.=2/ 2a  d D p g 0 cos 0 cos  s Z 2a  sin.=2/ D p d 2 g 0 2 cos .0 =2/ 2 cos2 .=2/ Let u D cos.=2/ du D 12 sin.=2/ d r Z cos.0 =2/ a du p D2 2 g 0 cos .0 =2/ u2  ˇˇcos.0 =2/ r a u ˇ 1 D2 sin ˇ g cos.0 =2/ ˇ 0 p D  ag

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CHALLENGING PROBLEMS 11 (PAGE 676)

ADAMS and ESSEX: CALCULUS 9

A

which is independent of 0 .

vertical section

y x

 D 0 starting point

E

y horizontal section

p

g D .g= 2/.i

 D

j/

B

D

. 2; 2/

.2; 2/ C

Fig. C-11-4 5.

x

a) The curve BCD is the graph of an even function; a fourth degree polynomial with terms of even degree only will enable us to match the height, slope, and curvature at D, and therefore also at C . We have f .x/ D ax 4 C bx 2 C c

f 0 .x/ D 4ax 3 C 2bx

f 00 .x/ D 12ax 2 C 2b: At D we have x D 2, so we need

Fig. C-11-5

6.

a) At time t, the hare is  at P D .0; vt / and the fox is at Q D x.t /; y.t / , where x and y are such that the slope dy=dx of the fox’s path is the slope of tline y vt dy D . PQ: dx x b) Since

2 D f .2/ D 16a C 4b C c 1 D f 0 .2/ D 32a C 4b 0 D f 00 .2/ D 48a C 2b: These equations yield a D 1=64, b D 3=8, c D 3=4, so the curved track BCD is the graph of 1 y D f .x/ D . x 4 C 24x 2 C 48/. 64 b) Since we are ignoring friction, the p speed v of the car during its drop is given by v D 2gs, where s is the vertical distance dropped. (See the previous solution.) At B the car p has dropped about 7.2 m, so its speed there is v  2.9:8/.7:2/  11:9 m/s. At C the car p has dropped 10 .c= 2/  9:47 m, so its speed there is v D 13:6 m/s. At D the car has dropped 10 m, so its speed is v D 14:0 m/s. c) At C we have x D 0, f 0 .0/ D 0, and f 00 .0/ D 2b D 3=4. Thus the curvature of the track at C is jf 00 .0/j 3 D D : 4 .1 C .f 0 .0//2 /3=2 The normal accelerationpis v 2   138:7 m/s2 (or about 14g). Since v D 2gs, we have p

p p 2g ds 2g 19:6 dv .13:6/  9:78 m/s2 ; D p D p v p dt 2 s dt 2 s 2 9:47 so the total acceleration has magnitude approximately p .138:7/2 C .9:78/2  139 m/s2 ;

 dx d 2 y d y D dt dx 2 dt  dy x dt D  1 dy D x dx 1 D 2 .y x



vt x v



x2 

dx dt vt /

.y

v

dx dt

vt /

dx dt

1 dx .y vt / x2 dt v 1 dx .y vt / D x x2 dt

v d 2y D . dx 2 dx=dt Since the fox’s speed is also v, we have

Thus x



dx dt

2

C



dy dt

2

D v2:

Also, the fox is always running to the left (towards the y-axis from points where x > 0), so dx=dt < 0. Hence v   D dx dt

s

.dy=dt /2 1C D .dx=dt /2

s

1C



dy dx

and so the fox’s path y D y.x/ satisfies the DE

which is again about 14g.

446

d 2 y dx d dy D , we have dt dx dx 2 dt

d 2y D x dx 2

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s

1C



dy dx

2

:

2

;

v : x

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INSTRUCTOR’S SOLUTIONS MANUAL

CHALLENGING PROBLEMS 11

c) If u D dy=dx, then u D 0 and y D 0 when x D a, and p du x D 1 C u2 Z dx Z du dx p D Let u D tan  2 x 1Cu du D sec2  d Z sec  d D ln x C ln C ln.tan  C sec  / D ln.C x/ p u C 1 C u2 D C x:

b) Since yourpvelocity at any point has a northward component v= 2, and progress northward is measured along a circle of radius a (a meridian), your colatitude .t / satisfies a

p x u 1 C u2 D a x 2 2xu 1 C u2 D 2 C u2 a a x2 2xu D 2 1 a a dy x a DuD dx 2a 2x a x2 ln x C C1 : yD 4a 2 Since y D 0 when x D a, we have C1 D so x 2 a2 a x ln yD 4 2 a

T D

a a=2 p D p : v= 2 2v

 2

vt p : a 2

Since p your velocity also has an eastward component v= 2 measured along a parallel of latitude that is a circle of radius a sin , your longitude coordinate  satisfies d v .a sin / D p dt 2   d v vt D p cos p a 2 dt a 2 Z v vt D p sec p dt a 2 a 2  vt vt C C: D ln sec p C tan p a 2 a 2

a a C ln a, 4 2

a) Since you are always travelling northeastpat speed v, you are always moving north at rate v= 2. Therefore you will reach the north pole in finite time

v p : 2

Since .0/ D =2, it follows that

As  D 0 at t D 0, we have C D 0, and so   vt vt .t / D ln sec p C tan p : a 2 a 2

is the path of the fox. 7.

d D dt

.t / D

Since u D 0 when x D a, we have C D 1=a.

(PAGE 676)

p c) As t ! T D a=. 2v/, the expression for .t / ! 1, so your path spirals around the north pole, crossing any meridian infinitely often.

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SECTION 12.1 (PAGE 684)

ADAMS and ESSEX: CALCULUS 9

z

CHAPTER 12. PARTIAL DIFFERENTIATION .2;0;2/

.2;3;2/

Section 12.1 Functions of Several Variables (page 684) 1.

zDx

xCy . f .x; y/ D x y The domain consists of all points in the xy-plane not on the line x D y.

p 2. f .x; y/ D xy. Domain is the set of points .x; y/ for which xy  0, that is, points on the coordinate axes and in the first and third quadrants. x . x2 C y2 The domain is the set of all points in the xy-plane except the origin.

3. f .x; y/ D

4. f .x; y/ D

Fig. 12.1-11

12. f .x; y/ D sin x; 0  x  2; 0  y  1 z

z D sin x

xy

. x2 y2 The domain consists of all points not on the lines x D ˙y. p 5. f .x; y/ D 4x 2 C 9y 2 36. The domain consists of all points .x; y/ lying on or outside the ellipse 4x 2 C 9y 2 D 36. p 6. f .x; y/ D 1= x 2 y 2 . The domain consists of all points in the part of the plane where jxj > jyj. 7.

f .x; y/ D ln.1 C xy/. The domain consists of all points satisfying xy > 1, that is, points lying between the two branches of the hyperbola xy D 1.

y

3 x

2 x 1

y

Fig. 12.1-12

13.

z D f .x; y/ D y 2 z

1

8. f .x; y/ D sin .x C y/. The domain consists of all points in the strip 1  x C y  1.

z D y2

xyz . x2 C y2 C z2 The domain consists of all points in 3-dimensional space except the origin.

9. f .x; y; z/ D

y

e xyz 10. f .x; y; z/ D p . xyz The domain consists of all points .x; y; z/ where xyz > 0, that is, all points in the four octants x > 0, y > 0, z > 0; x > 0, y < 0, z < 0; x < 0, y > 0, z < 0; and x < 0, y < 0, z > 0. 11.

z D f .x; y/ D x

448

x

Fig. 12.1-13

14.

f .x; y/ D 4

x2

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y 2 ; .x 2 C y 2  4; x  0; y  0/

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 12.1

(PAGE 684)

z z 4

zD4

x

2

y

2 x

2

y

y

2

x

Fig. 12.1-14

15.

z D f .x; y/ D

p

Fig. 12.1-17

18. f .x; y/ D 6

x2 C y2 z

zD

p x2 C y2

x

2y

z 6

zD6

x

2y y

3

y 6

x

x

Fig. 12.1-18 Fig. 12.1-15 19. 16. f .x; y/ D 4

f .x; y/ D x

y D C , a family of straight lines of slope 1.

x2

y

cD 3 cD 2

z

zD4

x2

cD 1 cD0

x cD1 cD2 y

cD3

x

x Fig. 12.1-19

Fig. 12.1-16 20. 17.

z D f .x; y/ D jxj C jyj

yDc

f .x; y/ D x 2 C 2y 2 D C , a family of similar ellipses centred at the origin.

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SECTION 12.1 (PAGE 684)

ADAMS and ESSEX: CALCULUS 9

y

23.

x 2 C 2y 2 D c

x y D C , a family of straight lines through xCy the origin, but not including the origin. f .x; y/ D

y

cD16

cD9

cD 1

cD4

cD :5

cD1 cD0 x cD:5 cD1

x cD2

cD 2

Fig. 12.1-20 21.

x y xCy

f .x; y/ D xy D C , a family of rectangular hyperbolas with the coordinate axes as asymptotes.

Dc

Fig. 12.1-23

y cD9 cD4 cD1

24. cD0 x cD 1

cD 4

y D C. C y2  1 2 D 4C1 2 of circles This is the family x 2 C y 2C passing through the origin and having centres on the yaxis. The origin itself is, however, not on any of the level curves.

f .x; y/ D

x2

y

cD 9

cD1

xy D c

cD2

Fig. 12.1-21 cD3

x2 D C , a family of parabolas, y D x 2 =C , 22. f .x; y/ D y with vertices at the origin and vertical axes.

x

y cD1

cD 3

cD0:5 cD 2 cD2 cD 1

Fig. 12.1-24

x x2 y

Dc

cD 2

cD 0:5

Fig. 12.1-22

450

cD 1

25.

f .x; y/ D xe y D C . x This is the family of curves y D ln . C

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y x 2 Cy 2

Dc

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 12.1

y

29.

cD 1

(PAGE 684)

The graph of the function whose level curves are as shown in part (a) of Figure 12.1.29 is a plane containing the yaxis and sloping uphill to the right. It is consistent with, say, a function of the form f .x; y/ D y. (a) (b) y y

cD1

C D10 cD2

cD 2

x

x

cD4

cD 4

xe

y

Dc CD 5

(c)

Fig. 12.1-25

26. f .x; y/ D

s

1 y

x2 D C ) y D y

f .x; y/ D

s

1 y

x2 D C

y

C D5 C D5

1 . x2 C C 2

x

C D0

(d)

y

C D3

x

C D 0:8

C D0

x

CD 5

Fig. 12.1-29 C D1

30.

The graph of the function whose level curves are as shown in part (b) of Figure 12.1.29 is a cylinder parallel to the x-axis, rising from height zero first steeply and then more and more slowly as y increases. Itpis consistent with, say, a function of the form f .x; y/ D y C 5.

31.

The graph of the function whose level curves are as shown in part (c) of Figure 12.1.29 is an upside down circular cone with vertex at height 5 on the z-axis and base circle in the xy-plane. It is consistent with, say, a function of p the form f .x; y/ D 5 x2 C y2.

C D2 x Fig. 12.1-26 27.

The landscape is steepest at B where the level curves are closest together.

500 A

500

600 C

32.

The graph of the function whose level curves are as shown in part (d) of Figure 12.1.29 is a cylinder (possibly parabolic) with axis in the yz-plane, sloping upwards in the direction of increasing y. It is consistent with, say, a function of the form f .x; y/ D y x 2 .

33.

The curves y D .x C /2 are all horizontally shifted versions of the parabola y D x 2 , and they all lie in the half-plane y  0. Since each of these curves intersects all of the others, they cannot be level curves of a function f .x; y/ defined in y  0. To be a family of level curves of a function f .x; y/ in a region, the various curves in the family cannot intersect one another in that region.

34.

4z 2 D .x z/2 C .y z/2 . If z D c > 0, we have .x c/2 C .y c/2 D 4c 2 , which is a circle in the plane z D c, with centre .c; c; c/ and radius 2c.

N

B W

E S

400 300 200 100 Fig. 12.1-27 28. C is a “pass” between two peaks to the east and west. The land is level at C and rises as you move to the east or west, but falls as you move to the north or south.

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SECTION 12.1 (PAGE 684)

ADAMS and ESSEX: CALCULUS 9

y

40. cD3

x2 C y2 . z2 The equation f .x; y; z/ D c can be rewritten x 2 C y 2 D C 2 z 2 . The level surfaces are circular cones with vertices at the origin and axes along the z-axis.

f .x; y; z/ D

cD2

41. f .x; y; z/ D jxj C jyj C jzj. The level surface f .x; y; z/ D c > 0 is the surface of the octahedron with vertices .˙c; 0; 0/, .0; ˙c; 0/, and .0; 0; ˙c/. (An octahedron is a solid with eight planar faces.)

cD1

x

42. .x

c/2 C .y

Fig. 12.1-34

c/2 D 4c 2

The graph of the function z D z.x; y/  0 defined by the given equation is (the upper half of) an elliptic cone with axis along the line x D y D z, and circular crosssections in horizontal planes. 35.

f .x; y; z; t / D x 2 C y 2 C z 2 C t 2 . The “level hypersurface” p f .x; y; z; t / D c > 0 is the “4-sphere” of radius c centred at the originpin R4 . That is, it consists of all points in R4 at distance c from the origin.

43.

z

2 2 2 a) f .x; y/ D C p is x C y D C implies that f .x; y/ D x 2 C y 2 .

zD

b) f .x; y/ D C is x 2 C y 2 D C 4 implies that f .x; y/ D .x 2 C y 2 /1=4 .

1 1 C x2 C y2

c) f .x; y/ D C is x 2 C y 2 D C implies that f .x; y/ D x 2 C y 2 .

d) f .x; y/ D Cpis x 2 C y 2 D .ln C /2 implies that f .x; y/ D e

x 2 Cy 2

y

.

36. If the level surface f .x; y; z/ D C is the plane

x Fig. 12.1-43

x y z C C D 1; C3 2C 3 3C 3 that is, x C

z y C D C 3 , then 2 3

44.

z zD

 z 1=3 y f .x; y; z/ D x C C : 2 3

cos x 1 C y2

37. f .x; y; z/ D x 2 C y 2 C z 2 . The level surface f .x; y; z/ D c > 0 is a sphere of radius p c centred at the origin. 38. f .x; y; z/ D x C 2y C 3z. The level surfaces are parallel planes having common normal vector i C 2j C 3k.

y

x

39. f .x; y; z/ D x 2 C y 2 . The level p surface f .x; y; z/ D c > 0 is a circular cylinder of radius c with axis along the z-axis.

452

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5  x  5;

5y5

Fig. 12.1-44

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 12.2

(PAGE 689)

z

45.

z zD

zD

y 1 C x2 C y2

1 xy

y

y

4x4 4y4

x Fig. 12.1-48

x Fig. 12.1-45

Section 12.2 Limits and Continuity (page 689) 46.

z zD

.x 2

1.

x 1/2 C y 2

2.

3. y

lim

.x;y/!.0;0/

xy C x 2 D 2. 1/ C 22 D 2

p

x2 C y2 D 0

x2 C y2 does not exist. y .x;y/!.0;0/ lim

If .x; y/ ! .0; 0/ along x D 0, then If .x; y/ ! .0; 0/ along y x2 C y2 D 1 C x 2 ! 1. y

x Fig. 12.1-46

47.

lim

.x;y/!.2; 1/

4.

x . x2 C y2 Then jf .x; 0/j D j1=xj ! 1 as x ! 0. But jf .0; y/j D 0 ! 0 as y ! 0. Thus lim.x;y/!.0;0/ f .x; y/ does not exist. Let f .x; y/ D

z 5. z D xy 6. y

lim

.x;y/!.1;/

1

cos.xy/ D x cos y 1

Fig. 12.1-47

1

x 2 .y 1/2 D 0, because 1/2 .x;y/!.0;1/ x 2 C .y lim

and x 2 ! 0 as .x; y/ ! .0; 1/. ˇ ˇ ˇ y3 ˇ y2 ˇ ˇ ˇ x 2 C y 2 ˇ  x 2 C y 2 jyj  jyj ! 0 as .x; y/ ! .0; 0/. Thus

48. The graph is asymptotic to the coordinate planes.

cos  D 1 cos 

ˇ 2 ˇ ˇ x .y 1/2 ˇ ˇ  x2 0  ˇˇ 2 x C .y 1/2 ˇ

7.

x

D

x2 C y2 D y ! 0. y 2 x , then

8.

lim

.x;y/!.0;0/

lim

.x;y/!.0;0/ x 2

y3 D 0. C y2

sin 0 sin.x y/ D D 0: cos.x C y/ cos 0

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SECTION 12.2 (PAGE 689)

ADAMS and ESSEX: CALCULUS 9

sin.xy/ . x2 C y2 2 Now f .0; y/ D 0=x D 0 ! 0 as x ! 0. sin x 2 1 However, f .x; x/ D ! as x ! 0. 2x 2 2 Therefore lim f .x; y/ does not exist.

However there is no way to define f .x; x/ so that f becomes continuous on y D x, since jf .x; y/j D 1=jx C yj ! 1 as y ! x.

9. Let f .x; y/ D

16.

Let f be the function of Example 3 of Section 3.2:

.x;y/!.0;0/

f .x; y/ D

10. The fraction is not defined at points of the line y D 2x and so cannot have a limit at .1; 2/ by Definition 4. However, if we use the extended Definition 6, then, cancelling the common factor 2x y, we get 2x 2 .x;y/!.1;2/ 4x 2 lim

x 2  x 2 C y 4 . Thus

xy 1 x D lim D : y2 4 .x;y/!.1;2/ 2x C y x y  y 2 ! 0 as y ! 0. Thus x2 C y4

x!a

17.

x3y3 . But C y2

ˇ ˇ 3 3 ˇ ˇ ˇ x y ˇ ˇ x2 ˇ 3 3 ˇDˇ ˇ ˇ ˇ x 2 C y 2 ˇ ˇ x 2 C y 2 ˇ jxy j  jxy j ! 0 lim

f .x; y/ D 1

0 D 1.

Define f .0; 0/ D 1. 14.

For x ¤ y, we have f .x; y/ D

15.

x3 x

y3 D x 2 C xy C y 2 : y

The latter expression has the value 3x 2 at points of the line x D y. Therefore, if we extend the definition of f .x; y/ so that f .x; x/ D 3x 2 , then the resulting function will be equal to x 2 C xy C y 2 everywhere, and so continuous everywhere. x y x y f .x; y/ D 2 D . x y2 .x y/.x C y/ Since f .x; y/ D 1=.x C y/ at all points off the line x D y and so is defined at some points in any neighbourhood of .1; 1/, it approaches 1=.1 C 1/ D 1=2 as .x; y/ ! .1; 1/; If we define f .1; 1/ D 1=2, then f becomes continuous at .1; 1/. Similarly, f .x; y/ can be defined to be 1=.2x/ at any point on the line x D y except the origin, and becomes continuous at such points.

454

fu .t / D f .a C t u; b C t v/, where u D ui C vj is a unit vector. f .x; y/ may not be continuous at .a; b/ even if fu .t / is continuous at t D 0 for every unit vector u. A counterexample is the function f of Example 4 in this section. Here a D b D 0. The condition that each fu should be continuous is the condition that f should be continuous on each straight line through .0; 0/, which it is if we extend the domain of f to include .0; 0/ by defining f .0; 0/ D 0. (We showed that f .x; y/ ! 0 as .x; y/ ! .0; 0/ along every straight line.) However, we also showed that lim.x;y/!.0;0/ f .x; y/ did not exist.

x2

.x;y/!.0;0/

yDb

Similarly, h.y/ D f .a; y/ is continuous at y D b.

x2y2 D 0: 2x 4 C y 4 2 2 x y x4 1 If x D y ¤ 0, then D D . 2x 4 C y 4 2x 4 C x 4 3 x2y2 Therefore lim does not exist. .x;y/!.0;0/ 2x 4 C y 4

12. If x D 0 and y ¤ 0, then

as .x; y/ ! .0; 0/. Thus

if .x; y/ D .0; 0/.

lim g.x/ D x!a lim f .x; y/ D f .a; b/:

x2y2 D 0. .x;y/!.0;0/ x 2 C y 4

x2 C y2 x3 y3 D1 x2 C y2

if .x; y/ ¤ .0; 0/

If f .x; y/ is continuous at .a; b/, then g.x/ D f .x; b/ is continuous at x D a because

lim

13. f .x; y/ D

2xy 2 C y2 x : 0

Let a D b D 0. If g.x/ D f .x; 0/ and h.y/ D f .0; y/, then g.x/ D 0 for all x, and h.y/ D 0 for all y, so g and h are continuous at 0. But, as shown in Example 3 of Section 3.2, f is not continuous at .0; 0/.

2 2

11.

8
2p. In this case lim

xm yn D 0: C y 2 /p

.x;y/!.0;0/ .x 2

19.

Suppose .x; y/ ! .0; 0/ along the ray y D kx. Then f .x; y/ D

ax 2

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xy k D : 2 C bxy C cy a C bk C ck 2

:

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 12.3

(PAGE 696)

z

Thus f .x; y/ has different constant values along different rays from the origin unless a D c D 0 and b ¤ 0. If this condition is not satisfied, lim.x;y/!.0;0/ f .x; y/ does not exist. If the condition is satisfied, then lim.x;y/!.0;0/ f .x; y/ D 1=b does exist. sin x sin3 y cannot be defined at .0; 0/ 1 cos.x 2 C y 2 / so as to become continuous there, because f .x; y/ has no limit as .x; y/ ! .0; 0/. To see this, observe that f .x; 0/ D 0, so the limit must be 0 if it exists at all. However,

20. f .x; y/ D

y 2x 2 y zD 4 x C y2

x 4

4

f .x; x/ D

1

sin x sin x D cos.2x 2 / 2 sin2 .x 2 / Fig. 12.2-22

which approaches 1/2 as x ! 0 by l’H^opital’s Rule or by using Maclaurin series. 23. 21.

z zD

2xy x2 C y2

24.

The graph of a function f .x; y/ that is continuous on region R in the xy-plane is a surface with no breaks or tears in it and that intersects each line parallel to the zaxis through a point .x; y/ of R at exactly one point. (a) We say that limx!a f .x/ D L provided that (i) every open interval containing a contains at least one point of the domain of f different from a, and (ii) if for every  > 0 there exists ı > 0 depending on  such that if x is in the domain of f and satisfies 0 < jx aj < ı, then jf .x/ Lj < . (b) There are no points in the domain of f to the right of 1 or between 1=2 and 1 so condition (i) of rhe definition is not satisfied and limx!1 f .x/ does not exist. If .a; b/ is any open interval containing 0, then b > 0. If integer n > 1=b, then 1=n < b and so .a; b/ contains a point of the domain of f . If  > 0, let ı D . If 1=n < ı, then

y

x

ˇ   ˇ ˇf 1 ˇ n

Fig. 12.2-21 The graphing software is unable to deal effectively with the discontinuity at .x; y/ D .0; 0/ so it leaves some gaps and rough edges near the z-axis. The surface lies between a ridge of height 1 along y D x and a ridge of height 1 along y D x. It appears to be creased along the z-axis. The level curves are straight lines through the origin. 22. The graphing software is unable to deal effectively with the discontinuity at .x; y/ D .0; 0/ so it leaves some gaps and rough edges near the z-axis. The surface lies between a ridge along y D x 2 , z D 1, and a ridge along y D x 2 , z D 1. It appears to be creased along the z-axis. The level curves are parabolas y D kx 2 through the origin. One of the families of rulings on the surface is the family of contours corresponding to level curves.

ˇ ˇ ˇ ˇn 1ˇˇ D ˇˇ

1 n

ˇ ˇ 1 1ˇˇ D < : n

Thus limx!0 f .x/ exists and equals 1.

(c) Since every open interval on the real line contains irrational numbers that are not in the domain of f , the conditions of Definition 8 in Section 1.5 are not met, so neither of the limits above can exist under that definition.

Section 12.3 Partial Derivatives (page 696) 1.

f .x; y/ D x y C 2, f1 .x; y/ D 1 D f1 .3; 2/, f2 .x; y/ D

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1 D f2 .3; 2/.

455

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SECTION 12.3 (PAGE 696)

ADAMS and ESSEX: CALCULUS 9

2. f .x; y/ D xy C x 2 , f1 .x; y/ D y C 2x, f2 .x; y/ D x, f1 .2; 0/ D 4; f2 .2; 0/ D 2:

9.

@w @y

3. f .x; y; z/ D x 3 y 4 z 5 , f1 .x; y; z/ D 3x 2 y 4 z 5 ; f2 .x; y; z/ D 4x 3 y 3 z 5 ; f3 .x; y; z/ D 5x 3 y 4 z 4 ;

f1 .0; 1; 1/ D 0, f2 .0; 1; 1/ D 0, f3 .0; 1; 1/ D 0.

@w @z

xz , yCz 1 z ; g1 .1; 1; 1/ D , g1 .x; y; z/ D yCz 2 1 xz ; g2 .1; 1; 1/ D , g2 .x; y; z/ D .y C z/2 4 1 xy ; g3 .1; 1; 1/ D : g3 .x; y; z/ D .y C z/2 4 1

z D tan @z D @x

1

y  x 

y  D x2

. 1;1/

. 1;1/

11.

1 : 2 12.

@w yze xyz , D @x 1 C e xyz xyz xyz @w xze xye @w ; , D D @y 1 C e xyz @z 1 C e xyz @w @w @w At .2; 0; 1/: D 0; D 1; D 0. @x @y @z p f .x; y/ D sin.x y/,   p p ; 4 D 1; f1 .x; y/ D y cos.x y/; f1 3     x p ;4 D : f2 .x; y/ D p cos.x y/; f2 2 y 3 24

1 , 8. f .x; y/ D p 2 x C y2 1 2 f1 .x; y/ D .x C y 2 / 2

3=2

.2x/ D

.x 2

y , C y 2 /3=2 4 3 , f2 . 3; 4/ D . f1 . 3; 4/ D 125 125 By symmetry, f2 .x; y/ D

456

.x 2

.e;2;e/

x1 x22 , then x3 C x42

1 x3 C x42 2x2 g2 .x1 ; x2 ; x3 ; x4 / D x3 C x42 x22 x1 g3 .x1 ; x2 ; x3 ; x4 / D .x3 C x42 /2 .x22 x1 /2x4 g4 .x1 ; x2 ; x3 ; x4 / D .x3 C x42 /2

6. w D ln.1 C e xyz /;

7.

;

g1 .x1 ; x2 ; x3 ; x4 / D

y x2 C y2

y2 x2   1 1 x @z D D 2 2 @y x x C y2 y 1C 2 x ˇ ˇ @z ˇˇ 1 @z ˇˇ ; D D ˇ ˇ @x ˇ 2 @y ˇ 1C

ˇ @w ˇˇ D 2e; ˇ @x ˇ .e;2;e/ ˇ @w ˇˇ y ln z D e2; D ln x ln z x ; ˇ @y ˇ ˇ .e;2;e/ y @w ˇˇ y ln z D ln x x ; D 2e: ˇ z @z ˇ 1

10. If g.x1 ; x2 ; x3 ; x4 / D

4. g.x; y; z/ D

5.

w D x y ln z , @w D y ln z x y ln z @x

x , C y 2 /3=2

13.

14.

1 3 2 g2 .3; 1; 1; 2/ D 3 2 g3 .3; 1; 1; 2/ D 9 8 g4 .3; 1; 1; 2/ D : 9 g1 .3; 1; 1; 2/ D

8 < 2x 3 y 3 f .x; y/ D x 2 C 3y 2 if .x; y/ ¤ .0; 0/ : 0 if .x; y/ D .0; 0/ 2h3 0 f1 .0; 0/ D lim D2 h!0 h.h2 C 0/ 1 k3 0 f2 .0; 0/ D lim D : 3 k!0 k.0 C 3k 2 / 8 < x 2 2y 2 if x ¤ y f .x; y/ D : x y 0 if x D y h 0 f .h; 0/ f .0; 0/ D lim D 1; f1 .0; 0/ D lim h h h!0 h!0 f .0; k/ f .0; 0/ 2k f2 .0; 0/ D lim D lim D 2: k k!0 k!0 k f .x; y/ D x 2 y 2 f . 2; 1/ D 3 f1 .x; y/ D 2x f1 . 2; 1/ D 4 f2 .x; y/ D 2y f2 . 2; 1/ D 2 Tangent plane: z D 3 4.x C 2/ 2.y 1/, or 4x C 2y C z D 3. y 1 z 3 xC2 D D . Normal line: 4 2 1 x y ; f .1; 1/ D 0; f .x; y/ D xCy 1 .x C y/ .x y/ ; f1 .1; 1/ D f1 .x; y/ D .x C y/2 2 .x C y/. 1/ .x y/ 1 f2 .x; y/ D ; f2 .1; 1/ D : .x C y/2 2 Tangent plane to z D f .x; y/ at (1,1) has equation x 1 y 1 , or 2z D x y. zD 2 2 Normal line: 2.x 1/ D 2.y 1/ D z.

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INSTRUCTOR’S SOLUTIONS MANUAL

15.

f .x; y/ D cos

x y

SECTION 12.3

1 f .; 4/ D p 2

20.

x 1 1 sin p f1 .; 4/ D y y 4 2 x x  f2 .x; y/ D 2 sin f2 .; 4/ D p y y 16 2 The tangent plane at x D , y D 4 is f1 .x; y/ D

 1 zD p 1 2

1 .x 4

/ C

p or 4x y C 16 2z D 16. Normal line: p p 16 2 4 2.x / D .y 4/ D 

 .y 16



z

 4/ ;

21.

p  .1= 2/ .

16. f .x; y/ D e xy ; f1 .x; y/ D ye xy ; f2 .x; y/ D xe xy , f .2; 0/ D 1; f1 .2; 0/ D 0; f2 .2; 0/ D 2. Tangent plane to z D e xy at (2,0) has equation z D 1C2y. Normal line: x D 2, y D 2 2z. 17.

x x2 C y2 .x 2 C y 2 /.1/ x.2x/ y2 x2 f1 .x; y/ D D .x 2 C y 2 /2 .x 2 C y 2 /2 2xy f2 .x; y/ D .x 2 C y 2 /2 1 3 4 f .1; 2/ D ; f1 .1; 2/ D ; f2 .1; 2/ D : 5 25 25 The tangent plane at x D 1, y D 2 is f .x; y/ D

zD

1 3 C .x 5 25

4 .y 25

1/

2/;

25z D 10. x 1 y 2 5z 1 Normal line: D D . 3 4 125

or 3x

4y

2

22.

2

f .1; f .x; y/ D ln.x 2 C y 2 / 2x f1 .x; y/ D 2 f1 .1; x C y2 2y f2 .1; f2 .x; y/ D 2 x C y2 The tangent plane at .1; 2; ln 5/

z D x 4 4xy 3 C 6y 2 2 @z D 4x 3 4y 3 D 4.x y/.x 2 C xy C y 2 / @x @z D 12xy 2 C 12y D 12y.1 xy/: @y The tangent plane will be horizontal at points where both first partials are zero. Thus we require x D y and either y D 0 or xy D 1. If x D y and y D 0, then x D 0. If x D y and xy D 1, then x 2 D 1, so x D y D ˙1. The tangent plane is horizontal at the points .0; 0/, .1; 1/, and . 1; 1/.

24.

z D xye .x Cy /=2 @z 2 2 D ye .x Cy /=2 x 2 ye @x @z 2 2 D x.1 y 2 /e .x Cy /=2 @y

2

2 z D ln 5 C .x 5

2/ D ln 5 2 2/ D 5 4 2/ D 5 is

1/

5z D 10 5 ln 5. x 1 yC2 z Normal line: D D 2=5 4=5

or 2x

4 .y C 2/; 5

4y

ln 5 . 1

2xy ; f .0; 2/ D 0 x2 C y2 2 2 .x C y /2y 2xy.2x/ 2y.y 2 x 2 / f1 .x; y/ D D .x 2 C y 2 /2 .x 2 C y 2 /2 2 2 2x.x y / (by symmetry) f2 .x; y/ D .x 2 C y 2 /2 f1 .0; 2/ D 1; f2 .0; 2/ D 0: Tangent plane at .0; 2/: z D x. Normal line: z C x D 0, y D 2. y   , f .x; y/ D tan 1 ; f .1; 1/ D x 4 1 y  y f1 .x; y/ D D , x2 x2 C y2 y2 1C 2 x   1 x 1 , D 2 f2 .x; y/ D x C y2 y2 x 1C 2 x 1 f1 .1; 1/ D f2 .1; 1/ D . The tangent plane is 2 1 1  1  C .x 1/ C .y C 1/, or z D C .x C y/. zD 4 2 2 4 2  . Normal line: 2.x 1/ D 2.y C 1/ D z 4 p 3 2 f .2; 1/ D 3 f .x; y/ D 1 C x y 2 2 f 3x y 1 .2; 1/ D 2 f1 .x; y/ D p 8 3 2 2 1Cx y f2 .2; 1/ D 3 2x 3 y f2 .x; y/ D p 3 2 2 1Cx y Tangent plane: z D 3 C 2.x 2/ C 38 .y 1/, or 6x C 8y 3z D 11. y 1 z 3 x 2 D D . Normal line: 2 8=3 1 f .x; y/ D

23.

18. f .x; y/ D ye x ; f1 D 2xye x ; f2 D e x , f .0; 1/ D 1; f1 .0; 1/ D 0; f2 .0; 1/ D 1. Tangent plane to z D f .x; y/ at .0; 1/ has equation z D 1 C 1.y 1/, or z D y. Normal line: x D 0, y C z D 2. 19.

(PAGE 696)

2

2

.x 2 Cy 2 /=2

D y.1

x 2 /e

.x 2 Cy 2 /=2

(by symmetry)

The tangent planes are horizontal at points where both of these first partials are zero, that is, points satisfying y.1

x2/ D 0

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and

x.1

y 2 / D 0:

457

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SECTION 12.3 (PAGE 696)

ADAMS and ESSEX: CALCULUS 9

These points are .0; 0/, .1; 1/, . 1; 1/, .1; 1/ and . 1; 1/. At (0,0) the tangent plane is z D 0. At .1; 1/ and . 1; 1/ the tangent plane is z D 1=e. At .1; 1/ and . 1; 1/ the tangent plane is z D 1=e. @z @z D e y and D xe y . @x @y @z @z D xe y D . Thus x @x @y

25. If z D xe y , then

26.

27.

31.

32.

xCy ; x y 2y .x y/.1/ .x C y/.1/ @z D ; D @x .x y/2 .x y/2 .x y/.1/ .x C y/. 1/ 2x @z D : D @y .x y/2 .x y/2 Therefore @z 2xy @z 2xy x C D 0: Cy D @x @y .x y/2 .x y/2 zD

33.

34.

p @z x x 2 C y 2 , then , and D p @x x2 C y2 y @z D p . Thus @y x2 C y2

28. w D x 2 C yz;

1 @w 2x , then , D x2 C y2 C z2 @x .x 2 C y 2 C z 2 /2 2y @w 2z @w D , and D . @y .x 2 C y 2 C z 2 /2 @z .x 2 C y 2 C z 2 /2 Thus

29. If w D

x2 C y2 C z2 D .x 2 C y 2 C z 2 /2

b/ c/:

1/j C Zk

1 D 2tX;

Y

1 2t

1 D 2t Y;

ZD

t:

, and, since Z D X 2 C Y 2 , we must 2 : .1 2t /2

1 . Since the 2 left and right sides of the equation have graphs similar to those in Figure 12.18(b) (in the text), the equation has only 1 1 this one real solution. Hence X D Y D , and so Z D . 2 2 The distance from .1; 1; 0/ to zpD x 2 is the distance from  .1; 1; 0/ to 21 ; 12 ; 21 , which is 3=2 units. Evidently this equation is satisfied by t D

D 2.x 2 C yz/ D 2w:

2w:

30. z D f .x 2 C y 2 /, @z @z D f 0 .x 2 C y 2 /.2x/, D f 0 .x 2 C y 2 /.2y/. @x @y @z @z x D 2xyf 0 .x 2 Cy 2 / 2xyf 0 .x 2 Cy 2 / D 0. Thus y @x @y

458

1/i C .Y

tD

2

a/ C f2 .a; b; c/.y C f3 .a; b; c/.z

If Q D .X; Y; Z/ is the point on the surface z D x 2 C y 2 that is closest to P D .1; 1; 0/, then

Thus X D Y D 1 have

@w @w @w Cy Cz @x @y @z

@w @w @w Cy Cz D @x @y @z

f .x C h; y; z/ f .x; y; z/ h f .x; y C k; z/ f .x; y; z/ f2 .x; y; z/ D lim k k!0 f .x; y; z C `/ f .x; y; z/ f3 .x; y; z/ D lim ` `!0   At a; b; c; f .a; b; c/ the graph of w D f .x; y; z/ has tangent hyperplane h!0

X

@w D y: @z

D 2x 2 C yz C yz

x

y 2 / D 0.

must be normal to the surface at Q, and hence must be ! parallel to n D 2Xi C 2Y j k. Hence PQ D t n for some real number t , so

Therefore x

2xy/f 0 .x 2

y 2 /. 2y/.

f1 .x; y; z/ D lim

! PQ D .X

@z x2 C y2 @z Cy D p D z: @x @y x2 C y2 @w @w D 2x; DD z; @x @y

@z D f 0 .x 2 @y

w D f .a; b; c/ C f1 .a; b; c/.x

If z D

x

z D f .x 2 y 2 /, @z D f 0 .x 2 y 2 /.2x/, @x @z @z Thus y Cx D .2xy @x @y

35.

If Q D .X; Y; Z/ is the point on the surface z D x 2 C 2y 2 that is closest to P D .0; 0; 1/, then ! PQ D Xi C Y j C .Z

1/k

must be normal to the surface at Q, and hence must be ! parallel to n D 2Xi C 4Y j k. Hence PQ D t n for some real number t , so X D 2tX;

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Y D 4t Y;

Z

1D

t:

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 12.4

If X ¤ t D 1=2, so Y D 0, Z Dp 1=2, and p 0, then p 1= 2. The distance from .1= 2; 0; 1=2/ to X D Z D p .0; 0; 1/ is 3=2 units. If Y ¤ t D 1=4, so X D 0, Z D 3=4,pand p 0, then p Y D Z=2 D 3=8. The distance from .0; 3=8; 3=4/ to p .0; 0; 1/ is 7=4 units. If X D Y D 0, then Z D 0 (and t D 1). The distance from .0; 0; 0/ to .0; 0; 1/ is 1 unit. Since p p 7 3 < < 1; 4 2

39.

.x 2 C y 2 /3x 2 .x 3 y 3 /2x .x 2 C y 2 /2 4 2 2 x C 3x y C 2xy 3 D .x 2 C y 2 /2 2 .x C y 2 /. 3y 2 / .x 3 y 3 /2y f2 .x; y/ D .x 2 C y 2 /2 4 2 2 y C 3x y C 2x 3 y D : .x 2 C y 2 /2

37.

Also, at .0; 0/,

k3 h3 D 1; f2 .0; 0/ D lim D 1: 2 k!0 k  k 2 h!0 h  h Neither f1 nor f2 has a limit at .0; 0/ (the limits along x D 0 and y D 0 are different in each case), so neither function is continuous at .0; 0/. However, f is continuous at .0; 0/ because ˇ ˇ ˇ ˇ ˇ x3 ˇ ˇ y3 ˇ ˇCˇ ˇ  jxj C jyj; jf .x; y/j  ˇˇ 2 x C y2 ˇ ˇ x2 C y2 ˇ f1 .0; 0/ D lim

2xy if .x; y/ ¤ .0; 0/; f .0; 0/ D 0 C y2 0 0 f .h; 0/ f .0; 0/ D lim D0 f1 .0; 0/ D lim h h h!0 h!0 f .0; k/ f .0; 0/ 0 0 f2 .0; 0/ D lim D lim D0 h k!0 k!0 k Thus f1 .0; 0/ and f2 .0; 0/ both exist even though f is not continuous at .0; 0/ (as shown in Example 2 of Section 3.2). f .x; y/ D

x2

8
simplify(diff(f,x$4) + 2*diff(f,x$2,y$2) + diff(f,y$4)); 0

D0 C2

@4 u @4 u C 4 D 24 2 2 @x @y @y

Section 12.5 The Chain Rule

(page 711)

24 D 0: 1.

Thus u is biharmonic. @2 u @2 u C D 0. If @x 2 @y 2 v.x; y/ D xu.x; y/, then

22. If u is harmonic, then

  @ @u @u @2 u @2 v D uCx D2 Cx 2 2 @x @x @x @x @x   @ @u @2 u @2 v D x Dx 2 @y 2 @y @y @y  2  2 2 @ v @ u @ v @u @2 u @u C x C D 2 C D2 : @x 2 @y 2 @x @x 2 @y 2 @x

If w D f .x; y; z/ where x D g.s; t /, y D h.s; t /, and z D k.s; t /, then @w D f1 .x; y; z/g2 .s; t / C f2 .x; y; z/h2 .s; t / @t C f3 .x; y; z/k2 .s; t /:

2.

If w D f .x; y; z/ where x D g.s/, y D h.s; t / and z D k.t /, then @w D f2 .x; y; z/h2 .s; t / C f3 .x; y; z/k 0 .t /: @t

Since u is harmonic, so is @u=dx: 

@2 @2 C 2 2 @x @y



@u @ D @x @x



@2 u @2 u C 2 2 @x @y



D

@ .0/ D 0: @x

@2 v @2 v Thus C is harmonic, and so v is biharmonic. The @x 2 @y 2 proof that w.x; y/ D yu.x; y/ is biharmonic is similar.

23. By Example 3, e x sin y is harmonic. Therefore xe x sin y is biharmonic by Exercise 22.

By Exercise 11, ln.x 2 C y 2 / is harmonic (except at the origin). Therefore y ln.x 2 C y 2 / is biharmonic by Exercise 22. x is harmonic (except at the ori25. By Exercise 10, 2 x C y2 xy gin). Therefore 2 is biharmonic by Exercise 22. x C y2

24.

462

3.

If z D g.x; y/ where y D f .x/ and x D h.u; v/, then @z D g1 .x; y/h1 .u; v/ C g2 .x; y/f 0 .x/h1 .u; v/: @u

4.

If w D f .x; y/ where x D g.r; s/, y D h.r; t /, r D k.s; t / and s D m.t /, then h  dw D f1 .x; y/ g1 .r; s/ k1 .s; t /m0 .t / dt  i C k2 .s; t / C g2 .r; s/m0 .t / h  C f2 .x; y/ h1 .r; t / k1 .s; t /m0 .t /  i C k2 .s; t / C h2 .r; t / :

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SECTION 12.5

5. If w D f .x; y; z/ where x D g.y; z/ and y D h.z/, then

Method I.   dz @z @z @x @x @y D C C dt @t @x @t @y @t @z @y C @y @t   y C 2t 2 2 D xy C ty 1 C C 2txy 2 : y C t2

h i dw D f1 .x; y; z/ g1 .y; z/h0 .z/ C g2 .y; z/ dz C f2 .x; y; z/h0 .z/ C f3 .x; y; z/ ˇ @w ˇˇ ˇ D f2 .x; y; z/h0 .z/ C f3 .x; y; z/ @z ˇ ˇx @w ˇˇ D f3 .x; y; z/: ˇ @z ˇ

Method II.   z D t t C ln.e t C t 2 / e 2t     @z e t C 2t D t C ln.e t C t 2 / e 2t C t e 2t 1 C t @t e C t2   C 2t e 2t t C ln.e t C t 2 /   y C 2t C 2txy 2 : D xy 2 C ty 2 1 C y C t2

x;y

6. If u D then

p x 2 C y 2 , where x D e st and y D 1 C s 2 cos t ,

Method I. y x @u se st C p . s 2 sin t / D p @t x2 C y2 x2 C y2 xse st ys 2 sin t D p : x2 C y2

9.

Method II. uD

p

10.

e 2st C .1 C s 2 cos t /2

@u 2se 2st 2s 2 sin t .1 C s 2 cos t / p D @t 2 e 2st C .1 C s 2 cos t /2 x 2 s ys 2 sin t D p : x2 C y2

7.

u , where u D 2x C y and v D 3x v Method I.

If z D tan

1

11. 12.

y, then 13.

@z @z @u @z @v D C @x @u @x  @v @x  u 1 1 1 .3/ .2/ C D 2 2 v v2 u u 1C 2 1C 2 v v 2v 3u 5y D 2 D : u C v2 13x 2 2xy C 2y 2

2x C y 3x y .3x y/.2/ .2x C y/.3/ 1 @z D @x .3x y/2 .2x C y/2 1C 2 .3x y/ 5y 5y D D : .3x y/2 C .2x C y/2 13x 2 2xy C 2y 2 z D tan

T D e t z, where z D f .t /.

e t f .t / C e t f 0 .t /:

dT D 0. The temIf f .t / D e t , then f 0 .t / D e t and dt perature is rising with respect to depth at the same rate at which it is falling with respect to time.

1

8. If z D txy 2 , where x D t C ln.y C t 2 / and y D e t , then

@ f .2x; 3y/ D 2f1 .2x; 3y/: @x @ f .2y; 3x/ D 3f2 .2y; 3x/: @x @ f .y 2 ; x 2 / D 2xf2 .y 2 ; x 2 /: @x  @  f yf .x; t /; f .y; t / @y   D f .x; t /f1 yf .x; t /; f .y; t /   C f1 .y; t /f2 yf .x; t /; f .y; t / : @T @T dz dT D C D dt @t @z dt

14.

Method II.

(PAGE 711)

If E D f .x; y; z; t /, where x D sin t , y D cos t and z D t , then the rate of change of E is @E dE D cos t dt @x

15.

@E @E @E sin t C C : @y @z @t

z D f .x; y/, where x D 2s C 3t and y D 3s 2t .  @2 z @ a) D 2f .x; y/ C 3f .x; y/ 1 2 @s 2 @s D 2.2f11 C 3f12 / C 3.2f21 C 3f22 / D 4f11 C 12f12 C 9f22

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ADAMS and ESSEX: CALCULUS 9

@2 z @ @2 z D D .2f1 C 3f2 / @s@t @t @s @t D 2.3f11 2f12 / C 3.3f21 D 6f11 C 5f12 6f22

b)

because we are given that f is harmonic, that is, f11 .u; v/ C f22 .u; v/ D 0.

2f22 /

Finally, u is harmonic by Exercise 10 of Section 3.4, and, by symmetry, so is v. Thus

@2 z @ D .3f1 2f2 / @t 2 @t D 3.3f11 2f12 / 2.3f21 2f22 / D 9f11 12f12 C 4f22 y x ,vD . Then 16. Let u D 2 x C y2 x2 C y2 c)

@u y2 x2 D 2 @x .x C y 2 /2 2xy @u D @y .x 2 C y 2 /2

@2 @2 f .u; v/ C 2 f .u; v/ D 0 2 @x @y

@v 2xy D 2 @x .x C y 2 /2 y2 x2 @v D 2 : @y .x C y 2 /2

17.

@ @u @v f .u; v/ D f1 .u; v/ C f2 .u; v/ @x @x @x @u @v @ f .u; v/ D f1 .u; v/ C f2 .u; v/ @y @y @y  2 @u @v @u @2 u @2 C f f .u; v/ D f C f 12 11 1 @x 2 @x @x @x @x 2  2 @u @v @2 v @v C f21 C f2 2 C f22 @x @x @x @x  2 @u @v @u @2 u @2 C f12 f .u; v/ D f11 C f1 2 @y 2 @y @y @y @y  2 @2 v @v @u @v C f2 2 : C f22 C f21 @y @y @y @y 

2

@u @u 1 C D 2 D @x @y .x C y 2 /2 @u @v @u @v C D 0; @x @x @y @y



@v @x

2

C



@v @y

is harmonic for

If x D t sin s and y D t cos s, then

C t .cos2 s

18.

@2 @3 f .2x C 3y; xy/ D .3f1 C xf2 / 2 @x@y @x@y @ .9f11 C 3xf12 C 3xf21 C x 2 f22 / D @x @ D .9f11 C 6xf12 C x 2 f22 / @x D 18f111 C 9yf112 C 6f12 C 12xf121 C 6xyf122 C 2xf22 C 2x 2 f221 C x 2 yf222

D 18f111 C .12x C 9y/f112 C .6xy C 2x 2 /f122 C x 2 yf222 C 6f12 C 2xf22 ;

2

where all partials are evaluated at .2x C 3y; xy/.

we have @2 @2 f .u; v/ C 2 f .u; v/ 2 @x @y "   2 # @u @u 2 C D f11 @x @y "   2 # 2 @v @v C C f22 @x @y   @u @v @u @v C 2f12 C @x @x @y @y  2   2  @2 u @2 v @ u @ v C 2 C f2 C 2 C f1 @x 2 @y @x 2 @y  2  2 2  2  @ u @ v @ v @ u C 2 C f2 C 2 ; D f1 @x 2 @y @x 2 @y

sin2 s/f12 ;

where all partials of f are evaluated at .t sin s; t cos s/.

19.

464



sin sf2 C t cos2 sf12 t sin s cos sf22 D cos sf1 sin sf2 C t cos s sin s.f11 f22 /

Noting that 2

y x2 C y2

 @ @2 f .x; y/ D sin sf1 .x; y/ C cos sf2 .x; y/ @s@t @s D cos sf1 C t sin s cos sf11 t sin2 sf12

We have





x ; x2 C y2 .x; y/ ¤ .0; 0/.

and f

20.

@2 @ f .y 2 ; xy; x 2 / D .yf2 2xf3 / @y@x @y D f2 C 2y 2 f21 C xyf22 4xyf31 2x 2 f32 ; where all partials are evaluated at .y 2 ; xy; x 2 /. @3 @2 f .s 2 t; s C t 2 / D 2 .2sf1 C f2 / 2 @t @s @t @ D . 2sf11 C 4stf12 f21 C 2tf22 / @t @ D . 2sf11 C .4st 1/f12 C 2tf22 / @t D 2sf111 4stf112 C 4sf12 .4st 1/f121 C 2t .4st

1/f122 C 2f22

2tf221 C 4t 2 f222

D 2sf111 C .1 8st /f112 C 4t .2st 1/f122 C 4t 2 f222 C 4sf12 C 2f22 ; where all partials are evaluated at .s 2 t; s C t 2 /.

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21.

SECTION 12.5

Let g.x; y/ D f .u; v/, where u D u.x; y/, v D v.x; y/. Then

Therefore we have

@z @z @z D e s cos t C e s sin t @s @x @y @z @z @z D e s sin t C e s cos t @t @x @y @z @z @2 z D e s cos t C e s sin t @s 2 @x @y   @2 z @2 z C e s cos t e s cos t 2 C e s sin t @x @y@x   2 @ z @2 z C e s sin t e s cos t C e s sin t 2 @x@y @y @z @z @2 z D e s cos t e s sin t @t 2 @x @y   2 @2 z @ z e s sin t e s sin t 2 C e s cos t @x @y@x   2 @ z @2 z C e s cos t e s sin t C e s cos t 2 : @x@y @y

g1 .x; y/ D f1 .u; v/u1 .x; y/ C f2 .u; v/v1 .x; y/ g2 .x; y/ D f1 .u; v/u2 .x; y/ C f2 .u; v/v2 .x; y/

g11 .x; y/ D f1 .u; v/u11 .x; y/ C f11 .u; v/.u1 .x; y//2 C f12 .u; v/u1 .x; y/v1 .x; y/ C f2 .u; v/v11 .x; y/

C f21 .u; v/u1 .x; y/v1 .x; y/ C f22 .u; v/.v1 .x; y//2

g22 .x; y/ D f1 .u; v/u22 .x; y/ C f11 .u; v/.u2 .x; y//2 C f12 .u; v/u2 .x; y/v2 .x; y/ C f2 .u; v/v22 .x; y/

C f21 .u; v/u2 .x; y/v2 .x; y/ C f22 .u; v/.v2 .x; y//2 g11 .x; y/ C g22 .x; y/ D f1 .u; v/Œu11 .x; y/ C u22 .x; y/ C f2 .u; v/Œv11 .x; y/ C v22 .x; y/ C Œ.u1 .x; y//2 C .u2 .x; y//2 f11 .u; v/

C Œ.v1 .x; y//2 C .v2 .x; y//2 f22 .u; v/ C 2Œu1 .x; y/v1 .x; y/ C u2 .x; y/v2 .x; y/f12 .u; v/: The first two terms on the right are zero because u and v are harmonic. The next two terms simplify to Œ.v1 /2 C .v2 /2 Œf11 C f22  D 0 because u and v satisfy the Cauchy-Riemann equations and f is harmonic. The last term is zero because u and v satisfy the Cauchy-Riemann equations. Thus g is harmonic.

It follows that  2  @ z @2 z @2 z @2 z 2s 2 2 C 2 D e .cos t C sin t / C 2 @s 2 @t @x 2 @y  2  2 @ z @ z D .x 2 C y 2 / C 2 : @x 2 @y

@r x @r D 2x, so D . @x @x r @r y @r z 1 Similarly, D and D . If u D , then @y r @z r r

22. If r 2 D x 2 C y 2 C z 2 , then 2r

@u D @x @2 u D @x 2

(PAGE 711)

1 @r x D r 2 @x r3 1 3x x 3x 2 r 2 C 4 : D 3 r r r r5

Similarly, @2 u 3y 2 r 2 D ; @y 2 r5

@2 u 3z 2 r 2 D : @z 2 r5 24.

Adding these three expressions, we get @2 u @2 u @2 u C 2 C 2 D 0; 2 @x @y @z

If x D r cos  and y D r sin  , then r 2 D x 2 C y 2 and @r x @r D 2x, so D D cos  , and tan  D y=x. Thus 2r @x @x r @r y similarly, D D sin  . Also @y r

so u is harmonic except at r D 0. 23. If x D e s cos t and y D e s sin t , then @x D e s cos t @s @x D e x sin t @t

sec2 

@y D e s sin t @s @y D e s cos t: @t

@ D @x @ D @x D

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y x2 y C y2 sin  r x2

sec2 

1 @ D @y x @ x D 2 @x x C y2 cos  : D r

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ADAMS and ESSEX: CALCULUS 9

Now @u @u @r @u @ @u sin  @u D C D cos  @x @r @x @ @x @r r @ @u @u @r @u @ @u cos  @u D C D sin  C @y @r @y @ @y @r r @     @ @u @2 u sin  @2 u @2 u D cos  C cos  cos  @x 2 @x @r @r 2 r @ @r     @ sin  @u sin  sin  @2 u @2 u cos  @x r @ r @r@ r @ 2 2 2 2 sin  cos  @u @ u sin  @u C C cos2  2 D r @r r2 @ @r sin2  @2 u 2 sin  cos  @2 u C 2 r  @r@ @ 2  r  2 @ u @ @u cos  @2 u @2 u D C sin  C sin  sin  @y 2 @y @r @r 2 r @ @r     2 cos  cos  @2 u @ u @ cos  @u C C sin  C @y r @ r @r@ r @ 2 2 2 cos  @u 2 sin  cos  @u @ u D C sin2  2 r @r r2 @ @r cos2  @2 u 2 sin  cos  @2 u : C C r @r@ r 2 @ 2

27.

n X

i;j D1

2

n X

xi fi .tx1 ;    ; txn / D k t k

iD1 n X

i;j D1

28.

i1 ;:::;im D1

25. If u D r 2 ln r, where r 2 D x 2 C y 2 , then, since @r=@x D x=r and @r=@y D y=r, we have x D x.1 C 2 ln r/ r 2x 2 D 1 C 2 ln r C 2 r 2y 2 D 1 C 2 ln r C 2 (similarly) r @2 u 2.x 2 C y 2 / C 2 D 2 C 4 ln r C D 4 C 4 ln r: @y r2

The constant 4 is harmonic, and so is 4 ln r by Exercise 11 @2 u @2 u of Section 3.4. Therefore C 2 is harmonic, and so 2 @x @y u is biharmonic. 26.

f .tx; ty/ D t k f .x; y/

xf1 .tx; ty/ C yf2 .tx; ty/ D k t k 1 f .x; y/   x xf11 .tx; ty/ C yf12 .tx; ty/   C y xf21 .tx; ty/ C yf22 .tx; ty/

D k.k 1/t k Put t D 1 and get

2

x 2 f11 .x; y/C2xyf12 .x; y/Cy 2 f22 .x; y/ D k.k 1/f .x; y/:

466

1/t k

2

f .x1 ;    ; xn /;

29.

xi1    xim fi1 :::im .x1 ;    ; xn / D k.k

1/    .k

m C 1/f .x1 ;    ; xn /:

The proof is identical to those of Exercises 26 or 27, except that you differentiate m times before putting t D 1. 8 < 2xy.x 2 y 2 / if .x; y/ ¤ .0; 0/ 2 2 F .x; y/ D : x Cy 0 if .x; y/ D .0; 0/ a) For .x; y/ ¤ .0; 0/, F .x; y/ D

2xy.x 2 y 2 / D x2 C y2

Since 0 D

2xy.y 2 x 2 / D x2 C y2

F .y; x/:

0, this holds for .x; y/ D .0; 0/ also.

b) For .x; y/ ¤ .0; 0/, @ @ F .x; y/ D F .y; x/ D F2 .y; x/ @x @x @ @ F12 .x; y/ D F1 .x; y/ D F2 .y; x/ D F21 .y; x/: @y @y F1 .x; y/ D

c) If .x; y/

f .x; y/

f =x n

If f .x1 ;    ; xn / is positively homogeneous of degree k and has continuous partial derivatives of mth order, then

as was to be shown.

D .2r ln r C r/

1

xi xj fij .tx1 ;    ; txn / D k.k

n X

@ u @ u @ u 1 @u 1 @ u C 2 D 2 C C 2 ; @x 2 @y @r r @r r @ 2

@u @x @2 u @x 2 @2 u @y 2 @2 u @x 2

1/f .x1 ;    ; xn /:

and then put t D 1.

2

2

x1 xj fij .x1 ;    ; xn / D k.k

Proof: Differentiate f .tx1 ;    ; txn / D t k f .x1 ;    ; xn / twice with respect to t :

Therefore 2

If f .x1 ;    ; xn / is positively homogeneous of degree k and has continuous partial derivatives of second order, then

¤

.0; 0/, @ x2 y2 2y.x 2 y 2 / C 2xy . then F1 .x; y/ D 2 2 x Cy @x x 2 C y 2 Thus F1 .0; y/ D 2y C 0 D 2y for y ¤ 0. This result holds for y D 0 also, since F1 .0; 0/ D limh!0 .0 0/= h D 0:.

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d) By (b) and (c), F2 .x; 0/ D F21 .0; 0/ D 2. 30.

SECTION 12.5

F1 .0; x/ D 2x, and

and hence

a) Since F12 .x; y/ D F21 .y; x/ for .x; y/ ¤ .0; 0/, we have F12 .x; x/ D F21 .x; x/ for x ¤ 0. However, all partial derivatives of the rational function F are continuous except possibly at the origin. Thus F12 .x; x/ D F21 .x; x/ for x ¤ 0. Therefore, F12 .x; x/ D 0 for x ¤ 0. b) F12 cannot be continuous at .0; 0/ because its value there (which is 2) differs from the value of F21 .0; 0/ (which is 2). Alternatively, F12 .0; 0/ is not the limit of F12 .x; x/ as x ! 0.

u.x; t / D f .x C ct / C g.x

34.

that is,

ct /:

By Exercise 39, the DE u t D c 2 uxx has solution u.x; t / D f .x C ct / C g.x

ct /;

for arbitrary sufficiently smooth functions f and g. The initial conditions imply that p.x/ D u.x; 0/ D f .x/ C g.x/ q.x/ D u t .x; 0/ D cf 0 .x/ cg 0 .x/:

@u @u D c , then v satisfies If u satisfies @t @x @v @v @v Dc Cc ; @ @ @

@2 w D 0: @r@s

By Exercise 38, w.r; s/ D f .r/ C g.s/, where f and g are arbitrary twice differentiable functions. Hence the original differential equation has solution

31. If  D x C ct ,  D x, and v.; / D v.x C ct; x/ D u.x; t /, then @u @v @ @v D Dc @t @ @t @ @v @ @v @ @v @v @u D C D C : @x @ @x @ @x @ @

c

(PAGE 711)

Integrating the second of these equations, we get

@v D 0: @

f .x/

Thus v is independent of , so v.; / D f ./ for an arbitrary differentiable function f of one variable. The original differential equation has solution

g.x/ D

1 c

Z

x

q.s/ ds; a

where a is a constant. Solving the two equations for f and g we obtain

u.x; t / D f .x C ct /:

Z x 1 1 q.s/ ds p.x/ C 2 2c a Z x 1 1 q.s/ ds: g.x/ D p.x/ 2 2c a

f .x/ D 32. If w.r/ D f .r/ C g.s/, where f and g are arbitrary twice differentiable functions, then @ 0 @2 w D g .s/ D 0: @r@s @r

Thus the solution to the initial-value problem is p.x C ct / C p.x u.x; t / D 2

33. If r D x C ct , s D x ct , and w.r; s/ D w.x C ct; x ct / D u.x; t /, then @u @t @2 w @t 2 @u @x @2 w @x 2

@2 u @2 u D c 2 2 , then w satisfies 2 @t @x   2 2 2  @ w @2 w @ w @2 w @ w 2 C 2 C 2 D c2 C @r@s @s @r 2 @r@s @s 2

If u satisfies c2



@2 w @r 2

@w @w c @r @s 2 @2 w @2 w 2@ w Dc 2c 2 C c2 2 2 @r @r@s @s @w @w D C @r @s 2 @ w @2 w @2 w D C2 C 2: 2 @r @r@s @s Dc

35.

ct /

1 C 2c

Z

xCct

q.s/ ds:

x ct

> f := u(r*cos(t),r*sin(t)): > simplify( diff(f,r$2) + (1/r)*diff(f,r) > +(1/r^2)*diff(f,t$2)); D2;2 .u/.r cos.t /; r sin.t // C D1;1 .u/.r cos.t /; r sin.t // which confirms the identity.

> g := f(x/(x^2+y^2),y/(x^2+y^2)): > simplify(diff(g,x$2)+diff(g,y$2));     y y x x ; ; C D .f / D1;1 .f / 2;2 x2 C y2 x2 C y2 x2 C y2 x2 C y2 : 2 2 2 .x C y /

36.

If f is harmonic, then the numerator is zero so g is harmonic.

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37. > >

ADAMS and ESSEX: CALCULUS 9

simplify(diff(diff( f(y^2,x*y,-x^2),x),y)); 2y 2 D1;2 .f / C xyD2;2 .f / C D2 .f / 4xyD1;3 .f / 2x 2 D2;3 .f /

3.

where all terms are evaluated at .y 2 ; xy; x 2 /. 38. > simplify(diff(diff > (f(s^2-t,s+t^2),s),t$2)); 2sD1;1;1 .f / 8stD1;1;2 .f / C 8st 2 D1;2;2 .f / C 4sD1;2 .f / CD1;1;2 .f / 4tD1;2;2 .f / C 4t 2 D2;2;2 .f / C 2D2;2 .f / where all terms are evaluated at .s 2

39. > > > >

4.

t; s C t 2 /.

z := u(x,y): x := exp(s)*cos(t): y := exp(s)*sin(t): simplify( (diff(z,s$2)+diff(z,t$2))/(x^2+y^2)); D2;2 .u/.e s cos t; e s sin t / C D1;1 .u/.e s cos t; e s sin t /;

which confirms the identity in Exercise 23.

f .x; y/ D sin.xy C ln y/, f .0; 1/ D 0 f1 .x; y/ D  y cos.xy  C ln y/, f1 .0; 1/ D  1 cos.xy C ln y/, f2 .0; 1/ D 1 f2 .x; y/ D x C y f .0:01; 1:05/  f .0; 1/ C 0:01f1 .0; 1/ C 0:05f2 .0; 1/ D 0 C 0:01 C 0:05  0:081416 24 x 2 C xy C y 2 24.x C 2y/ 24.2x C y/ ; f2 .x; y/ D 2 f1 .x; y/ D 2 .x C xy C y 2 /2 .x C xy C y 2 /2 f .2; 2/ D 2; f1 .2; 2/ D 1; f2 .2; 2/ D 1 f .x; y/ D

f .2:1; 1:8/  f .2; 2/ C 0:1f1 .2; 2/ D 2 0:1 C 0:2 D 2:1

5.

40. > u := (x,t) -> (p(x-c*t)+p(x+c*t))/2 > +(1/((2*c))*int(q(s),x=xc*t..x+c*t): > simplify(diff(u(x,t),t$2) > -c^2*diff(u(x,t),x$2)); 0 > simplify(u(x,0)); p.x/ > simplify(subs(t=0,diff(u(x,t),t))); q.x/

f .x; y; z/ D

p

x C 2y C 3z, f .2; 2; 1/ D 3 1 1 ; f2 .x; y; z/ D p f1 .x; y; z/ D p 2 x C 2y C 3z x C 2y C 3z 3 f3 .x; y; z/ D p 2 x C 2y C 3z f .1:9; 1:8; 1:1/  f .2; 2; 1/ 0:1f1 .2; 2; 1/ 0:2f2 .2; 2; 1/ C 0:1f3 .2; 2; 1/ 0:1 0:2 0:1 D3 C  2:967 6 3 2

so u satisfies the PDE and initial conditions given in Exercise 34.

f .x; y/ D x 2 y 3

f1 .x; y/ D 2xy 3

f2 .x; y/ D 3x 2 y 2

2.

f .3; 1/ D 9 f1 .3; 1/ D 6 f2 .3; 1/ D 27

f .3:1; 0:9/ D f .3 C 0:1; 1 0:1/  f .3; 1/ C 0:1f1 .3; 1/ 0:1f2 .3; 1/ D 9 C 0:6 2:7 D 6:9  y f .3; 3/ D f .x; y/ D tan 1 x 4 y 1 f1 .x; y/ D f1 .3; 3/ D x2 C y2 6 1 x f2 .3; 3/ D f2 .x; y/ D 2 x C y2 6 f .3:01; 2:99/ D f .3 C 0:01; 3 0:01/  f .3; 3/ C 0:01f1 .3; 3/ 0:01f2 .3; 3/ 0:01 0:01  0:01  D D 4 6 6 4 3  0:7820648

468

2

6.

f .x; y/ D xe yCx f .2; 4/ D 2 yCx 2 2 f1 .x; y/ D e .1 C 2x / f1 .2; 4/ D 9 2 f2 .x; y/ D xe yCx f2 .2; 4/ D 2 f .2:05; 3:92/  f .2; 4/ C 0:05f1 .2; 4/ C 0:08f2 .2; 4/ D 2 C 0:45 C 0:16 D 2:61

7.

We have dz D 2xe 3y dx C 3x 2 e 3y dy. If x D 3 and y D 0, then z D 9. If also dx D 0:05 and dy D 0:02, then dz D 6.0:05/ C 27. 0:02/ D 0:24. Thus z  0 0:24 D 8:76.

Section 12.6 Linear Approximations, Differentiability, and Differentials (page 722) 1.

0:2f2 .2; 2/

8.

9.

s2 2s dt . dx t t2 If s D t D 2, and ds D dt D 0:1, then g.s; t / D 2 and dg D 2.0:1/ 1. 0:1/ D 0:3. Thus g.2:1; 1:9/  2 C 0:3 D 2:3. We have dg D

x dx C y dy C z dz We have dF D p . x2 C y C 2 C z2 Also F .1; 2; 2/ D 3. If dx D dz D 0:3 and dy D 0:6,  1 1. 0:3/ C 2.0:6/ C 2. 0:3/ D 0:1. Thus then dF D 3 F .0:9; 2:2; 1:9/  3 C 0:1 D 3:1.

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lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 12.6

10. We have   du D sin.x C y/ C x cos.x C y/ dx C x cos.x C y/ dy. If x D y D =2, dx D 1=20, dy D 1=30, then u D 0  and     1   1  . and du D 0 C D 2 20 2 30 120  1  1 Therefore, at x D C ; y D , we have 2 20 2 30  . u 120 11.

If the edges are x, y, and z, and

dy dz 1 dx D D D , x y z 100

For x D 224, y D 158,  D 64ı D 64=180, dx D dy D 0:4, and d D 2ı D 2=180, we have dA 0:4 0:4 2 D C C .cot 64ı /  0:0213: A 224 158 180 The calculated area of the plot can be in error by a little over 2%. 15.

From the figure we have h D s tan  h D .s C x/ tan  D

then a) V D xyz ) d V D yz dx C xz dy C xy dz dV dx dy dz 3 ) D C C D : V x y z 100 The volume can be in error by about 3%. b) A D xy ) dA D y dx C x dy dx dy 2 dA D C D : ) A x y 100 The area of a face can be in error by about 2%. c) D 2 D x 2 C y 2 C z 2 ) 2D dD D 2x dx C 2y dy C 2z dz )

dD x 2 dx y 2 dy z 2 dz 1 D 2 C 2 C 2 D : D D x D y D z 100

The diagonal can be in error by about 1%. 12. V D 31  r 2 h ) d V D 32  rh dr C 13  r 2 dh. If r D 25 ft, h D 21 ft, and dr D dh D 0:5=12 ft, then dV D

 0:5 .2  25  21 C 252 /  73:08: 3 12

The calculated volume can be in error by about 73 cubic feet. p 13. S D  r r 2 C h2 , so



 h C x tan : tan 

Solving the latter equation for h, we obtain hD

x tan  tan  : tan  tan 

We calculate the values of h and its first partials at x D 100,  D 50ı ,  D 35ı : h  170 tan  tan  @h D  1:70 @x tan  tan  @h .tan  tan / sec2  tan  sec2  D x tan  @ .tan  tan /2 2 2 x tan  sec  D  491:12 .tan  tan /2 x tan2  sec2  @h  876:02: D @ .tan  tan /2 Thus dh  1:70 dx 491 d C 876 d. For dx D 0:1 m and jd j D jdj D 1ı D =180, the largest value of dh will come from taking d negative and d positive: dh  .1:70/.0:1/ C .491 C 876/

 p  r2  rh dS D  r 2 C h2 C p dh dr C p 2 2 r Ch r 2 C h2 p  252 C 25  21 0:5 D 252 C 212 C p  8:88: 12 252 C 212

(PAGE 722)

  24:03: 180

The calculated height of the tower is 170 m and can be in error by as much as 24 m. The calculation of the height is most sensitive to the accuracy of the measurement of .

The surface area can be in error by about 9 square feet. 14.

If the sides and contained angle of the triangle are x and y m and  radians, then its area A satisfies

h

1 xy sin  2 1 1 1 dA D y sin  dx C x sin  dy C xy cos  d 2 2 2 dA dx dy D C C cot  d: A x y AD

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 s

A

x

B

Fig. 12.6-15

469

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SECTION 12.6 (PAGE 722)

16.

ADAMS and ESSEX: CALCULUS 9

@w 2xy 3 2w x2y3 D D 4 4 z @x z x 3w 4w 3x 2 y 2 4x 2 y 3 @w @w D D D D : @y z4 y @z z5 x @w @w @w dw D dx C dy C dz @x @y @z dw dx dy dz D2 C3 4 : w x y z wD

Since x increases by 1%, then

21.

f .a C h; b C k/

f .a; b/ hf1 .a; b/ kf2 .a; b/ p h2 C k 2 approaches 0 as .h; k/ ! .0; 0/. Since the denominator of this fraction approaches zero, the numerator must also approach 0 or the fraction would not have a limit. Since the terms hf1 .a; b/ and kf2 .a; b/ both approach 0, we must have

1 dx D . Similarly, x 100

dy 2 dz 3 D and D . Therefore y 100 z 100

dw 2 C 6 12 w  D D w w 100

lim

18.

19.

20.

f .a; b/ D 0:

Thus f is continuous at .a; b/. 22. 4 ; 100

Let g.t / D f .a C t h; b C t k/. Then

g 0 .t / D hf1 .a C t h; b C t k/ C kf2 .a C t h; b C t k/:

If h and k are small enough that .a C h; b C k/ belongs to the disk referred to in the statement of the problem, then we can apply the (one-variable) Mean-Value Theorem to g.t / on Œ0; 1 and obtain

f.r;  / D .r cos ; r sin  /   cos  r sin  Df.r;  / D sin  r cos 

g.1/ D g.0/ C g 0 . /; for some  satisfying 0 <  < 1, i.e.,

f.R; ;  / D .R sin  cos ; R sin  sin ; R cos / 0 1 sin  cos  R cos  cos  R sin  sin  Df.R; ;  / D @ sin  sin  R cos  sin  R sin  cos  A cos  R sin  0  2  x C yz f.x; y; z/ D y 2 x ln z   2x z y Df.x; y; z/ D ln z 2y x=z   4 1 2 Df.2; 2; 1/ D 0 4 2 0 1 0:02 f.1:98; 2:01; 1:03/  f.2; 2; 1/ C Df.2; 2; 1/ @ 0:01 A 0:03       6 0:01 5:99 D C D 4 0:02 3:98 0 2 1 r s g.r; s; t / D @ r 2 t A s2 t 2 0 1 2rs r 2 0 2 r A Dg.r; s; t / D @ 2rt 0 0 2s 2t 1 0 6 1 0 Dg.1; 3; 3/ D @ 6 0 1 A 0 6 6 0 1 0:01 g.0:99; 3:02; 2:97/  g.1; 3; 3/ C Dg.1; 3; 3/ @ 0:02 A 0:03 0 1 0 1 0 1 3 0:04 2:96 D @ 3 A C @ 0:09 A D @ 2:91 A 0 0:30 0:30 470

Œf .a C h; b C k/

.h;k/!.0;0/

and w decreases by about 4%. 17.

If f is differentiable at .a; b/, then

f .a C h; b C k/ D f .a; b/ C hf1 .a C h; b C  k/ C kf2 .a C h; b C  k/: 23.

Apply Taylor’s Formula: g 00 . / 2Š for some  between 0 and 1 to g.t / D f .a C t h; b C t k/. We have g.1/ D g.0/ C g 0 .0/ C

g 0 .t / D hf1 .a C t h; b C t k/ C kf2 .a C t h; b C t k/ g 0 .0/ D hf1 .a; b/ C kf2 .a; b/

g 00 .t / D h2 f11 .a C t h; b C t k/ C 2hkf12 .a C t h; b C t k/ C k 2 f22 .a C t h; b C t k/:

Thus

f .a C h; b C k/ D f .a; b/ C hf1 .a; b/ C kf2 .a; b/ C

1 2 h f11 .a C h; b C  k/ C 2hkf12 .a C h; b C  k/ 2 !

C k 2 f22 .a C h; b C  k/

f D f .a C h; b C k/ f .a; b/ df D hf1 .a; b/ C kf2 .a; b/ ˇ ˇ ˇ ˇ ˇf df ˇ ˇ 1 ˇˇ  ˇh2 f11 .a C h; b C  k/ C 2hkf12 .a C h; b C  k/ 2ˇ ˇ ˇ ˇ 2 C k f22 .a C h; b C  k/ˇ ˇ  K.h2 C k 2 /

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.since 2hk  h2 C k 2 /;

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 12.6

for some K depending on f , and valid in some disk h2 C k 2  R2 of positive radius R. 24.

29.

3

2p . Thus 3p

f  .p/ D xp

@E @E @E @E CV C N1 C    C Nn EDS @S @V @N1 @Nn D ST P V C 1 N1 C    C n Nn :

30.

Now calclate the differential of this equation:

dG D

P d V C 1 dN1 C    C n dNn

@G @G dT C dP: @T @P

We conclude that, @G D @T

@G D V: @P

and

S

V dP C N1 d1 C    C Nn dn ;

showing that the intensive variables are not independent.

31.

25. By direct calculation

1 @S D ; @E T

If f .x/ D x 2 , then f 0 .x/ D 2x D p. Thus x D p=2, and x2 D x2 D

x 4 D 3x 4 D 3

n dNn ;

@S P D ; @V T

and

@S D @Ni

i : T

dˆ D dS D

Ed



1 T



E P dT C dV T2 T

1 dE T 1 dN1 T

Thus ˆ D ˆ.T; V; N1 ;    ; Nn /. 32.

We start with the differential of H D X  @H i

dqi C

@H dpi @pi



@qi X qPi dpi C pi d qPi D i

 P

i

@L dqi @qi

n dNn : T

pi qPi

L.

 @L d qPi : @qPi

2

p : 4

28. If f .x/ D x 4 , then f 0 .x/ D 4x 3 D p, so that x D .p=4/1=3 . Thus f .x/ D 4x 4



Therefore we have

26. To maximize g.x/ D px f .x/ we look for a critical point. Thus we want 0 D g 0 .x/ D p f 0 .x/, so that the critical point of g satisfies f 0 .x/ D p. Since g 00 .x/ D f 00 .x/ > 0 for all x, f 0 is increasing (and so invertible), and the critical point must provide a maximum value for g. Now f 0 .x/ D p can be solved for x as a function of p and so the maximum must satisfy g.x.p// D px.p/ f .x.p//. Comparing this equation with f  .p/ D px f .x/ shows that f  .p/ must be that maximum value of g.

f .x/ D 2x 2

1 dN1

from which we conclude that

2 3 @E D E ) E D N kT; @S 3N k 2 2 @ 2 @E 2E P D D EV 3 V 3 D @V @V 3V 2 ) P V D E D N kT: 3

f  .p/ D px

From the Gibbs equation T dS D dE C P d V

T D

f  .p/ D xp

  3 : p

Since G depends only on T and P ,

from the above result leaves us with the Gibbs-Duhem equation

27.

ln

Fixed numbers mean dNi D 0 for all i .

Subtracting Gibbs equation

0 D S dT

2p 3

ln.2 C 3x/ D 1

dG D dE T dS S d T C P d V C V dP D T dS P d V T dS S d T C P d V C V dP D S d T C V dP:

dE D S d T C T dS P d V V dP C 1 dN1 C N1 d1 C    C n dNn C Nn dn :

dE D T dS

3 , so that 2 C 3x

If f .x/ D ln.2 C 3x/, then p D f 0 .x/ D xD

Since E.S; V; N1 ; : : : ; Nn / is homogeneous of degree 1, Euler’s Theorem tells us that

(PAGE 722)

 p 4=3 4

:

(a) Since each variable qPi on the right side has been replaced by pi on the left side, the conjugate pairs for this Legendre transformation are the pairs fpi ; qPi g, (1  i  n). Also, since there are no differentials d qP i on the left side, the coefficients of these differentials on the right side @L D pi , for 1  i  n. must vanish. Thus @qPi

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471

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SECTION 12.6 (PAGE 722)

ADAMS and ESSEX: CALCULUS 9

(b) Comparing the coefficients of the remaining differentials on the left and right sides and using the principle of least action, we have @H D @qi 1 2 2 .q C @H D p. @p

(c) H D qP D

@L D @qi

pPi

and

p 2 /, thus pP D

Thus qR D pP D

5.

@H D qPi : @pi @H @q

D

q and

q or qR C q D 0.

f .x; y/ D x 2 y 2 ; f .2; 1/ D 3. rf .x; y/ D 2xi 2yj, rf .2; 1/ D 4i C 2j. Tangent plane to z D f .x; y/ at .2; 1; 3/ has equation 4.x 2/ C 2.y C 1/ D z 3, or 4x C 2y z D 3. Tangent line to f .x; y/ D 3 at .2; 1/ has equation 4.x 2/ C 2.y C 1/ D 0, or 2x C y D 3. x y ; f .1; 1/ D 0. xCy 2yi 2xj , rf D .x C y/2 1 rf .1; 1/ D .i j/. Tangent plane to z D f .x; y/ 2 at .1; 1; 0/ has equation 21 .x 1/ 21 .y 1/ D z, or x y 2z D 0. Tangent line to f .x; y/ D 0 at .1; 1/ has equation 1 .x 1/ 12 .y 1/, or x D y. 2 f .x; y/ D f1 .x; y/ D f2 .x; y/ D rf .x; y/ D rf .1; 2/ D

x ; x2 C y2 .x 2 C y 2 /.1/ x.2x/ y2 x2 D ; .x 2 C y 2 /2 .x 2 C y 2 /2 2xy : .x 2 C y 2 /2   1 .y 2 x 2 /i 2xyj ; 2 2 2 .x C y / 3 4 25 i 25 j:

7.

f .x; y; z/ D x 2 y C y 2 z C z 2 x, f .1; 1; 1/ D 1. rf .x; y; z/ D .2xy C z 2 /i C .x 2 C 2yz/j C .y 2 C 2zx/k, rf .1; 1; 1/ D i j C 3k. Tangent plane to f .x; y; z/ D 1 at .1; 1; 1/ has equation .x 1/ .y C 1/ C 3.z 1/ D 0, or x C y 3z D 3.

8.

f .x; y; z/ D cos.x C 2y C 3z/,   11 f ; ;  D cos D 0. 2 2 rf .x; y; z/ D sin.x C 2y C 3z/.i C 2j C 3k/,   11 ; ;  D sin .i C 2j C 3k/ D i C 2j C 3k: rf 2 2   Tangent plane to f .x; y; z/ D 0 at ; ;  has equation 2

472

f .x; y/ D

x

 C 2.y 2

or x C 2y C 3z D 9.

Tangent plane to z D f .x; y/ at .1; 2; 15 / has equation 3 4 1 .x 1/ .y 2/ D z , or 3x 4y 25z D 10. 25 25 5 Tangent line to f .x; y/ D 1=5 at .1; 2/ has equation 3 4 .x 1/ .y 2/ D 0, or 3x 4y D 5. 25 25 4. f .x; y/ D e xy ; rf D ye xy i C xe xy j, rf .2; 0/ D 2j. Tangent plane to z D f .x; y/ at .2; 0; 1/ has equation 2y D z 1, or 2y z D 1. Tangent line to f .x; y/ D 1 at .2; 0/ has equation y D 0.

p

1 C xy 2 , f .2; 2/ D 3. y 2 i C 2xyj rf .x; y/ D p , 2 1 C xy 2 2 4 rf .2; 2/ D i j. 3 3 Tangent plane to z D f .x; y/ at .2; 2; 3/ has equation 4 2 .x 2/ .y C 2/ D z 3, or 2x 4y 3z D 3. 3 3 Tangent line to f .x; y/ D 3 at .2; 2/ has equation 2 4 .x 2/ .y C 2/ D 0, or x 2y D 6. 3 3

2. f .x; y/ D

3.

rf .x; y/ D

6.

Section 12.7 Gradients and Directional Derivatives (page 733) 1.

2xi C 2yj , x2 C y2 2 4 rf .1; 2/ D 5 i 5 j. Tangent plane to z D f .x; y/ at 2 4 .1; 2; ln 5/ has equation .x 1/ .y C 2/ D z ln 5, 5 5 or 2x 4y 5z D 10 5 ln 5. Tangent line to f .x; y/ D ln 5 at .1; 2/ has equation 2 4 .x 1/ .y C 2/ D 0, or x 2y D 5. 5 5 f .x; y/ D ln.x 2 C y 2 /;

10.

/ C 3.z

/ D 0;

11 . 2

p 2 f .x; y; z/ D ye x sin z, f .0; 1; =3/ D 3=2. 2 2 2 x rf .x; y; z/ D 2xye sin ziCe x sin zjCye x cos zk, p 3 1 j C k. rf .0; 1; =3/ D 2 2 p 3 The tangent plane to f .x; y; z/ D at 0; 1; =3/ has 2 equation p 3 1  .y 1/ C z D 0; 2 2 3 p p  or 3y C z D 3 C . 3 f .x; y/ D 3x D i f .0; 2/ D

4y; i  .3i

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rf .0; 2/ D rf .x; y/ D 3i 4j/ D 3:

4j;

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INSTRUCTOR’S SOLUTIONS MANUAL

11.

12.

SECTION 12.7

f .x; y/ D x 2 y; rf D 2xyi C x 2 j, rf . 1; 1/ D 2i C j. Rate of change of f at . 1; 1/ in the direction of i C 2j is 4 i C 2j p  .2i C j/ D p : 5 5

f .x; y/ D

x ; 1Cy

rf .x; y/ D

i j uD p ;   2 i j 1 Du f .0; 0/ D i  p D p : 2 2

1 i 1Cy

Therefore, @f 1 @f O rO C  @r  r @  @f @f C sin  cos  i D cos2  @x @y   @f @f C cos  sin  C sin2  j @x @y   @f @f C sin2  sin  cos  i @x @y   @f @f C cos  sin  C cos2  j @x @y @f @f iC j D rf: D @x @y

x j; .1 C y/2

rf .0; 0/ D i;

13. f .x; y/ D x 2 C y 2 ; rf D 2xi C 2yj, rf .1; 2/ D 2i 4j. A unit vector in the directionpmaking a 60ı angle with the positive x-axis is u D 12 i C 23 j. The rate of change of fp at .1; 2/ in the direction of u is u  rf .1; 2/ D 1 2 3. 14.

15.

17.



p 1 3 , and therefore u1 D ˙ . At .2; 0/, f has 2 2p 1 3 rate of change 1 in the directions ˙ i j. 2 2 3 If 3 D Du f .2; 0/ D 2u2 , then u2 D . This is 2 not possible for a unit vector u, so there is no direction at .2; 0/ in which f changes at rate 3.

if u2 D

 x y r iC j D 2: jrj jrj jrj

n f .x; y; pz/ D jrj , where r D xi C yj C zk. Since 2 2 jrj D x C y C z 2 , we have

rf .x; y; z/ D D

njrj

n 1

nr : jrjnC2



 x y z iC jC k jrj jrj jrj

If 2 D Du f .2; 0/ D 2u2 , then u2 D 1 and u1 D 0. At .2; 0/, f has rate of change 2 in the direction j. 18. f .x; y; z/ D x 2 C y 2 z 2 . rf .a; b; c/ D 2ai C 2bj 2ck. The maximum rate of change of f at .a; b; c/ is in the direction of rf .a; b; c/, and is equal to jrf .a; b; c/j. Let u be a unit vector making an angle  with rf .a; b; c/. The rate of change of f at .a; b; c/ in the direction of u will be half of the maximum rate of change of f at that point provided 1 jrf .a; b; c/j D u  rf .a; b; c/ D jrf .a; b; c/j cos ; 2

16. Since x D r cos  and y D r sin  , we have @f @f @f D cos  C sin  @r @x @y @f @f @f D r sin  C r cos  : @ @x @y

1 , which means  D 60ı . At .a; b; c/, 2 f increases at half its maximal rate in all directions making 60ı angles with the direction ai C bj ck. that is, if cos  D

19. Also, xi C yj D .cos  /i C .sin  /j r yi C xj D .sin  /i C .cos  /j: O D r rO D

f .x; y/ D xy, rf .x; y/ D yi C xj, rf .2; 0/ D 2j. Let u D u1 i C u2 j be a unit vector. Thus u21 C u22 D 1. We have 1 D Du f .2; 0/u  rf .2; 0/ D 2u2

f .x; y/ p D ln jrj, where r D xi C yj. Since jrj D x 2 C y 2 , we have 1 rf .x; y/ D jrj

(PAGE 733)

Let rf .a; b/ D ui C vj. Then p iCj uCv 3 2 D D.iCj/=p2 f .a; b/ D p  .ui C vj/ D p 2 2 3i 4j 3u 4v 5 D D.3i 4j/=5 f .a; b/ D  .ui C vj/ D : 5 5

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ADAMS and ESSEX: CALCULUS 9

Thus u C v D 6 and 3u 4v D 25. This system has solution u D 7, v D 1. Thus rf .a; b/ D 7i j.

e) To continue to experience maximum rate of cooling, the ant should crawl along the curve x D x.t /, y D y.t /, which is everywhere tangent to rT .x; y/. Thus we want

20. Given the values D1 f .a; b/ and D2 f .a; b/, we can solve the equations

dy dx iC j D .2xi dt dt 1 dy D y dt integration,

f1 .a; b/ cos 1 C f2 .a; b/ sin 1 D D1 f .a; b/ f1 .a; b/ cos 2 C f2 .a; b/ sin 2 D D2 f .a; b/

Thus 1 and 2 must not differ by an integer multiple of .

21.

a) T .x; y/ D x 2

ln jy.t /j D 2 ln jx.t /j C ln jC j; or yx 2 D C . Since the curve passes through .2; 1/, we have yx 2 D 4. Thus, the ant should crawl along the path y D 4=x 2 . 22.

Let the curve be y D g.x/. At .x; y/ this curve has normal r g.x/ y D g 0 .x/i j.

A curve of the family x 4 C y 2 D C has normal r.x 4 C y 2 / D 4x 3 i C 2yj. These curves will intersect at right angles if their normals are perpendicular. Thus we require that

2y 2 . y

0 D 4x 3 g 0 .x/

TD 8

or, equivalently,

TD 2

T D2 .2; 1/

g 0 .x/ 1 : D g.x/ 2x 3

2

TD 8

23. Fig. 12.7-21 b) rT D 2xi 4yj, rT .2; 1/ D 4i C 4j. An ant at .2; 1/ should move in the direction of rT .2; 1/, that is, in the direction i j, in order to cool off as rapidly as possible.

1 C ln jC j, 4x 2

Let the curve be y D f .x/. At .x; y/ it has normal dy i j. dx The curve x 2 y 3 D K has normal 2xy 3 i C 3x 2 y 2 j. These curves will intersect at right angles if their normals are perpendicular, that is, if dy 3x 2 y 2 D 0 dx dy 3x D dx 2y 2y dy D 3x dx 3 y 2 D x 2 C C: 2

2xy 3

c) If the ant moves at speed k in the direction i j, it will experience p temperature decreasing at rate jrT .2; 1/jk D 4 2k degrees per unit time. d) If the ant moves at speed k in the direction i 2j, it experiences temperature changing at rate

Since the curve must pass through .2; 1/, we have 1 D 6 C C , so C D 5. The required curve is 3x 2 2y 2 D 10.

12k p ; 5

p that is, decreasing at rate 12k= 5 degrees per unit time.

2g.x/;

or g.x/ D C e .1=4x / : Since the curve passes through .1; 1/, we must have 1 D g.1/ D C e 1=4 , so C D e 1=4 . 2 The required curve is y D e .1=4/ .1=4x / .

T D8

i 2j p  .4i C 4j/k D 5

2y D 4x 3 g 0 .x/

Integration gives ln jg.x/j D

x

T D0

474

2 dx , from which we obtain, on x dt

Thus

for unique values of f1 .a; b/ and f2 .a; b/ (and hence determine rf .a; b/ uniquely), provided the coefficients satisfy ˇ ˇ ˇ cos 1 sin 1 ˇ ˇ D sin.2 1 /: ˇ 0¤ˇ cos 2 sin 2 ˇ

4yj/:

24.

Let f .x; y/ D e

.x 2 Cy 2 /

rf .x; y/ D

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. Then 2e

.x 2 Cy 2 /

.xi C yj/:

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 12.7

ai C bj The vector u D p is a unit vector in the direction a2 C b 2 directly away from the origin at .a; b/. The first directional derivative of f at .x; y/ in the direction of u is u  rf .x; y/ D

p

2 a2 C b 2

.ax C by/e

.x 2 Cy 2 /

and y 2 C z 2 D 2 has normal ˇ ˇ n2 D r.y 2 C z 2 /ˇˇ

.1; 1;1/

.i

2

D 2 2.a2 C b 2 /

1 e

2a2 b 2 C b 2 2a2 b 2  2 2 a2 b 2 e .a Cb /

.a2 Cb 2 /

2b 4

27.

:

r Da Cb

25. f .x; y; z/ D xyz, rf .x; y; z/ D yzi C xzj C xyk. The first directional derivative of f in the direction i j k is k 3

1  rf .x; y; z/ D p .yz 3

xz

1  p r.yz xz xy/ 3 3 i i j k h  .y C z/i C .z x/j C .y x/k D 3 i 1h 2x 2y 2z D .y C z/ .z x/ .y x/ D : 3 3 j p

k

At .2; 3; 1/ this second directional derivative has value 4=3. 26. At .1; 1; 1/ the surface x 2 C y 2 D 2 has normal ˇ ˇ D 2i 2j; n1 D r.x 2 C y 2 /ˇˇ .1; 1;1/

Any vector parallel to i .1; 2; 3/. 28.

2j C k is tangent to the circle at

A vector tangent to the path of the fly at .1; 1; 2/ is given by ˇ ˇ v D r.3x 2 y 2 z/  r.2x 2 C 2y 2 z 2 /ˇˇ ˇ .1;1;2/ ˇ D .6xi 2yj k/  .4xi C 4yj 2zk/ˇˇ .1;1;2/

D .6i 2j k/  .4i C 4j 4k/ ˇ ˇ ˇi j k ˇˇ ˇ 2 1 ˇˇ D 4.3i C 5j C 8k/: D 4 ˇˇ 6 ˇ1 1 1ˇ

xy/:

The second directional derivative in that direction is i

The vector n1 D i C j C k is normal to the plane x C y C z D 6 at .1; 2; 3/. A normal to the sphere x 2 C y 2 C z 2 D 14 at that point is ˇ ˇ 2 2 2 ˇ D 2i C 4j C 6k: n2 D r.x C y C z /ˇ

A vector tangent to the circle of intersection of the two surfaces at .1; 2; 3/ is ˇ ˇ ˇ i j kˇ ˇ ˇ n1  n2 D ˇˇ 1 1 1 ˇˇ D 2i 4j C 2k: ˇ2 4 6ˇ

2

j p

.i C j C k/;

.1;2;3/



Remark: Since f .x; y/ D e r (expressed in terms of polar coordinates), the second directional derivative of f at .a; b/ in the direction directly away from the origin (i.e., the direction of increasing r) can be more easily calculated as ˇ d 2 r 2 ˇˇ e ˇ : ˇ2 2 2 dr 2

i

j/  . j C k/ D

the vector i C j C k, or any scalar multiple of this vector, is tangent to the curve at the given point.

At .a; b/ this second directional derivative is 2

2j C 2k:

A vector tangent to the curve of intersection of the two surfaces at .1; 1; 1/ must be perpendicular to both these normals. Since

:

The second directional derivative is   2 2 2 ur p .ax C by/e .x Cy / a2 C b 2 2 2 2 .ai C bj/  e .x Cy / D 2 C b2 a     a 2x.ax C by/ i C b 2y.ax C by/ j : 2e .a Cb /  2 a 2a4 a2 C b 2  2 2.a2 C b 2 /2 D 2 2 a C b 

D

(PAGE 733)

The temperature T D x 2 .1; 1; 2/ given by

y 2 C z 2 C xz 2 has gradient at

2

rT .1; 1; 2/ D .2x C z /i D 6i

2j C 8k:

ˇ ˇ 2yj C 2z.1 C x/kˇˇ

.1;1;2/

Thus the fly, passing through .1; 1; 2/ with speed 7, experiences temperature changing at rate 7

3i C 5j C 8k v  rT .1; 1; 2/ D 7 p  .6i 2j C 8k/ jvj 98 1 72 D p .18 10 C 64/ D p : 2 2

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y

We don’t know which direction the fly is moving along the curve, so all we canpsay is that it experiences temperature changing at rate 36 2 degrees per unit time.

y 3 Dx 2

29. If f .x; y; z/ is differentiable at the point .a; b; c/ and rf .a; b; c/ ¤ 0, then rf .a; b; c/ is normal to the level surface of f which passes through .a; b; c/. The proof is very similar to that of Theorem 6 of Section 3.7, modified to include the extra variable. The angle  between rf .a; b; c/ and the secant vector from .a; b; c/ to a neighbouring point .a C h; b C k; c C `/ on the level surface of f passing through .a; b; c/ satisfies

x

Fig. 12.7-32

33.

rf .a; b; c/  .hi C kj C `k/ p jrf .a; b; c/j h2 C k 2 C `2 hf1 .a; b; c/ C kf2 .a; b; c/ C `f3 .a; b; c/ D p jrf .a; b; c/j h2 C k 2 C `2 h 1 p D f .a C h; b C k; c C `/ jrf .a; b; c/j h2 C k 2 C `2

cos  D

f .a; b; c/

hf1 .a; b; c/

! 0 as .h; k; `/ ! .0; 0; 0/

kf2 .a; b; c/

@f @f @f C v2 C v3 Dv f D v1 @x @y @z   @2 f @2 f @2 f C v3 i r.Dv f / D v1 2 C v2 @x @x@y @x@z   @2 f @2 f @2 f C v2 2 C v3 j C v1 @y@x @y @y@z   @2 f @2 f @2 f C v1 C v2 C v3 2 k @x@z @y@z @z Dv .Dv f / D v  r.Dv f /

i `f3 .a; b; c/

 , and 2 rf .a; b; c/ is normal to the level surface of f through .a; b; c/.

@2 f @2 f @2 f C 2v v C 2v v 1 2 1 3 @x 2 @x@y @x@z 2 2 @ f @2 f @ f C v22 2 C 2v2 v3 C v32 2 @y @y@z @z

because f is differentiable at .a; b; c/. Thus  !

D v12

30. The level surface of f .x; y; z/ D cos.x C 2y C 3z/ through .; ; / has equation cos.x C 2y C 3z/ D cos.6/ D 1, which simplifies to x C 2y C 3z D 6. This level surface is a plane, and is therefore its own tangent plane. We cannot determine this plane by the method used to find the tangent plane to the level surface of f through .=2; ; / in Exercise 10, because rf .; ; / D 0, so the gradient does not provide a usable normal vector to define the tangent plane. 31. By the version of the Mean-Value Theorem in Exercise 18 of Section 3.6, f .x; y/ D f .0; 0/ C xf1 . x; y/ C yf2 . x; y/ for some  between 0 and 1. Since rf is assumed to vanish throughout the disk x 2 C y 2 < r 2 , this implies that f .x; y/ D f .0; 0/ throughout the disk, that is, f is constant there. (Note that Theorem 3 of Section 3.6 can be used instead of Exercise 18 of Section 3.6 in this argument.) 32. Let f .x; y/ D x 3 y 2 . Then rf .x; y/ D 3x 2 i 2yj exists everywhere, but equals 0 at .0; 0/. The level curve of f passing through .0; 0/ is y 2 D x 3 , which has a cusp at .0; 0/, so is not smooth there.

476

Let v D v1 i C v2 j C v3 k. Thus

(assuming all second partials are continuous). Dv .Dv f / gives the second time derivative of the quantity f as measured by an observer moving with constant velocity v.

34.

T D T .x; y; z/. As measured by the observer, dT D Dv.t/ T D v.t /  rT dt d 2T d D a.t /  rT C v.t /  rT dt 2 dt   d @T C  D Da.t/ T C v1 .t / dt @x   @T D Da.t/ T C v1 .t /v.t /  r C  @x    2 @2 T @2 T D Da.t/ T C v1 .t / C v .t /v .t / C    1 2 @x 2 @y@x D Da.t/ T C Dv.t/ .Dv.t/ T / (as in Exercise 37 above).

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 12.8

35. T D T .x; y; z; t /. The calculation is similar to that of Exercise 38, but produces a few more terms because of the dependence of T explicitly on time t . We continue to use r to denote the gradient with respect to the spatial variables only. Using the result of Exercise 38, we have dT @T D C v.t /  rT dt @t 2 d @T d d T D C v.t /  rT dt 2 dt @t dt 2 @ T @T D C v.t /  @t 2 @t @ C v.t /  rT C Da.t/ T C Dv.t/ .Dv.t/ T / @t   @2 T @T D C 2D C Da.t/ T C Dv.t/ .Dv.t/ T /: v .t/ @t 2 @t 8 < sin.xy/ p 2 2 36. f .x; y/ D : x Cy 0 a) f1 .0; 0/ D lim

h!0

if .x; y/ ¤ .0; 0/

1.

xy 3 C x 4 y D 2 defines x as a function of y. dx dx y3 C 3xy 2 C 4x 3 y C x4 D 0 dy dy dx x 4 C 3xy 2 D : dy y 3 C 4x 3 y The given equation has a solution x D x.y/ with this derivative near any point where y 3 C 4x 3 y ¤ 0, i.e., y ¤ 0 and y 2 C 4x 3 ¤ 0.

2.

xy 3 D y z: x D x.y; z/ 3 @x 2 y C 3xy D 1 @y @x 1 3xy 2 : D @y y3 The given equation has a solution x D x.y; z/ with this partial derivative near any point where y ¤ 0.

3.

z 2 C xy 3 D

0 h

rf .0; 0/ D 0.

p b) If u D .i C j/= 2, then

h!0C

1 1 sin.h2 =2/ p D : 2 h 2 h

4.

e yz  x 2 z ln y  D : y D y.x; z/ @y x 2 z @y yz 2 e z Cy x ln y D0 @z y @z x 2 ln y ye yz @y x 2 y ln y y 2 e yz D : D 2 @z yze yz x 2 z x z ze yz y The given equation has a solution y D y.x; z/ with this derivative near any point where y > 0, z ¤ 0, and ye yz ¤ x 2 .

5.

x 2 y 2 Cy 2 z 2 Cz 2 t 2 Ct 2 w 2 xw D 0: @x @x 2xy 2 C 2t 2 w w xD0 @w @w x 2t 2 w @x D : @w 2xy 2 w

c) f cannot be differentiable at .0; 0/; if it were, then the directional derivative obtained in part (b) would have been u  rf .0; 0/ D 0.

8 < 2x 2 y 37. f .x; y/ D x 4 C y 2 if .x; y/ ¤ .0; 0/ . : 0 if .x; y/ D .0; 0/ Let u D ui C vj be a unit vector. If v ¤ 0, then

1 2.h2 u2 /.hv/ Du f .0; 0/ D lim h!0C h h4 u4 C h2 v 2 2u2 2u2 v D : D lim 2 4 v h!0C h u C v 2

h!0C

1 0 D 0: h h2

Thus f has a directional derivative in every direction at the origin even though it is not continuous there.

Section 12.8 Implicit Functions

(page 743)

x D x.y; z; t; w/

The given equation has a solution with this derivative wherever w ¤ 2xy 2 .

If v D 0, then u D ˙1 and Du f .0; 0/ D lim D

z D z.x; y/

2z

D 0 D f2 .0; 0/. Thus

Du f .0; 0/ D lim

xz : y

x @z xz @z C 3xy 2 D @y y @y y2 xz C 3xy 2 xz C 3xy 4 @z y2 D x : D @y xy 2y 2 z 2z y The given equation has a solution z D z.x; y/ with this derivative near any point where y ¤ 0 and x ¤ 2yz.

.

if .x; y/ D .0; 0/

0

(PAGE 743)

6.

F .x; y; x 2 y 2 / D0: y D y.x/  dy dy F1 C F2 C F3 2x 2y D0 dx dx F1 .x; y; x 2 y 2 / C 2xF3 .x; y; x 2 dy D dx 2yF3 .x; y; x 2 y 2 / F2 .x; y; x 2

y2/ : y2/

The given equation has a solution with this derivative near any point where F2 .x; y; x 2 y 2 / ¤ 2yF3 .x; y; x 2 y 2 /.

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7.

ADAMS and ESSEX: CALCULUS 9

@x .4x w/ C 4y 2w D 0 @y   @x 2w 4y : D @y z 4x w

G.x; y; z; u; v/ D 0: u D u.x; y; z; v/ @u G1 C G4 @x G1 .x; y; z; u; v/ @u D : @x G4 .x; y; z; u; v/ The given equation has a solution with this derivative near any point where G4 .x; y; z; u; v/ ¤ 0.

8. F .x2 z 2 ; y 2 Cxz/ D  0: z Dz.x; y/ @z @z Cz D0 F1 2x 2z C F2 x @x @x 2xF1 .x 2 z 2 ; y 2 C xz/ C zF2 .x 2 z 2 ; y 2 C xz/ @z D : @x 2zF1 .x 2 z 2 ; y 2 C xz/ xF2 .x 2 z 2 ; y 2 C xz/

The given equations have a solution of the indicated form with this derivative near any point where w ¤ 4x.   u D u.x/ x 2 y C y 2 u u3 D 0 12. ) y D y.x/ x 2 C yu D 1 2xy 2x

The given equation has a solution with this derivative near any point where xF2 .x 2 z 2 ; y 2 C xz/ ¤ 2zF1 .x 2 z 2 ; y 2 C xz/.

.x 2 C 2yu/ dy u dx

C

C

1

C

@y @x @y @x

xuv

C

@v @x @v @x

xyu

du D dx

C

0

D

0

13.

478

C 2y

C

0 D

C

C

2

0

D

0

@u @x @u v @x

3u2

1 D

D

0

du D0 dx

x : 2u3

C

@v @x @v 2v/ : @x

3v 2

C .u

@u @x @u @x

3

C

@v @x @v : @x

3

@v 1 @u D D . @x @x 6 Similarly, differentiating the given equations with respect to y and putting u D v D 1, we get

Thus

0 D 1 D @u D @y Finally,

Thus D

0

Take partials with respect to x:

0 D

The given equations have a solution of the indicated form with this derivative near any point where u ¤ 0, x ¤ 0 and y ¤ v.   x D x.y; z/ x2 C y 2 C z2 C w2 D 1 ) w D w.y; z/ x C 2y C 3z C 4w D 2 @w 2w @y @w 4 @y

D

At u D v D 1 we have

@y D0 yuv xyu C .xuv xyu/ @x   @y y.x v/ D : @x u x.v y/

@x 2x @y @x @y

C

du dx

The given equations have a solution with the indicated derivative near any point where u ¤ 0.   u D u.x; y/ x D u3 C v 3 ) 2 v D v.x; y/ y D uv v

Multiply the last equation by xyu and subtract the two equations:

11.

3u2 / du y dx

2x.x 2 C yu/ D 3u3 C x 2 y C y 2 u

1 D

D

.y 2

C

2x.x 2 C yu/ C .x 2 y C y 2 u C 3u3 /

Differentiate the given equations with respect to x: yuv

dy dx

Multiply the first equation by u and the second by x 2 C 2yu and subtract:

9. H.u2 w; v 2 t; wt / D 0: w D w.u;v; t / @w @w H1 u2 C H2 v 2 C H3 t Cw D0 @t @t @w H2 .u2 w; v 2 t; wt /v 2 C H3 .u2 w; v 2 t; wt /w D : @t H1 .u2 w; v 2 t; wt /u2 C H3 .u2 w; v 2 t; wt /t

The given equation has a solution with this derivative near any point where tH3 .u2 w; v 2 t; wt / ¤ u2 H1 .u2 w; v 2 t; wt /.   xyuv D 1 y D y.x; u/ 10. ) xCy CuCv D0 v D v.x; u/

C

2 w

@u @y @u @y

3

C

@v @y @v : @y

3

@v 1 D . @y 2 ˇ1 ˇ @.u; v/ D ˇˇ 16 @.x; y/ 2

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1 6 1 2

ˇ ˇ ˇD ˇ

1 : 6

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INSTRUCTOR’S SOLUTIONS MANUAL

14.



x D r 2 C 2s y D s 2 2r

SECTION 12.8

At point P0 where x D y D z D u D v D 1, we have

ˇ ˇ 2r @.x; y/ D ˇˇ 2 @.r; s/

ˇ ˇ1 2 ˇ @.F; G; H / D ˇˇ 3 2 @.x; y; z/ ˇ0 0

ˇ 2 ˇˇ D 4.rs C 1/: 2s ˇ

The given system can be solved for r and s as functions of x and y near any point .r; s/ where rs ¤ 1. We have @r @s 1 D 2r C 2 @x @x @r @s 0 D 2 C 2s @x @x @s @r C 2 0 D 2r @y @y @r @s 1 D 2 C 2s : @y @y s @r D @x 2.rs C 1/ 1 @s D @x 2.rs C 1/ x D r cos ;

y D r sin  ˇ ˇ cos  @.x; y/ D ˇˇ sin  @.r;  /

@r 1 D @y 2.rs C 1/ r @s D : @y 2.rs C 1/



@y @u

 ˇˇ ˇ ˇ vˇ

.1;1/

D D D

ˇ @.F; G/ ˇˇ ˇ @.u; v/ ˇ

P0

16. x D R sin  cos  , y D R sin  sin  , z D R cos . ˇ ˇ ˇ sin  cos  R cos  cos  R sin  sin  ˇˇ ˇ @.x; y; z/ D ˇˇ sin  sin  R cos  sin  R sin  cos  ˇˇ @.R; ;  / ˇ ˇ cos  R sin  0 ˇ ˇ ˇ R cos  cos  ˇ R sin  sin  ˇ D cos  ˇˇ R cos  sin  R sin  cos  ˇ ˇ ˇ ˇ sin  cos  R sin  sin  ˇˇ C R sin  ˇˇ sin  sin  R sin  cos  ˇ h i D R2 cos  cos  sin  cos2  C sin  cos  sin2  h i C R2 sin  sin2  cos2  C sin2  sin2 

3

3

G.x; y; z; u; v/ D x z C 2y uv 2 H.x; y; z; u; v/ D xu C yv xyz 1: Then ˇ ˇ ˇ y2 2xy u ˇˇ ˇ @.F; G; H / 2 x 3 ˇˇ : D ˇˇ 3x 2 z @.x; y; z/ ˇ u yz v xz xy ˇ

2 2

ˇˇ ˇ ˇ z sin v ˇˇˇˇ ˇ Dˇ cos y x 2 ˇˇˇ P0 ˇ ˇ ˇ1 0ˇ ˇ ˇ Dˇ D 4: 1 4ˇ

Since this Jacobian is not zero, the equations F D G D 0 can be solved for u, and v in terms of x, y and z near P0 . Also, 

@u @z

ˇ ˇ ˇ ˇ x;y ˇ



.2;0;1/

D D D

D R2 cos2  sin  C R2 sin3  D R2 sin :

Let F .x; y; z; u; v/ D xy 2 C zu C v 2

cos v 2

G.x; y; z; u; v/ D u cos y C x v yz 1: If P0 is the point where .x; y; z/ D .2; 0; 1/ and .u; v/ D .1; 0/, then

The transformation is one-to-one (and hence invertible) near any point where r ¤ 0, that is, near any point except the origin.

17.

ˇ 1 @.F; G; H / ˇˇ ˇ 4 @.x; u; z/ ˇ P0 ˇˇ ˇ ˇ y2 z u ˇˇˇ 1 ˇˇ ˇ 3x 2 z v x 3 ˇˇˇ ˇ 4 ˇˇ u yz x ˇ xy P0 ˇ ˇ ˇ1 1 1 ˇˇ 1 ˇˇ ˇ D 3: 3 1 1 ˇ 4 ˇˇ 0 1 2 1ˇ

18. Let F .x; y; z; u; v/ D xe y C uz

ˇ r sin  ˇˇ D r: r cos  ˇ

The transformation is one-to-one (and invertible) near any point where R2 sin  ¤ 0, that is, near any point not on the z-axis.

ˇ 1 ˇˇ 1 ˇˇ D 4: 1ˇ

Since this Jacobian is not zero, the equations F D G D H D 0 can be solved for x, y, and z as functions of u and v near P0 . Also,

Thus

15.

(PAGE 743)

19.

8 < F .x; y; z; w/ G.x; y; z; w/ : H.x; y; x; w/

=0 =0 =0

)

ˇ 1 @.F; G/ ˇˇ ˇ 4 @.z; v/ ˇ P0 ˇ ˇˇ 1 ˇˇ u sin v ˇˇˇˇ 2 ˇ 4 ˇ 2yz x ˇˇ P0 ˇ ˇ 1 ˇˇ 1 0 ˇˇ D 1: 4 ˇ0 4ˇ 8

> >

(PAGE 751)

v := (r,p,t) -> u(r*sin(p)*cos(t), r*sin(p)*sin(t), r*cos(p));

and then asked Maple to calculate and simplify the left side of the identity: > > > > >

simplify(diff(v(r„p,t),r$2) +(2/r)*diff(v(r,p,t),r) +(cot(p)/r^2)*diff(v(r,p,t),p) +(1/r^2)*diff(v(r,p,t),p$2) +(1/(r*sin(p))^2)*diff(v(r,p,t),t$2));

Maple responded with D1;1 .u/ C D3;3 .u/ C D2;2 .u/; with all three terms evaluated at .r sin.p/ cos.t /; r sin.p/ sin.t /; r cos.p//, thus confirming the identity. 4. If u.x; y; z; t / D v.R; t / D and , then

f .R ct / is independent of  R

@2 u @2 u @2 u @2 v 2 @v C 2 C 2 D C 2 @x @y @z @R2 R @R

490

ADAMS and ESSEX: CALCULUS 9

by Problem 3. We have @v @R @2 v @R2 @v @t @2 v @t 2 @2 v @R2

f 0 .R ct / f .R ct / R R2 00 0 f .R ct / 2f .R ct / 2f .R ct / D C R R2 R3 cf 0 .R ct / D R c 2 f 00 .R ct / D R 2 @v C R @R 2f .R ct / f 00 .R ct / 2f 0 .R ct / C D R R2 R3 2f 0 .R ct / 2f .R ct / C R2 R3 f 00 .R ct / D R 1 @2 v 1 @2 u D 2 2 D 2 2: c @t c @t D

The function f .R ct /=R represents the shape of a symmetrical wave travelling uniformly away from the origin at speed c. Its amplitude at distance R from the origin decreases as R increases; it is proportional to the reciprocal of R.

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lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 13.1

1 Thus B 2 AC D 16 maximum.

CHAPTER 13. APPLICATIONS OF PARTIAL DERIVATIVES Section 13.1 Extreme Values 1.

f .x; y/ D cos.x C y/; f1 D sin.x C y/ D f2 . All points on the lines x C y D n (n is an integer) are critical points. If n is even, f D 1 at such points; if n is odd, f D 1 there. Since 1  f .x; y/  1 at all points in R2 , f must have local and absolute maximum values at points x C y D n with n even, and local and absolute minimum values at such points with n odd.

7.

f .x; y/ D x sin y. For critical points we have f1 D sin y D 0;

2. f .x; y/ D xy x C y; f1 D y 1; f2 D x C 1 A D f11 D 0; B D f12 D 1; C D f22 D 0. Critical point . 1; 1/ is a saddle point since B 2 AC > 0. 3.

3

f .x; y/ D x C y

3

A D f11 .x; y/ D 6x; C D f22 .x; y/ D 6y:

B D f12 .x; y/ D

8.

f1 D 4.x 3 y/;

f2 D 4.y 3 x/

A D f11 D 12x 2 ; B D f12 D 4; C D f22 D 12y 2 . For critical points: x 3 D y and y 3 D x. Thus x 9 D x, or x.x 8 1/ D 0, and x D 0, 1, or 1. The critical points are .0; 0/, .1; 1/ and . 1; 1/. At .0; 0/, B 2 AC D 16 0 > 0, so .0; 0/ is a saddle point. At .1; 1/ and . 1; 1/, B 2 AC D 16 144 < 0, A > 0, so f has local minima at these points. 5.

8 x C y y x 8 1 D 0 if 8y D x 2 f1 .x; y/ D y x2 x f2 .x; y/ D 1 D 0 if x D y 2 : y2 For critical points: 8y D x 2 D y 4 , so y D 0 or y D 2. f .x; y/ is not defined when y D 0, so the only critical point is . 4; 2/. At . 4; 2/ we have

f .x; y/ D cos x C cos y; f1 D sin x; f2 D sin y A D f11 D cos x; B D f12 D 0; C D f22 D cos y. The critical points are points .m; n/, where m and n are integers. Here B 2 AC D cos.m/ cos.n/ D . 1/mCnC1 which is negative if m C n is even, and positive if m C n is odd. If m C n is odd then f has a saddle point at .m; n/. If m C n is even and m is odd then f has a local (and absolute) minimum value, 2, at .m; n/. If m C n is even and m is even then f has a local (and absolute) maximum value, 2, at .m; n/.

3;

At .0; 0/: A D C D 0, B D 3. Thus AC < B 2 , and .0; 0/ is a saddle point of f . At .1; 1/: A D C D 6, B D 3, so AC > B 2 . Thus f has a local minimum value at .1; 1/. 4. f .x; y/ D x 4 Cy 4 4xy;

9.

f .x; y/ D x 2 ye

16 D x3 2x D 3 D y

1 ; 4

C D f22

1:

B D f12 D

1 D y2

1 ; 4

.x 2 Cy 2 /

f1 .x; y/ D 2xy.1

f2 .x; y/ D x 2 .1

A D f11 .x; y/ D 2y.1 B D f12 .x; y/ D 2x.1

x 2 /e

.x 2 Cy 2 /

2y 2 /e

.x 2 Cy 2 /

5x 2 C 2x 4 /e

x 2 /.1

C D f22 .x; y/ D 2x 2 y.2y 2

.x 2 Cy 2 /

2y 2 /e

3/e

.x 2 Cy 2 /

.x 2 Cy 2 /

:

For critical points:

f .x; y/ D

A D f11 D

f2 D x cos y D 0:

Since sin y and cos y cannot vanish at the same point, the only critical points correspond to x D 0 and sin y D 0. They are .0; n/, for all integers n. All are saddle points.

3xy

f1 .x; y/ D 3.x 2 y/; f2 .x; y/ D 3.y 2 x/: 2 For critical points: x D y and y 2 D x. Thus x 4 x D 0, that is, x.x 1/.x 2 C x C 1/ D 0. Thus x D 0 or x D 1. The critical points are .0; 0/ and .1; 1/. We have

1 < 0, and . 4; 2/ is a local 4

6.

(page 759)

f .x; y/ D x 2 C 2y 2 4x C 4y f1 .x; y/ D 2x 4 D 0 if x D 2 f2 .x; y/ D 4y C 4 D 0 if y D 1: Critical point is .2; 1/. Since f .x; y/ ! 1 as x 2 C y 2 ! 1, f has a local (and absolute) minimum value at that critical point.

(PAGE 759)

xy.1 2

x .1

x2/ D 0

2y 2 / D 0:

p The critical p points are .0; y/ for all y, .˙1; 1= 2/, and .˙1; 1= 2/. Evidently, f .0; y/ D 0. Also f .x; y/ > 0 if y > 0 and x ¤ 0, and f .x; y/ < 0 if y < 0 and x ¤ 0. Thus f has a local minimum at .0; y/ if y > 0, and a local maximum if y < 0. The origin is a saddle point. p p At .˙1; 1= 2/: A D C D 2 2e 3=2 , B D 0, and so AC > B 2 . Thus f has local maximum values at these two points.

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491

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SECTION 13.1 (PAGE 759)

ADAMS and ESSEX: CALCULUS 9

p p At .˙1; 1= 2/: A D C D 2 2e 3=2 , B D 0, and so AC > B 2 . Thus f has local minimum values at these two points. 2 2 Since f .x; py/ ! 0 as xp C y ! 1, the value maximum p f .˙1; 1= 2/ D e 3=2 = 2 is the absolute p value for f , and the value f .˙1; 1= 2/ D e 3=2 = 2 is the absolute minimum value.

xy 2 C x4 C y4 y.2 C y 4 3x 4 / .2 C x 4 C y 4 /y xy4x 3 D f1 D .2 C x 4 C y 4 /2 .2 C x 4 C y 4 /2 x.2 C x 4 3y 4 / f2 D . .2 C x 4 C y 4 /2 For critical points, y.2 C y 4 3x 4 / D 0 and x.2 C x 4 3y 4 / D 0. One critical point is .0; 0/. Since f .0; 0/ D 0 but f .x; y/ > 0 in the first quadrant and f .x; y/ < 0 in the second quadrant, .0; 0/ must be a saddle point of f . Any other critical points must satisfy 2 C y 4 3x 4 D 0 and 2 C x 4 3y 4 D 0, that is, y 4 D x 4 , or y D ˙x. Thus 2 2x 4 D 0 and x D ˙1. Therefore there are four other critical points: .1; 1/, . 1; 1/, .1; 1/ and . 1; 1/. f is positive at the first two of these, and negative at the other two. Since f .x; y/ ! 0 as x 2 C y 2 ! 1, f must have maximum values at .1; 1/ and . 1; 1/, and minimum values at .1; 1/ and . 1; 1/.

13.

10. f .x; y/ D

f .x; y/ D xe

11.

f1 .x; y/ D .1

3x 3 /e 2

3y 2 .3x 3

x 3 Cy 3

f1 .x; y/ D

4/e

x 3 Cy 3

1/e

3

3

x2 C y2 2 2xy 2 .x C y 2 /2x 2x 3 D 2 f1 .x; y/ D 2 2 2 .x C y / .x C y 2 /2 2 2x y f2 .x; y/ D : .x 2 C y 2 /2 Both partial derivatives are zero at all points of the coordinate axes. Also f .x; 0/ D 1 for x ¤ 0, and f .0; y/ D 0 for y ¤ 0. Evidently 0  f .x; y/  1 for all .x; y/ ¤ .0; 0/. Thus, f has absolute maximum value 1 at all points .x; 0/

492

x2



x 3 Cy 3

C D f22 .x; y/ D 3xy.3y 3 C 2/e x Cy For critical points: 3x 3 D 1 and 3xy 2 D 0. The only critical point is .3 1=3 ; 0/. At that point we have B D C D 0 so the second derivative test is inconclusive. 3 3 However, note that f .x; y/ D f .x; 0/e y , and e y has an inflection point at y D 0. Therefore f .x; y/ has neither a maximum nor a minimum value at .3 1=3 ; 0/, so has a saddle point there. f .x; y/ D

1

Evidently f has absolute maximum value 2 at

x 3 Cy 3

A D f11 .x; y/ D 3x 2 .3x 3

12.

1 x C y C x2 C y2 1 D  :    1 2 1 1 2 C yC C x 2 2 2

f .x; y/ D

Since

x 3 Cy 3

f2 .x; y/ D 3xy e

B D f12 .x; y/ D

14.

for x ¤ 0, and absolute minimum value 0 at all points .0; y/ for all y ¤ 0. xy f .x; y/ D 2 x C y2 .x 2 C y 2 /y 2x 2 y f1 .x; y/ D .x 2 C y 2 /2 y.y 2 x 2 / D 2 .x C y 2 /2 x.x 2 y 2 / f2 .x; y/ D 2 (by symmetry): .x C y 2 /2 Both partial derivatives are zero at all points of the lines y D ˙x for x ¤ 0. Also f .x; x/ D 21 , and f .x; x/ D 12 for x ¤ 0. Since x 2 ˙ 2xy C y 2 D .x ˙ y/2  0, we have jxyj  21 .x 2 C y 2 / for all .x; y/ ¤ .0; 0/, so jf .x; y/j  on its domain. Thus, f has absolute maximum value 12 at all points .x; x/ for x ¤ 0, and absolute minimum value 21 at all points .x; x/ for all x ¤ 0.

15.

1 ; 2

1 2



f2 .x; y/ D



1 ; 2

1 2x x C y C x 2 C y 2 /2 1 C 2y ; .1 x C y C x 2 C y 2 /2

.1

is the only critical point of f .

    1 1 1 1 f .x; y/ D 1 C C 1C x y x y .x C 1/.y C 1/.x C y/ D x2y2 .y C 1/.xy C x C 2y/ f1 .x; y/ D x3y2 .x C 1/.xy C y C 2x/ f2 .x; y/ D x2y3 2.y C 1/.xy C x C 3y/ A D f11 .x; y/ D x4y2 2.xy C x C y/ B D f12 .x; y/ D x3y3 2.x C 1/.xy C y C 3x/ : C D f22 .x; y/ D x2y4 For critical points:

and

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yD xD

1 1

or xy C x C 2y D 0; or xy C y C 2x D 0:

 1 . 2

1 2

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 13.1

If y D 1, then x D 1 or x 1 D 0. If x D 1, then y D 1 or y 1 D 0. If x ¤ 1 and y ¤ 1, then x y D 0, so x 2 C 3x D 0. Thus x D 0 or x D 3. However, the definition of f excludes x D 0. Thus, the only critical points are .1; 1/;

. 1; 1/;

. 1; 1/;

and

17.

f3 .x; y; z/ D x 2

x2

0 D f1 D yz 2x;

y2

2v C xw/v C .yu C xv

18.



h2 .1 C 2h/ > 0 for small 2

jhj. If h D k D 0, then D D m2 < 0 for m ¤ 0. Thus f has a saddle point at 1; 1; 12 . f .x; y; z/ D 4xyz x 4 y 4 z 4 D D f .1 C h; 1 C k; 1 C m/ f .1; 1; 1/

.1 C h/4

.1 C k/4

.1 C 4h C 6h2 C 4h3 C h4 /

.1 C 4k C 6k 2 C 4k 3 C k 4 /

.1 C 4m C 6m2 C 4m3 C m4 /

D 4.hk C hm C km/

2

2

1 2

6.h C k C m / C    ;

where    stands for terms of degree 3 and 4 in the variables h, k, and m. Completing some squares among the quadratic terms we obtain

2v C 2w/v

2w/w

DD

2.u2 C v 2 C w 2 / C 4.uv C vw C wu/

D 2Œ.u v w/2 4vw  < 0 if v D w D 0, u ¤ 0 > 0 if v D w ¤ 0, u v w D 0.

h i 2 .h k/2 C.k m/2 C.h m/2 Ch2 Ck 2 Cm2 C  

which is negative if jhj, jkj and jmj are small and not all 0. (This is because the terms of degree 3 and 4 are smaller in size than the quadratic terms for small values of the variables.) Hence f has a local maximum value at .1; 1; 1/.

Thus .2; 2; 2/ is a saddle point. At .2; 2; 2/, we have

19.

2.u2 C v 2 C w 2 C 2uv C 2uw

f 1; 1; 21

.1 C m/4 1 D 4.1 C h C k C m C hk C hm C km C hkm/

2z/w

At .2; 2; 2/, we have

  Du Du f D



D 4.1 C h/.1 C k/.1 C m/

 At .0; 0; 0/, Du Du f .0; 0; 0/ D 2u2 2v 2 2w 2 < 0 for u ¤ 0, so f has a local maximum value at .0; 0; 0/.

D

Cm

 . We have

If m D h and k D 0, then D D



C .2u C 2v

1 2

1 C 2h C h2 C .1 C 2h C h2 /m 2   1 3 m m2 1 2h h2 1 k 4 4 h2 .2m 1/ C 2h.k C 2m/ 2m2 : D 2

2w/w:

  Du Du f .2; 2; 2/ D . 2u C 2v C 2w/u C .2u

1 2

D 1 C h C k C hk C

Let u D ui C vj C wk, where u2 C v 2 C w 2 D 1. Then Du f .x; y; z/ D .yz 2x/u C .xz 2y/v C .xy   Du Du f .x; y; z/ D . 2u C zv C yw/u

z2

2z:

D D f 1 C h; 1 C k;

0 D f3 D xy 2z:

Thus xyz D 2x 2 D 2y 2 D 2z 2 , so x 2 D y 2 D z 2 . Hence x 3 D ˙2x 2 , and x D ˙2 or 0. Similarly for y and z. The only critical points are .0; 0; 0/, .2; 2; 2/, . 2; 2; 2/, . 2; 2; 2/, and .2; 2; 2/.

C .zu

y

The only critical point is 1; 1;

z 2 . For critical points we

0 D f2 D xz 2y;

x2 1/

. 3; 3/:

At .1; 1/, . 1; 1/, and . 1; 1/ we have AC D 0 and B ¤ 0. Therefore these three points are saddle points of f. At . 3; 3/, A D C D 4=243 and B D 2=243, so AC > B 2 . Therefore f has a local minimum value at . 3; 3/. 16. f .x; y; z/ D xyz have

f .x; y; z/ D xy C x 2 z f1 .x; y; z/ D y C 2x.z f2 .x; y; z/ D x 1

(PAGE 759)

2vw/

D 2Œ.u C v C w/2 4vw  < 0 if v D w D 0, u ¤ 0 > 0 if v D w ¤ 0, u C v C w D 0.

.x 2 Cy 4 /

f .x; y/ D xye f1 .x; y/ D y.1 f2 .x; y/ D x.1

2x 2 /e

.x 2 Cy 4 /

4y 4 /e

.x 2 Cy 4 /

For critical points y.1 The critical points are

Thus .2; 2; 2/ is a saddle point. By symmetry, so are the remaining two critical points.

.0; 0/;



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2x 2 / D 0 and x.1

 1 1 ˙p ; p ; 2 2

 1 ˙p ; 2

4y 4 / D 0.  1 p : 2

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SECTION 13.1 (PAGE 759)

ADAMS and ESSEX: CALCULUS 9

We have

The critical points must satisfy

f .0; 0/ D 0    1 1 1 Df f p ;p p ; 2   2  2 1 1 1 f p ;p Df p ; 2 2 2

x2y x D D 8; y xy 2

 1 1 D e 3=4 > 0 p 2 2 1 3=4 1 p e 0; y > 0/ xy 1 D 0 ) x2y D 1 f1 .x; y/ D 1 2 x y 1 f2 .x; y/ D 8 D 0 ) 8xy 2 D 1: xy 2

494

2V 2V C ; x y

0D

Any critical point must satisfy yz.1

V xy

where x > 0 and y > 0. Since S ! 1 as x ! 0C or y ! 0C or x 2 C y 2 ! 1, S must have a minimum value at a critical point in the first quadrant. For CP:

.x 2 Cy 2 Cz 2 /

2x 2 /e

Let the length, width, and height of the box be x, y, and z, respectively. Then V D xyz. The total surface area of the bottom and sides is

24.

Let the length, width, and height of the box be x, y, and z, respectively. Then V D xyz. If the top and side walls cost $k per unit area, then the total cost of materials for the box is C D 2kxy C kxy C 2kxz C 2kyz     V 2V 2V D k 3xy C 2.x C y/ C D k 3xy C ; xy x y where x > 0 and y > 0. Since C ! 1 as x ! 0C or y ! 0C or x 2 C y 2 ! 1, C must have a minimum value at a critical point in the first quadrant. For CP:  @C D k 3y @x  @C 0D D k 3x @y 0D

 2V x2  2V : y2

Thus 3x 2 y D 2V D 3xy 2 , so that x D y D .2V =3/1=3 and z D V =.2V =3/2=3 D .9V =4/1=3 .

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lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 13.1

Hence 9b C 6c D 180 D 6b C 8c, from which we obtain 3b D 2c D 30. The three numbers are b D 10, c D 15, and a D 30 10 15 D 5.

25. Let .x; y; z/ be the coordinates of the corner of the box that is in the first octant of space. Thus x; y; z  0, and y2 z2 x2 C 2 C 2 D 1: 2 a b c

27.

Differentiate the given equation e 2zx

The volume of the box is

V D .2x/.2y/.2z/ D 8cxy 2

2

s 2

y b2

x a2

1 2

for x  0, y  0, and .x =a / C .y =b /  1. For analysis it is easier to deal with V 2 than with V :  V 2 D 64c 2 x 2 y 2

x4y2 a2

x2y4 b2



2xy 4 b2 2

y b2  2y 2 : b2

.e /



.e

1 3

2

1 8abc D p cubic units. 3 3 3

c/b 2 c 3 D 30b 2 c 3

b3 c 3

3e

z2

z2

2e 3/.e

D2

z2

z2

3D0 C 1/ D 0:

2

2

We will use the second derivative test to classify the two critical points calculated in Exercise 25. To calculate the second partials AD

26. Given that a > 0, b > 0, c > 0, and a C b C c D 30, we want to maximize b

./

Thus e z D 3 or e z D 1. Since e z D 1 is not possip 2 ble, we have e z D 3, sopz D ˙p ln 3. ln 3/, and Thepcritical p points are . ln 3; . ln 3; ln 3/.

p so that p x 2 =a2 D y 2 =b 2 D 1=3, and x D a= 3, y D b= 3. The largest box has volume 1

2

z2 2

2x 2 y2 x2 2y 2 C 2 D1D 2 C 2 ; 2 a b a b

P D ab 2 c 3 D .30

ez

28.

r

./

For a critical point we have

Hence we must have

8abc V D 3

2

3e 2zyCy D 2

@z @z D 0 and D 0, and it @x @y follows from the equations above that z D x and z D y. Substituting these into the given equation, we get

:

Since V D 0 if x D 0 or y D 0 or .x 2 =a2 /C.y 2 =b 2 / D 1, the maximum value of V 2 , and hence of V , will occur at a critical point of V 2 where x > 0 and y > 0. For CP:  @V 2 4x 3 y 2 D 64c 2 2xy 2 0D @x a2  2x 2 D 128c 2 xy 2 1 a2  2 @V x2 0D D 128c 2 x 2 y 1 @y a2

x2

with respect to x and y, regarding z as a function of x and y:     @z @z 2 2 e 2zx x 2x C 2z 2x 3e 2zyCy 2y D0 @x @x     @z @z 2 2 e 2zx x 2x 3e 2zyCy 2y C 2z C 2y D 0 @y @y

2

2

(PAGE 759)

b2 c 4:

Since P D 0 if b D 0 or c D 0 or b C c D 30 (i.e., a D 0), the maximum value of P will occur at a critical point .b; c/ satisfying b > 0, c > 0, and b C c < 30. For CP:

@2 z ; @x 2

BD

@2 z ; @x@y

C D

@2 z ; @y 2

we differentiate the expressions ./, and ./ obtained in Exercise 25. Differentiating ./ with respect to x, we obtain " !2 @z 2zx x 2 e 2x C 2z 2x @x # @2 z @z C 2x 2 2 C4 @x @x " # !2 @z @2 z 2zyCy 2 3e 2y C 2y 2 D 0: @x @x At a critical point, 2

z D ln 3, so

@P 0D D 60bc 3 3b 2 c 3 2bc 4 D bc 3 .60 3b 2c/ @b @P 0D D 90b 2 c 2 3b 3 c 2 4b 2 c 3 D b 2 c 2 .90 3b 4c/: @c

@z D 0, z D x, z D @x

y, and

   3 @2 z @2 z 2y 2 D 0; 3 2x 2 2 @x 3 @x @2 z 6 AD D : @x 2 6x 2y 

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SECTION 13.1 (PAGE 759)

ADAMS and ESSEX: CALCULUS 9

Since f1 .0; 0/ D f2 .0; 0/ D 0, therefore .0; 0/ is a critical point of f . Let g.x/ D f .x; kx/ D k 2 x 2 4kx 3 C 3x 4 . Then

Differentiating ./ with respect to y gives

e

2zx x 2

"

3e 2zyCy

@z 2x @y "

2

!2

2y

@2 z C 2x 2 @y

#

@z C 2z C 2y @y

!2

2

C4

g 0 .x/ D 2k 2 x

#

g 00 .x/ D 2k 2

@ z @z C 2y 2 C 2 D 0; @y @y

    @2 z @2 z 3 2y 2 C 2 D 0; 3 2x 2 @y 3 @y @2 z 2 C D 2 D : @y 6x 2y

f .x; 2x 2 / D x 2 . x 2 / D

Finally, differentiating ./ with respect to y gives e

"

@z C 2z 2x @x

2x

!

@z 2x @y

!

# @z @2 z C2 C 2x @x@y @y ! ! " @z @z 2zyCy 2 C 2z C 2y 2y 3e 2y @y @x # @2 z @z C2 C 2y D 0; @x @x@y

2y/

.0;0/

Thus AC D B 2 , and the second derivative test is indeterminate at the origin.

30.

@2 z D 0; @x@y

@2 z D 0: @x@y p p At the critical point . ln 3; ln 3/ we have BD

6 ; 8 ln 3

B D 0;

C D

6 ; 8 ln 3

B D 0;

C D

2 ; 8 ln 3

so B 2 AC < 0, and f has a local maximum at that critical point. 29.

f .x; y/ D .y

x 2 /.y

f2 .x; y/ D 2y

4x 2 :

f1 .x; y/ D

496

3x 2 / D y 2

8xy C 12x 3 D 4x.3x 2

4x 2 y C 3x 4 2y/

B2 A



v2

ˇ ˇ ˇA B ˇ ˇ D AC B 2 > 0, both terms above have If ˇˇ B Cˇ the same sign, positive if A > 0 and negative if A < 0, ensuring that Q is positive definite or negative definite respectively, since the two terms cannot both vanish if .u; v/ ¤ .0; 0/. If AC B 2 < 0, Q.u; v/ is a difference of squares, and must be indefinite.

2 ; 8 ln 3

so B 2 AC < 0, and f has a local minimum at that critical point. p p ln 3; ln 3/ we have At the critical point . AD

We have Q.u; v/ D Au2 C 2Buv C C v 2    B2 2B uv C 2 v 2 C C D A u2 C A A   Bv 2 AC B 2 2 C v : DA uC A A

so that

AD

x4;

which has a local maximum value at the origin. Therefore f does not have an (unrestricted) local minimum value at .0; 0/. ˇ ˇ Note that A D f11 .0; 0/ D . 8y C 36x 2 /ˇˇ D0 .0;0/ ˇ ˇ B D f12 .0; 0/ D 8x ˇˇ D 0:

and, evaluating at a critical point, .6x

24kx C 36x 2 :

Since g 0 .0/ D 0 and g 00 .0/ D 2k 2 > 0 for k ¤ 0, g has a local minimum value at x D 0. Thus f .x; kx/ has a local minimum at x D 0 if k ¤ 0. Since f .x; 0/ D 3x 4 and f .0; y/ D y 2 both have local minimum values at .0; 0/, f has a local minimum at .0; 0/ when restricted to any straight line through the origin. However, on the curve y D 2x 2 we have

and evaluation at a critical point gives

2zx x 2

12kx 2 C 12x 3

31.

Let Q.u; v; w/ D Au2 C Bv 2 C C w 2 C 2Duv C 2Euw C 2F vw and let K1 D A; ˇ ˇA ˇ K3 D ˇˇ D ˇE

ˇ ˇ ˇA Dˇ ˇ D AB D 2 K2 D ˇˇ D Bˇ ˇ D E ˇˇ B F ˇˇ D ABC C 2DEF BE 2 F Cˇ

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CD 2

AF 2 :

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 13.2

Suppose that K1 ¤ 0, K2 ¤ 0, and K3 ¤ 0. We have Q.u; v; w/ "

Dv C Ew D A u C 2u C A 2

C

D2

AB A

v2 C

E2

AC

  Dv C Ew 2 DA uC A



A

Dv C Ew A w2 C

2 #

2.AF

DE/ A

vw

!   AF DE 2 2 DE/ vw C w A D2 AB D 2   AC E 2 .AF DE/2 w2 C A A.AB D 2 /    2 Dv C Ew 2 AB D 2 AF DE DA uC C vC w A A AB D 2 2 2 2 A.ABC BE AF CD C 2DEF / 2 w C A.AB D 2 /  2   2. Dv C Ew 2 K2 AF DE D K1 u C C w vC A K1 AB D 2 K3 2 C w : K2 C

AB

D2

v2 C

2.AF AB

If K1 > 0, K2 > 0, and K3 > 0, then all three squares the last expression above have positive coefficients, and so Q is positive definite. If K1 < 0, K2 > 0, and K3 < 0, then all three squares the last expression above have negative coefficients, and so Q is negative definite. In all other cases where none of the Ki D 0, the coefficients of the squares are not all of the same sign so choices of .u; v; w/ can be made which make the expression either positive or negative, and Q is indefinite.

D D f12 .a; b; c/; E D f23 .a; b; c/; F D f23 .a; b; c/:

Then f has a local minimum value at .a; b; c/ if K1 > 0, K2 > 0, and K3 > 0, a local maximum value at .a; b; c/ if K1 < 0, K2 > 0, and K3 < 0, and a saddle point at .a; b; c/ if K1 ; K2 ; K3 are all nonzero but satisfy neither of the above conditions.

Section 13.2 Extreme Values of Functions Defined on Restricted Domains (page 765) 1.

f .x; y/ D x x 2 C y 2 on R D f.x; y/ W 0  x  2; 0  y  1g. For critical points: 0 D f1 .x; y/ D 1

2x;

0 D f2 .x; y/ D 2y:

The only CP is .1=2; 0/, which lies on the boundary of R. The boundary consists of four segments; we investigate each. On x D 0 we have f .x; y/ D f .0; y/ D y 2 for 0  y  1, which has minimum value 0 and maximum value 1. On y D 0 we have f .x; y/ D f .x; 0/ D x x 2 D g.x/ for 0  x  2. Since g 0 .x/ D 1 2x D 0 at x D 1=2, g.1=2/ D 1=4, g.0/ D 0, and g.2/ D 2, the maximum and minimum values of f on the boundary segment y D 0 are 1/4 and 2 respectively. On x D 2 we have f .x; y/ D f .2; y/ D 2 C y 2 for 0  y  1, which has minimum value 2 and maximum value 1. On y D 1, f .x; y/ D f .x; 1/ D x x 2 C 1 D g.x/ C 1 for 0  x  2. Thus the maximum and minimum values of f on the boundary segment y D 1 are 5/4 and 1 respectively. Overall, f has maximum value 5=4 and minimum value 2 on the rectangle R. f .x; y/ D xy 2x on R D f.x; y/ W 1  x  1; 0  y  1g. For critical points: 0 D f1 .x; y/ D y

2;

0 D f2 .x; y/ D x:

The only CP is .0; 2/, which lies outside R. Therefore the maximum and minimum values of f on R lie on one of the four boundary segments of R. On x D 1 we have f . 1; y/ D 2 y for 0  y  1, which has maximum value 2 and minimum value 1. On x D 1 we have f .1; y/ D y 2 for 0  y  1, which has maximum value 1 and minimum value 2. On y D 0 we have f .x; 0/ D 2x for 1  x  1, which has maximum value 2 and minimum value 2. On y D 1 we have f .x; 1/ D x for 1  x  1, which has maximum value 1 and minimum value 1. Thus the maximum and minimum values of f on the rectangle R are 2 and 2 respectively.

If f has continuous partial derivatives of order two and .a; b; c/ is a critical point of f .x; y; z/, let A D f11 .a; b; c/; B D f22 .a; b; c/; C D f33 .a; b; c/;

(PAGE 765)

3.

f .x; y/ D xy y 2 on D D f.x; y/ W x 2 C y 2  1g. For critical points: 0 D f1 .x; y/ D y;

0 D f2 .x; y/ D x

2y:

The only CP is .0; 0/, which lies inside D. We have f .0; 0/ D 0. The boundary of D is the circle x D cos t , y D sin t ,   t  . On this circle we have g.t / D f .cos t; sin t / D cos t sin t i 1h sin 2t C cos 2t 1 ; D 2 g.0/ D g.2/ D 0 g 0 .t / D cos 2t sin 2t:

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sin2 t .   t  /:

497

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SECTION 13.2 (PAGE 765)

ADAMS and ESSEX: CALCULUS 9

The critical points of g satisfy cos 2t D sin 2t , that is,  5  5 tan 2t D 1, so 2t D ˙ or ˙ , and t D ˙ or ˙ . 4 4 8 8 We have   1 1 1 1 1 C p D p >0 D p g 8 2 2 2 2 2 2 2   1 1 1 1 g C p D D p 8 2 2 2 2 2 2   5 1 1 1 1 1 g D p p D p 8 2 2 2 2 2 2 2   1 1 5 1 1 : D p g p D 8 2 2 2 2 2 2

6.

f .x; y/ D xy.1 x y/ on the triangle T shown in the figure. Evidently f .x; y/ D 0 on all three boundary segements of T , and f .x; y/ > 0 inside T . Thus the minimum value of f on T is 0, and the maximum value must occur at an interior critical point. For critical points: 0 D f1 .x; y/ D y.1 2x y/;

The only critical points are .0; 0/, .1; 0/ and .0; 1/, which are on the boundary of T , and .1=3; 1=3/, which is inside T . The maximum value of f over T is f .1=3; 1=3/ D 1=27. y

Thus the maximum and minimum values of f on the disk 1 1 1 1 D are p and p respectively. 2 2 2 2

T 1 x

Fig. 13.2-6

7.

Since 1  f .x; y/ D sin x cos y  1 everywhere, and since f .=2; 0/ D 1, f .3=2; 0/ D 1, and both .=2; 0/ and .3=2; 0/ belong to the triangle bounded by x D 0, y D 0 and x C y D 2, therefore the maximum and minimum values of f over that triangle must be 1 and 1 respectively.

8.

f .x; y/ D sin x sin y sin.x C y/ on the triangle T shown in the figure. Evidently f .x; y/ D 0 on the boundary of T , and f .x; y/ > 0 at all points inside T . Thus the minimum value of f on T is zero, and the maximum value must occur at an interior critical point. For critical points inside T we must have

0 For critical points of g: 0 D gp .t / D sin t C p 2 cos t . Thus tan t D 2, and x p D ˙1= p5, y D ˙2= 5. The has value critical points p are . 1= p 5; 2= 5/, where f p p 5, and .1= 5; 2= 5/, where f has value 5. Thus the p maximum p and minimum values of f .x; y/ on the disk are 5 and 5 respectively.

5. f .x; y/ D xy x 3 y 2 on the square S: 0  x  1, 0  y  1. f1 D y 3x 2 y 2 D y.1 3x 2 y/; f2 D x 2x 3 y D x.1 2x 2 y/. .0; 0/ is a critical point. Any other critical points must satisfy 3x 2 y D 1 and 2x 2 y D 1, that is, x 2 y D 0. Therefore .0; 0/ is the only critical point, and it is on the boundary of S. We need therefore only consider the values of f on the boundary of S. On the sides x D 0 and y D 0 of S, f .x; y/ D 0. On the side x D 1 we have f .1; y/ D y y 2 D g.y/, .0  y  1/. g has maximum value 1=4 at its critical point y D 1=2. On the side y D 1 we have f .x; 1/ D x x 3 D h.x/, .0  x  1/.p h has critical point given by 1 3x 2 D 0; only  xD  1= 3 is on the side of S. 1 1 2 h p D p > : 4 3 3 3 On the square S, f .x; y/ has minimum value 0 (on the sides x D 0 and y D 0 and at the corner .1; 1/ of p the p square), and maximum value 2=.3 3/ at the point .1= 3; 1/. There is a smaller local maximum value at .1; 1=2/.

498

1

xCyD1

4. f .x; y/ D x C 2y on the closed disk x 2 C y 2  1. Since f1 D 1 and f2 D 2, f has no critical points, and the maximum and minimum values of f , which must exist because f is continuous on a closed, bounded set in the plane, must occur at boundary points of the domain, that is, points of the circle x 2 C y 2 D 1. This circle can be parametrized x D cos t , y D sin t , so that f .x; y/ D f .cos t; sin t / D cos t C 2 sin t D g.t /; say.

0 D f2 .x; y/ D x.1 x 2y/:

0 D f1 .x; y/ D cos x sin y sin.x C y/ C sin x sin y cos.x C y/ 0 D f2 .x; y/ D sin x cos y sin.x C y/ C sin x sin y cos.x C y/: Therefore cos x sin y D cos y sin x, which implies x D y for points inside T , and cos x sin x sin 2x C sin2 x cos 2x D 0

2 sin2 x cos2 x C 2 sin2 x cos2 x

4 cos2 x D 1:

sin2 x D 0

Thus cos x D ˙1=2, and x D ˙=3. The interior critical p point is .=3; =3/, where f has the value 3 3=8. This is the maximum value of f on T .

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 13.2

y

On the boundary y D 0 we have



f .x; 0/ D

zCyD T

x

Fig. 13.2-8 2

9. T D .x C y/e x y on D D f.x; y/ W x 2 C y 2  1g. For critical points:  @T D 1 @x  @T D 1 0D @y

 2x.x C y/ e  2y.x C y/ e

0D

x2 y2 x2 y2

:

The critical points are given by 2x.x C y/ D 1 D 2y.x C y/, which forces x D y 1 and 4x 2 D 1, so x D y D ˙ . 2     1 1 1 1 ; ; and , both The two critical points are 2 2 2 2 1=2 of which lie inside D. T takes the values ˙e at these points. On the boundary of D, x D cos t , y D sin t , 0  t  2, so that T D .cos t C sin t /e

1

D g.t /;

We have g.0/ D g.2/ D e

1

.0  t  2/:

. For critical points of g:

0 D g 0 .t / D .cos t

sin t /e

1

;

so tan t D p1 and t D =4 or t D 5=4. Observe that p 2e 1 . g.=4/ D 2e p1 , and g.5=4/ D Since e 1=2 > 2e 1 (because e > 2), the maximum and minimum values of T on the disk are ˙e 1=2 , the values at the interior critical points. x y on the half-plane y  0. 10. f .x; y/ D 1 C x2 C y2 For critical points: 0 D f1 .x; y/ D 0 D f2 .x; y/ D

1

x 2 C y 2 C 2xy .1 C x 2 C y 2 /2 1 x 2 C y 2 2xy : .1 C x 2 C y 2 /2

Any critical points must satisfy 1 x 2 C y 2 C 2xy D 0 2 and 1 x 2 C y 2 2xy D 0, and hence xp D y2 and 2xy D 1. Therefore y D x D ˙1= p2. The p only critical point in the region p y  0 is . 1= 2; 1= 2/, where f has the value 1= 2.

x D g.x/; 1 C x2

. 1 < x < 1/:

Evidently, g.x/ ! 0 as x ! ˙1. 1 x2 Since g 0 .x/ D , the critical points of g are .1 C x 2 /2 1 x D ˙1. We have g.˙1/ D ˙ . 2 The maximum and minimum values p of f on the upper half-plane y  0 are 1=2 and 1= 2 respectively.



2

(PAGE 765)

11.

Let f .x; y; z/ D xy 2 C yz 2 on the ball B: x 2 C y 2 C z 2  1. First look for interior critical points: 0 D f1 D y 2 ;

0 D f2 D 2xy C z 2 ;

0 D f3 D 2yz:

All points on the x-axis are CPs, and f D 0 at all such points. Now consider the boundary sphere z 2 D 1 it

x2

y 2 . On

f .x; y; z/ D xy 2 Cy.1 x 2 y 2 / D xy 2 Cy x 2 y y 3 D g.x; y/; where g is defined for x 2 C y 2  1. Look for interior CPs of g: 0 D g1 D y 2 2xy D y.y 2x/ 0 D g2 D 2xy C 1

x2

3y 2 :

Case I: y D 0. Then g D 0 and f D 0. Case II: y D 2x. Then 4x 2 C 1 x 2 12x 2 D 0, so 9x 2 D 1 and x D ˙1=3. This case produces critical points   1 2 2 4 ; ;˙ ; where f D ; and 3 3 3 9   2 4 1 2 ; ;˙ : ; where f D 3 3 3 9 Now we must consider the boundary x 2 C y 2 D 1 of the domain of g. Here g.x; y/ D xy 2 D x.1

x2/ D x

x 3 D h.x/

for 1  x  1. At the endpoints x D ˙1, h D 0, so g D 0 and f D 0. For CPs of h: 0 D h0 .x/ D 1 3x 2 ; p p so x D ˙1= 3 and y D ˙ 2=3. The value of h at such p p points is ˙2=.3 3/. However 2=.3 3/ < 4=9, so the maximum value of f is 4/9, and the minimum value is 4=9. 12. Let f .x; y; z/ D xz C yz on the ball x 2 C y 2 C z 2  1. First look for interior critical points: 0 D f1 D z;

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0 D f2 D z;

0 D f3 D x C y:

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SECTION 13.2 (PAGE 765)

ADAMS and ESSEX: CALCULUS 9

All points on the line z D 0, x C y D 0 are CPs, and f D 0 at all such points.

14.

f .x; y/ D xy 2 e xy on Q D f.x; y/ W x  0; y  0g. As in Exercise 13, f .x; 0/ D f .0; y/ D 0 and 2 limx!1 f .x; kx/ D k 2 x 3 ex D0. y 1 ; y D ! 1 as y ! 1, Also, f .0; y/ D 0 while f y e so that f has no limit as x 2 C y 2 ! 1 in Q, and f has no maximum value on Q.

15.

If brewery A produces x litres per month and brewery B produces y litres per month, then the monthly profits of the two breweries are given by

Now consider the boundary sphere x 2 C y 2 C z 2 D 1. On it p f .x; y; z/ D .x Cy/z D ˙.x Cy/ 1

x2

y 2 D g.x; y/;

where g has domain x 2 C y 2  1. On the boundary of its domain, g is identically 0, although g takes both positive and negative values at some points inside its domain. Therefore, we need consider only critical points of g in x 2 C y 2 < 1. For such CPs: 0 D g1 D D 0 D g2 D

p 1 1

1

x2 x2 p

1

2

x p

.x C y/. 2x/ y2 C p 2 1 x2 y2 2 2 y x xy x2 y2 y 2 xy y 2 x2

1

y2

:

Since we have considered all points where f can have extreme values, we p conclude that the maximum value of f on the ball is 1= 2 (which occurs at the p boundary points ˙. 12 ; 12 ; p1 /) and minimum value 1= 2 (which occurs 2

at the boundary points ˙. 12 ; 12 ;

r/e

r

D0

)

r D 1;

f .x; y/ is everywhere on Q less than g.1/ D 1=e. Thus f does have a maximum value on Q.

500

@P D2 @x

4x 106

4y 2 C x 2 : 2  106

x D 5  105 :

)

B chooses y to satisfy 0D

@Q D2 @y

8y 2  106

y D 5  105 :

)

The total profit of the two breweries under this strategy is 3  25  1010 C 106 106 D $625; 000:

P C Q D 106

5  25  1010 2  106

STRATEGY II. The two breweries cooperate to maximize the total profit

p1 /). 2

13. f .x; y/ D xye xy on Q D f.x; y/ W x  0; y  0g. 2 Since f .x; kx/ D kx 2 e kx ! 0 as x ! 1 if k > 0, and f .x; 0/ D f .0; y/ D 0, we have f .x; y/ ! 0 as .x; y/ recedes to infinity along any straight line from the origin lying in the  first quadrant Q.  1 However, f x; D 1 and f .x; 0/ D 0 for all x > 0, x   1 and .x; 0/ become arbitrareven though the points x; x ily close together as x increases. Thus f does not have a limit as x 2 C y 2 ! 1. Observe that f .x; y/ D re r D g.r/ on the hyperbola xy D r > 0. Since g.r/ ! 0 as r approaches 0 or 1, and g 0 .r/ D .1

Q D 2y

STRATEGY I. Each brewery selects its production level to maximize its own profit, and assumes its competitor does the same. Then A chooses x to satisfy 0D

Therefore 2x 2 C y 2 C xy D 1 D x 2 C 2y 2 C xy, from which x 2 D y 2 . Case I: x D y. Then g D 0, so f D 0. Case II: x D y. Then 2x 2 Cx 2 Cx 2 D 1, so x 2 D 1=4 and x D ˙1=2. g (which is really two functions depending on our choice of the “C” or “ ” sign) has four CPs, two corresponding to x D y D 1=2 and two to x p D y D 1=2. The values of g at these four points are ˙1= 2.

2x 2 C y 2 ; 106

P D 2x

T D P C Q D 2x C 2y

5x 2 C 6y 2 2  106

by choosing x and y to satisfy @T D2 @x @T 0D D2 @y 0D

10x ; 2  106 12y : 2  106

1 Thus x D 4  105 and y D  106 . 3 In this case the total monthly profit is 2 P C Q D 8  10 C  106 3  $733; 333: 5

2  1012 3 2  106

80  1010 C

Observe that the total profit is larger if the two breweries cooperate and fix prices to maximize it.

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 13.2

16. Let the dimensions be as shown in the figure. Then 2x C y D 100, the length of the fence. For maximum area A of the enclosure we will have x > 0 and 0 <  < =2. Since h D x cos  , the area A is

17.

(PAGE 765)

To maximize Q.x; y/ D 2x C 3y subject to x  0;

y  0;

y  5;

x C 2y  12;

4x C y  12:

The constraint region is shown in the figure. y

1 A D xy cos  C 2  .x sin  /.x cos  / 2 D x.100 2x/ cos  C x 2 sin  cos  1 D .100x 2x 2 / cos  C x 2 sin 2: 2

4xCyD12

We look for a critical point of A satisfying x > 0 and 0 <  < =2.

yD5

wall xC2yD12



h

h

x

x





Observe that any point satisfying y  5 and 4x C y  12 automatically satisfies x C2y  12. Since y D 5 and 7 ; 5 , the maximum value of 4x C y D 12 intersect at 4 Q.x; y/ subject to the given constraints is   7 7 37 Q ; 5 D C 15 D : 4 2 2

Fig. 13.2-16

@A D .100 4x/ cos  C x sin 2 @x ) cos .100 4x C 2x sin  / D 0 ) 4x

2x sin  D 100 ) x D

2

50 sin 

@A D .100x 2x 2 / sin  C x 2 cos 2 0D @ ) x.1 2 sin2  / C 2x sin  100 sin  D 0: Substituting the first equation into the second we obtain  50  1 2 sin2  C 2 sin  100 sin  D 0 2 sin  2 50.1 2 sin  C 2 sin  / D 100.2 sin  sin2  / 50 D 100 sin : Thus sin  D 1=2, and  D =6. 50 Therefore x D D 2 .1=2/ 100 y D 100 2x D . 3

x

Fig. 13.2-17

y

0D



7 4 ;5

18. Minimize F .x; y; z/ D 2x C 3y C 4z subject to x  0; x C y  2;

y  0; y C z  2;

z  0; x C z  2:

Here the constraint region has vertices .1; 1; 1/, .2; 2; 0/, .2; 0; 2/, and .0; 2; 2/. Since F .1; 1; 1/ D 9, F .2; 2; 0/ D 10, F .2; 0; 2/ D 12, and F .0; 2; 2/ D 14, the minimum value of F subject to the constraints is 9. z

xCyD2

xD0

yD0

100 , and 3

.0;2;2/ .2;0;2/ .1;1;1/

The maximum area for the enclosure is p  p    100 2 1 3 2500 100 2 3 C D p AD 3 2 3 2 2 3

xCzD2

yCzD2 .2;2;0/

y

x

square units. All three segments of the fence will be the same length, and the bend angles will be 120ı .

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zD0

Fig. 13.2-18

501

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SECTION 13.2 (PAGE 765)

ADAMS and ESSEX: CALCULUS 9

Section 13.3 Lagrange Multipliers (page 773)

19. Suppose that x kg of deluxe fabric and y kg of standard fabric are produced. Then the total revenue is R D 3x C 2y: The constraints imposed by raw material availability are

1.

10 20 xC y  2; 000; , 2x C y  20; 000 100 100 50 40 xC y  6; 000; , 5x C 4y  60; 000 100 100 30 50 xC y  6; 000; , 3x C 5y  60; 000: 100 100

@L D 3x 2 y 5 C  @x @L D 5x 3 y 4 C  0D @y @L 0D D x C y 8: @

0D

The lines 2x C y D 20; 000 and 5x C4y D 60; 000 20; 000 20; 000 ; intersect at the point , which satisfies 3 3 3x C 5y  60; 000, so lies in the constraint region. We have   20; 000 20; 000 ;  33; 333: f 3 3 The lines 2xCy D 20; 000 and 3x C5y D 60; 000 intersect 40; 000 60; 000 at the point ; , which does not satisfy 7 7 5x C 4y  60; 000 and so does not lie in the constraint region. The lines 5x C 4y D 60; 000 and 3x C5y D 60; 000 60; 000 120; 000 ; , which satisfies intersect at the point 13 13 2x C y  20; 000 and so lies in the constraint region. We have   60; 000 120; 000 ;  32; 307: f 13 13 To produce the maximum revenue, the manufacturer should produce 20; 000=3  6; 667 kg of each grade of fabric.

First we observe that f .x; y/ D x 3 y 5 must have a maximum value on the line x C y D 8 because if x ! 1 then y ! 1 and if x ! 1 then y ! 1. In either case f .x; y/ ! 1. Let L D x 3 y 5 C .x C y 8/. For CPs of L:

The first two equations give 3x 2 y 5 D 5x 3 y 4 , so that either x D 0 or y D 0 or 3y D 5x. If x D 0 or y D 0 then f .x; y/ D 0. If 3y D 5x, then x C 35 x D 8, so 8x D 24 and x D 3. Then y D 5, and f .x; y/ D 33 55 D 84; 375. This is the maximum value of f on the line.

2.

a) Let D be the distance from .3; 0/ to the point .x; y/ on the curve y D x 2 . Then D 2 D .x

The legal constraints imposed require that x y z C C  10; 6 8 12

that is 4x C 3y C 2z  240;

and also z  x C y:

dD 2 D 2.x 3/ C 4x 3 : Thus dx 2x 3 C x 3 D 0. Clearly x D 1 is a root of this cubic equation. Since 2x 3 C x 3 D 2x 2 C 2x C 3; x 1 and 2x 2 C 2x C 3 has negative discriminant, x D 1 is the only critical point. Thus the p minimum distance p from .3; 0/ to y D x 2 is D D . 2/2 C 14 D 5 units. b) We want to minimize D 2 D .x 3/2 C y 2 2 subject to the constraint y D x . Let L D .x 3/2 C y 2 C .x 2 y/. For critical points of L we want

Evidently we must also have x  0, y  0, and z  0. The planes 4x C 3y C 2z D 240 and z D x C y intersect where 6x C 5y D 240. Thus the constraint region has vertices .0; 0; 0/, .40; 0; 40/, .0; 48; 48/, and .0; 0; 120/, which yield revenues of $0, $2,240,000, $1,728,000, and $1,920,000 respectively. For maximum profit, the developer should build 40 houses, no duplex units, and 40 apartments.

502

3/2 C x 4 :

For a minimum, 0 D

20. If the developer builds x houses, y duplex units, and z apartments, his profit will be P D 40; 000x C 20; 000y C 16; 000z:

3/2 C y 2 D .x

@L D 2.x 3/ C 2x @x ) .1 C /x 3 D 0 @L 0D D 2y  @y @L D x 2 y: 0D @ 0D

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.A/ .B/ .C /

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 13.3

Eliminating  from (A) and (B), we get x C 2xy 3 D 0. Substituting (C) then leads to 2x 3 C x 3 D 0, or .x 1/.2x 2 C 2x C 3/ D 0. The only real solution is x D 1, so the point on y D x 2 closest to .3; 0/ is .1; 1/. 2 Thus p the minimum distance p from .3; 0/ to y D x is D D .1 3/2 C 12 D 5 units.

The first three equations yield y D z D , x D =2. Substituting these into the fourth equation we get  D 23 , so that the critical point is once  again 13 ; 23 ; 23 , whose distance from the origin is 1 unit. 4.

Let f .x; y; z/ D x C y function

3. Let .X; Y; Z/ be the point on the plane x C 2y C 2z D 3 closest to .0; 0; 0/.

@L @x @L 0D @y @L 0D @z @L 0D @

0D

for some scalar t . Thus X D t , Y D 2t , Z D 2t , and, since .X; Y; Z/ lies on the plane, 3 D X C 2Y C 2Z D t C 4t C 4t D 9t: Thus t D 31 , and we have X D 13 and Y D Z D 32 . The minimum p distance from the origin to the plane is therefore 13 1 C 4 C 4 D 1 unit.

2 2.y C z/ C y 2 C z 2 :

The critical points of this function are given by  4 3  4 3

 2.y C z/ C 2y D  2.y C z/ C 2z D

Therefore Y D Z D 23 and X D is 1 unit as in part (a).

1 3,

12 C 10y C 8z

c) The point .X; Y; Z/ must be a critical point of the Lagrange function L D x 2 C y 2 C z 2 C .x C 2y C 2z

@L @x @L 0D @y @L 0D @z @L 0D @

3/:

D

1 C 2z;

D x2 C y2 C z2

1:

The distance D from .2; 1; 2/ to .x; y; z/ is given by D 2 D .x

2/2 C .y

1/2 C .z C 2/2 :

We can extremize D by extremizing D 2 . If .x; y; z/ lies on the sphere x 2 Cy 2 Cz 2 D 1, we should look for critical points of the Lagrange function L D .x

2/2 C .y

@L @x @L 0D @y @L 0D @z @L 0D @ 0D

D 2x C  D 2y C 2 D 2z C 2 D x C 2y C 2z

D 1 C 2y;

1/2 C .z C 2/2 C .x 2 C y 2 C z 2

1/:

Thus

To find these critical points we have 0D

5.

12 C 8y C 10z:

and the distance

D 1 C 2x;

Therefore 2x D 2y D 2z. Either  D 0 or x D y D z.  D 0 is not possible. (It implies 0 D 1 from the first equation.) From x D y D z we obtain 1 1 D x 2 C y 2 C z 2 D 3x 2 , so x D ˙ p . L has critical 3     1 1 1 1 1 1 points at p ; p ; p and p ; p ;p . 3 p 3 3 3 3 3 value of At the first f D 3, which is the maximum p 3, which is the f on the sphere; at the second f D minimum value.

b) .X; Y; Z/ must minimize the square of the distance from the origin to .x; y; z/ on the plane. Thus it is a critical point of S D x 2 C y 2 C z 2 . Since x C 2y C 2z D 3, we have x D 3 2.y C z/, and

@S D @y @S 0D D @z

1/:

Solutions to the constrained problem will be found among the critical points of L. To find these we have

Xi C Y j C Zk D t .i C 2j C 2k/;

0D

z, and define the Lagrange

z C .x 2 C y 2 C z 2

LDxCy

a) The vector r.x C 2y C 2z/ D i C 2j C 2k is perpendicular to the plane, so must be parallel to the vector Xi C Y j C Zk from the origin to .X; Y; Z/. Thus

 S D S.y; z/ D 3

(PAGE 773)

3:

D 2.x

2/ C 2x

,

D 2.y

1/ C 2y

,

D 2.z C 2/ C 2z

,

D x2 C y2 C z2

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2 1C 1 yD 1C 2 zD 1C xD

1:

503

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SECTION 13.3 (PAGE 773)

ADAMS and ESSEX: CALCULUS 9

Substituting the solutions of the first three equations into the fourth, we obtain

8.

@L D 2x C 6x C 2y @x @L 0D D 2y C 6y C 2x: @y

@L @x @L 0D @y @L 0D @z @L 0D @

,

xyz 2 D 2x 2

D 2y C xz 2

,

xyz 2 D 2y 2

D xyz 2

,

xyz 2 D z 2

For critical points of L: @L @a @L 0D @b @L 0D @c @L 0D @

9.

4bc 2 2abc  , D 2 3 a3 3 a 2abc 4ac 8 4 , D D 2 3 b3 3 b 2abc 4ab 2  , D D 2 3 c3 3 c 4 1 1 D 2 C 2 C 2 1: a b c D

@L @x @L 0D @y @L 0D @z @L 0D @

D yz C 2x

.A/

D xz C 2y

.B/

D xy C 2z

.C /

D x2 C y2 C z2

12:

3z C .x 2 C 4y 2 C 9z 2

10. Let L D x C 2y of L:

@L @x @L 0D @y @L 0D @z @L 0D @

0D

.D/

108/. For CPs

D 1 C 2x

.A/

D 2 C 8y

.B/

D

.C /

3 C 18z

D x 2 C 4y 2 C 9z 2

108:

From (A), (B), and (C),

p p p so a D ˙ 3, b D ˙2 3, and c D ˙ 3.

504

12/. For CPs of L:

Multiplying equations (A), (B), and (C) by x, y, and z, respectively, and subtracting in pairs, we conclude that x 2 D y 2 D z 2 , so that either  D 0 or x 2 D y 2 D z 2 . If  D 0, then (A) implies that yz D 0, so xyz D 0. If x 2 D y 2 D z 2 , then (D) gives 3x 2 D 12, so x 2 D 4. We obtain eight points .x; y; z/ where each coordinate is either 2 or 2. At four of these points xyz =8, which is the maximum value of xyz on the sphere. At the other four xyz D 8, which is the minimum value.

abc ¤ 0 implies  ¤ 0, and so we must have 4 1 1 1 D 2 D 2 D ; a2 b c 3

x 2 / D 0:

Let L D xyz C .x 2 C y 2 C z 2 0D

4abc We want to minimize V D subject to the con3 4 1 1 straint 2 C 2 C 2 D 1. Note that abc cannot be zero. a b c Let   1 4 1 4abc C C 1 : C LD 3 a2 b2 c2

0D

.B/

Thus, either  D 0, or y D x, or y D x.  D 0 is not possible, since it implies x D 0 and y D 0, and the point .0; 0/ does not lie on the given p ellipse. If y D x, then 8x 2 D 16, so x D y D ˙ 2. If y D x, then 4x 2 D 16, so x D y D ˙2. p p The points p onpthe ellipse nearest the origin are . 2; 2/ 2; 2/. The points farthest from the origin are and . .2; 2/ and . 2; 2/. The major p axis of the ellipse lies along y D x and has length 4 2. The minor axis lies along y D x and has length 4.

2:

From the first three equations, x 2 D y 2 and z 2 D 2x 2 . The fourth equation then gives x 2 y 2 4z 4 D 4, or x 8 D 1. Thus x 2 D y 2 D 1 and z 2 D 2. The shortest distance from the origin to the surface xyz 2 D 2 is p 1 C 1 C 2 D 2 units. 7.

2.y 2

2/. For critical points:

D 2x C yz 2

D 2z C 2xyz

.A/

Multiplying .A/ by y and .B/ by x and subtracting we get

 Thus we must consider the two points P D 32 ; 13 ; 23 ,  1 2 2 and Q D 3 ; 3 ; 3 for giving extreme values for D. At P , D D 2. At Q, D D 4. Thus the greatest and least distances from .2; 1; 2/ to the sphere x 2 C y 2 C z 2 D 1 are 4 units and 2 units respectively.

0D

16/. We have

0D

1 .4 C 1 C 4/ D 1 .1 C /2 .1 C /2 D 9 1 C  D ˙3:

6. Let L D x 2 C y 2 C z 2 C .xyz 2

Let L D x 2 C y 2 C .3x 2 C 2xy C 3y 2

D

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1 D 2x

2 3 D ; 8y 18z

.D/

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INSTRUCTOR’S SOLUTIONS MANUAL

so x D 2y D 3z. From (D): x2 C 4



2

x 4

C9



2

x 9

SECTION 13.3

The maximum value is thus

iD1

D 108;

13.

2

so x D 36, and x D ˙6. There are two CPs: .6; 3; 2/ and . 6; 3; 2/. At the first, x C 2y 3z D 18, the maximum value, and at the second, x C 2y 3z D 18, the minimum value. 11.

0D 0D

32;

0D 0D

x ¤ 0; y ¤ 0; z ¤ 0:

0D

Thus we calculate @L @x @L 0D @y @L 0D @z @L 0D @ 0D

D 2x C y 2 z 4 D 2y C 2xyz 4 D 2z C 4xy 2 z 3 D xy 2 z 4

2x D  y2z4 1 ” D  xz 4 1 D ” 2xy 2 z 2



from which it follows that y 2 D 2x 2 and z 2 D 2y 2 D 4x 2 . The constraint equation then gives x.2x 2 /.16x 4 / p D 32, or, simply, x 7 D 1. This implies x D 1, so y D ˙ 2 and z D ˙2. The distance from the surface to the origin is p p 1 C 2 C 4 D 7 units.

14.

D 1 C  C 2x

.A/

D  C 4y

.B/

D

.C /

 C 4z

DxCy

z

.D/

D x 2 C 2y 2 C 2z 2

Let L D x 2 C y 2 C z 2 C .x 2 C y 2 For critical points of L: 0D

12. The maximum will occur at a critical point of the Lagrange function ! n n X X 2 LD xi C  xi 1 :

0D 0D 0D

iD1

For a critical point we have:

0D 1i n

i 1

The first n equations show that xi D 1=.2/ for each i , so xi D x1 for 1  i  n. The constraint equation now gives n X 1 1D xi2 D nx12 ; so x1 D ˙ p : n iD1

8/. For

8:

.E/

CASE II. y C z D 0. Then z D y and, by (D), x D 2y. Therefore, by (E), 4y 2 C 2y 2 C 2y 2 D 8, and so y D ˙1. From this case we obtain two points: .2; 1; 1/ and . 2; 1; 1/. The function f .x; y; z/ D x has maximum value 2 and minimum value 2 when restricted to the curve x Cy D z, x 2 C 2y 2 C 2z 2 D 8.

2x 1 1 D D ; y2z4 xz 4 2xy 2 z 2

@L D 1 C 2xi ; @xi n X @L D xi2 1: 0D @

n:

CASE I.  D 0. Then  D 0 by (B), and 1 D 0 by (A), so this case is not possible.

The first three equations imply that

0D

p

From (B) and (C) we have .y C z/ D 0. Thus  D 0 or y C z D 0.



1:

iD1

@L @x @L @y @L @z @L @ @L @

xi D nx1 D

z/ C .x 2 C 2y 2 C 2z 2

Let L D x C .x C y critical points of L:

The surface has no points where any coordinate is zero, and is not bounded, so it has no farthest point from the origin. To find the closest point we look at critical points of L D x 2 Cy 2 Cz 2 Cxy 2 z 4

n X

(PAGE 773)

@L @x @L @y @L @z @L @ @L @

z 2 / C .x

2z

3/.

D 2x.1 C / C 

.A/

D 2y.1 C /

.B/

D 2z.1

/

D x2 C y2 Dx

From (B), either y D 0 or  D

2z

2 z2

3:

.C / .D/ .E/

1.

CASE I. y D 0. Then (D) implies x D ˙z. If x D z then (E) implies z D 3, so we get the point . 3; 0; 3/. If x D z then (E) implies z D 1, so we get the point .1; 0; 1/. CASE II.  D 1. Then (A) implies  D 0 and (C) implies z D 0. By (D), x D y D 0, and this contradicts (E), so this case is not possible.

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SECTION 13.3 (PAGE 773)

ADAMS and ESSEX: CALCULUS 9

If f .x; y; z/ D x 2 C y 2 C z 2 , then f . 3; 0; 3/ D 18 is the maximum value of f on the ellipse x 2 C y 2 D z 2 , x 2z D 3, and f .1; 0; 1/ D 2 is the minimum value. 15.

Let L D 4 z C .x 2 C y 2 critical points of L: 0D 0D 0D 0D 0D

@L @x @L @y @L @z @L @ @L @

8/ C .x C y C z

17.

Let a/2 C .y b/2 C .z C .a C b/ C .c

L D .x

1/. For

.A/

0D

D 2y C 

.B/

0D

D

.C /

0D

.D/

0D

.E/

0D

D x2 C y2

8

DxCy Cz

1:

From (C),  D 1. From (A) and (B), .x either  D 0 or x D y.

0D

y/ D 0, so

0D

CASE I.  D 0. Then  D 0 by (A), and this contradicts (C), so this case is not possible. CASE II. x D y. Then x D y D ˙2 by (D). If x D y D 2, then z D 3 by (E). If x D y D 2, then z D 5 by (E). Thus we have two points, .2; 2; 3/ and . 2; 2; 5/, where f .x; y; z/ D 4 z takes the values 7 (maximum), and 1 (minimum) respectively. 16. The max and min values of f .x; y; z/ D x C y 2 z subject to the constraints y 2 C z 2 D 2 and z D x will be found among the critical points of L D x C y 2 z C .y 2 C z 2 Thus 0D 0D 0D 0D 0D

@L @x @L @y @L @z @L @ @L @

D1

2/ C .z

x/:

 D 0;

D y 2 C 2z C  D 0;

Dz

2;

0D 0D 0D

@L @x @L @y @L @z @L @a @L @b @L @c @L @ @L @ @L @ @L @

D 2.x

a/ C 

D 2.y

b/

C

.B/

D 2.z

c/



.C /

.A/

D

2.x

a/ C 

.D/

D

2.y

b/ C 

.E/

D

2.z

c/ C 

.F /

Dx

y

.G/

Dy

z

.H /

DaCb

.I /

Dc

.J /

2:

Subtracting (D) and (E) we get x y D a b. From (G), x D y, and therefore a D b. From (I), a D b D 0, and from (J), c D 2. Adding (A), (B) and (C), we get x Cy Cz D aCb Cc D 2. From (G) and (H), x D y D z D 2=3. The minimum distance between the two lines is s p 2  2  2 r  24 2 2 2 2 6 0 C 0 C 2 D D units. 3 3 3 9 3

S D xy C 2xz C 2yz subject to the constraint that xyz D V , where V is a given positive volume. Let L D xy C 2xz C 2yz C .xyz

x:

From the first equation  D 1. From the second, either y D 0 or z D . Ifpy D p 0 then z 2 D p 2, z D p x, so critical points arep . 2; 0; 2/ and . 2; 0; 2/. f has the values ˙ 2 at these points. If z D  then y 2 2z 2 C 1 D 0. Thus 2z 2 1 D 2 z 2 , or z 2 D 1, z D ˙1. This leads to critical points .1; ˙1; 1/ and . 1; ˙1; 1/ where f has values ˙2. The maximum value of f subject to the constraints is 2; the minimum value is 2.

506

z/

18. Let the width, depth, and height of the box be x, y and z respectively. We want to minimize the surface area

D 2yz C 2y D 0;

D y2 C z2

y/ C .y

For critical points of L, we have

D 2x C 

1C

c/2 C .x 2/:

V /:

For critical points of L, @L @x @L 0D @y @L 0D @z @L 0D @ 0D

D y C 2z C yz

,

xyz D xy C 2xz

D x C 2z C xz

,

xyz D xy C 2yz

D 2x C 2y C xy D xyz

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V:

,

xyz D 2xz C 2yz

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 13.3

From the first three equations, xy D 2xz D 2yz. Since x, y, and z are all necessarily positive, we must therefore have x D y D 2z. Thus the most economical box with no top has width and depth equal to twice the height.

21.

(PAGE 773)

Let the width, depth, and height of the box be x, y, and z as shown in the figure. Let the cost per unit area of the back and sides be $k. Then the cost per unit area of the front and bottom is $5k. We want to minimize C D 5k.xz C xy/ C k.2yz C xz/

19. We want to maximize V D xyz subject to 4xC2yCz D 2. Let L D xyz C .4x C 2y C z 2/:

subject to the constraint xyz D V (constant). Let L D k.5xy C 6xz C 2yz/ C .xyz

For critical points of L,

V /:

For critical points of L, 0D 0D 0D 0D

@L @x @L @y @L @z @L @

D yz C 4

,

xyz C 4x D 0

D xz C 2

,

xyz C 2y D 0

D xy C 

,

@L @x @L 0D @y @L 0D @z @L 0D @ 0D

xyz C z D 0

D 4x C 2y C z

2 D 0:

The first three equations imply that z D 2y D 4x (since we cannot have  D 0 if V is positive). The fourth equation then implies that 12x D 2. Hence x D 1=6, y D 1=3, and z D 2=3. The largest box has volume V D

D 5ky C 6kz C yz

,

xyz D 5kxy C 6kxz

D 5kx C 2kz C xz

,

xyz D 5kxy C 2kyz

D 6kx C 2ky C xy

,

xyz D 6kxz C 2kyz

D xyz

V:

From the first three of these equations we obtain 5x . From the 5xy D 6xz D 2yz. Thus y D 3x and z D 2 15 3 fourth equation, V D xyz D x .    2 1=3 2V 1=3 2V , depth 3 , The largest box has width 15 15  1=3 5 2V and height . 2 15

1 1 1 2   D cubic units. 6 3 3 27

20. We want to maximize xyz subject to xyC2yzC3xz D 18. Let L D xyz C .xy C 2yz C 3xz 18/:

back

For critical points of L, side

0D 0D 0D 0D

@L @x @L @y @L @z @L @

D yz C .y C 3z/

,

xyz D .xy C 3xz/

D xz C .x C 2z/

,

xyz D .xy C 2yz/

D xy C .2y C 3x/ D xy C 2yz C 3xz

,

xy D 2yz D 3xz D 6: Thus the maximum volume of the box is V D xyz D

p

.xy/.yz/.xz/ D

p

6  3  2 D 6 cubic units.

y

x

Fig. 13.3-21 22.

From the first three equations xy D 2yz D 3xz. From the fourth equation, the sum of these expressions is 18. Thus

side

bottom

xyz D .2yz C 3xz/

18:

z

front

2

f .x; y; z/ D xy Cz on B D f.x; y; z/ W x 2 Cy 2 Cz 2  1g: For critical points of f , 0 D f1 .x; y; z/ D y; 0 D f3 .x; y; z/ D 2z:

0 D f2 .x; y; z/ D x;

Thus the only critical point is the interior point .0; 0; 0/, where f has the value 0, evidently neither a maximum nor a minimum. The maximum and minimum must therefore occur on the boundary of B, that is, on the sphere x 2 C y 2 C z 2 D 1. Let L D xy C z 2 C .x 2 C y 2 C z 2

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1/:

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SECTION 13.3 (PAGE 773)

ADAMS and ESSEX: CALCULUS 9

For critical points of L, @L @x @L 0D @y @L 0D @z @L 0D @ 0D

24.

D y C 2x

.A/

D x C 2y

.B/

D 2z.1 C /

.C /

2

2

Dx Cy Cz

From (C) either z D 0 or  D

2

1:

Let L D sin

x y z sin sin C .x C y C z 2 2 2

@L 1 x y z D cos sin sin C  @x 2 2 2 2 1 x y z @L D sin cos sin C  0D @y 2 2 2 2 @L 1 x y z 0D D sin sin cos C : @z 2 2 2 2 0D

1 1 p ;˙p ;0 2 2



and

1 1 p ;˙p ;0 2 2

P D sin



1 1 and . 2 2 CASE II.  D 1. (A) and (B) imply that x D y D 0, and so by (D), z D ˙1. f has the value 1 at the points .0; 0; ˙1/. Thus the maximum and minimum values of f on B are 1 and 1=2 respectively. 23. In this problem we do the boundary analysis for Exercise 22 using the suggested parametrization of the sphere x 2 C y 2 C z 2 D 1. We have f .x; y; z/ D xy C z 2

D sin2  sin  cos  C cos2  1 D sin2  sin 2 C cos2  2 D g.;  /

for 0     and 0    2. For critical points of g, 2 sin  cos  2/

0 D g2 .;  / D sin2  cos 2:

y z x sin sin 2 2 2

1 z x y sin sin D 0: 2 2 2 It follows that we must have x D y; all other possibilities lead to a zero value for P . Similarly, y D z. Thus the triangle for which P is maximum must be equilateral: x D y D z D =3. Since sin.=3/ D 1=2, the maximum value of P is 1/8. 25.

We are given that g2 .a; b/ ¤ 0, and therefore that the equation g.x; y/ D C hasa solution  of the form y D h.x/ valid near .a; b/. Since g x; h.x/ D C holds identically for x near a, we must have 0D



ˇ ˇ d  ˇ g x; h.x/ ˇ ˇ dx

xDa

D g1 .a; b/ C g2 .a; b/h0 .a/:

If f .x; y/, subject to the constraint g.x;y/ D C, has an extreme value at .a; b/, then F .x/ D f x; h.x/ has an extreme value at x D a, so 0 D F 0 .a/ D f1 .a; b/ C f2 .a; b/h0 .a/:

The first of these equations implies that either sin  D 0 or cos  D 0. If sin  D 0, then both equations are satisfied. Since cos  D ˙1 in this case, we have g.;  / D 1. If cos  D 0, then sin  D ˙1, and the second equation  3 requires cos 2 D 0. Thus  D ˙ or ˙ . In this case 4 4 1 g.;  / D ˙ . 2 Again we find that f .x; y; z/ D xy C z 2 has maximum 1 when restricted to the value 1 and minimum value 2 surface of the ball B. These are the maximum and minimum values for the whole ball as noted in Exercise 22.

508

.C /

is 0 if any of x, y or z is 0 or . Subtracting equations .A/ and .B/ gives

f takes the values

0 D g1 .;  / D sin  cos  sin 2 D sin  cos .sin 2

.B/

For any triangle we must have 0  x  , 0  y   and 0  z  . Also

1.



.A/

.D/

CASE I. z D 0. (A) and (B) imply that y 2 D x 2 and (D) then implies that x 2 D y 2 D 1=2. At the four points 

/: Then

Together these equations imply that g1 .a; b/f2 .a; b/ D g2 .a; b/f1 .a; b/, and therefore that f2 .a; b/ f1 .a; b/ D D g1 .a; b/ g2 .a; b/



(say).

(Since g2 .a; b/ ¤ 0, therefore, if g1 .a; b/ D 0, then f1 .a; b/ D 0 also.) It follows that 0 D f1 .a; b/ C g1 .a; b/;

0 D f2 .a; b/ C g2 .a; b/;

so .a; b/ is a critical point of L D f .x; y/ C g.x; y/.

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 13.4

26. As can be seen in the figure, the minimum distance p 2 from p .0; 1/ to points of the semicircle y D 1 x is 2, the closest points to .0; 1/ on the semicircle being .˙1; 0/. These points will not be found by the method of Lagrange multipliers because the level curve f .x; y/ D 2 of the function f giving the square of the distance from .x; y/ to .0; 1/ is not tangent to the semicircle at .˙1; 0/. This could only have happened because .˙1; 0/ are endpoints of the semicircle. y

p so that 42 D n, and  D ˙ n=2. The maximum and minimum values of x1 C x2 C    C xn p n subject to x12 C    C xn2 D 1 are ˙ , that is, n and 2 p n respectively. 2.

Let L D x1 C 2x2 C    C nxn C .x12 C x22 C    C xn2 For critical points of L we have

.1;0/

1 @L D 1 C 2x1 , x1 D @x1 2 @L 2 0D D 2 C 2x2 , x2 D @x2 2 @L 3 0D D 3 C 2x3 , x3 D @x3 2 :: : @L n 0D D n C 2xn , xn D @xn 2 @L D x12 C x22 C    C xn2 1: 0D @

x

.0; 1/

Thus

Fig. 13.3-26 27.

1 4 9 n2 C C C    C D1 42 42 42 42 n.n C 1/.2n C 1/ 42 D 1 C 4 C 9 C    C n2 D 6 r 1 n.n C 1/.2n C 1/ D˙ : 2 6

If f .x; y/ has an extreme value on g.x; y/ D 0 at a point .x0 ; y0 / where rg ¤ 0, and if rf exists at that point, then rf .x0 ; y0 / must be parallel to rg.x0 ; y0 /; rf .x0 ; y0 / C rg.x0 ; y0 / D 0 as shown in the text. The argument given there holds whether or not rf .x0 ; y0 / is 0. However, if

Thus the maximum and minimum values of x1 C 2x2 C    C nxn over the hypersphere x12 C x22 C    C xn2 D 1 are

rf .x0 ; y0 / D 0 then we will have  D 0.

Let L D x1 C x2 C    C xn C .x12 C x22 C    C xn2 For critical points of L we have @L @L D 1 C 2x1 ; : : : 0 D D 1 C 2xn @x1 @xn @L 0D D x12 C x22 C    C xn2 1: @

0D

The first n equations give x1 D x2 D    D xn D

1 ; 2

and the final equation gives

s

6 .12 C 22 C 32 C    C n2 / n.n C 1/.2n C 1/ r n.n C 1/.2n C 1/ D˙ : 6

˙

Section 13.4 Lagrange Multipliers in n-Space (page 783) 1.

1/.

0D

p yD 1 x 2

. 1;0/

(PAGE 783)

1/. 3.

The Lagrange function here is

LD

10 X

xi2

iD1

C

10 X

xi

iD1

!

!

10 C 

10 X iD1

ixi

!

!

55 :

For a critical point we need @L D 2xi C  C i; @xi 10 X @L 0D D xi 10 @

0D

.1  i  10/

iD1 10

1 1 1 C 2 C    C 2 D 1; 42 4 4

X @L D ixi 0D @

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55:

iD1

509

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SECTION 13.4 (PAGE 783)

ADAMS and ESSEX: CALCULUS 9

Since

Summing the first equation and using the other two we get

 @2 L 1 D 0 @xi @xj

20 C 10 C 55 D 0:

the Hessian matrix for L at any point is diagonal, with all diagonal elements equal to 2, and so all eigenvalues equal 2 and the matrix is positive definite. Thus,the above value of S is a local minimum value. Since there are no other critical points, and S  0 for all choices of the 10 numbers xi satisfying the constraints, it is an absolute minimum.

Multiplying first equation by i and summing leads to P the 2 (since 10 iD1 i D 385), 110 C 55 C 385:

Together these latter equations imply that  D 2 and  D 0, so that each xi D 2 and S D 10. Since  @2 L 1 if i D j ; D 0 if i ¤ j @xi @xj

5.

the Hessian matrix for L at any point is diagonal, with all diagonal elements equal to 2, and so all eigenvalues equal 2 and the matrix is positive definite. Thus, S D 10 is a local minimum value. Since there are no other critical points, and S  0 for all choices of the 10 numbers xi satisfying the constraints, it is an absolute minimum.

The Lagrange function is L.x; y; u; v; ; / D .x u/2 C.y v/2 C.y x 2 /C.v 2u2 1/: Its critical points must satisfy

10 X iD1

10 X

xi2 C 

xi

iD1

!

0D !

10 C 

10 X iD1

ixi

!

!

0D

60 :

0D

For a critical point we need @L 0D D 2xi C  C i; @xi 10 X @L 0D D xi 10 @ 0D

@L D @

iD1 10 X

ixi

0D .1  i= le10/

60:

iD1

Summing the first equation and using the other two we get 20 C 10 C 55 D 0: Multiplying first equation by i and summing leads to P the 2 (since 10 iD1 i D 385), 120 C 55 C 385:

0D

v/ C 

2x

.B/

D

2.x

u/

D

2.y

v/ C 

Dy

x2

Dv

2u2

.A/

4u

.C / .D/ .E/

1:

.F /

p 6 3 6 7 1 ; ; ; ; ; 2 2 4 4 2 p p 6 3 6 7 ; ; ; ; 2 2 4 4

1 2

!

1 ; 2

and 1 2

!

:

Now the Hessian matirx for L is

   10  1 X 2i 2 X 4 8i 4i 2 340 1 D C C C : D 0 SD 3 33 9 99 1089 33

510

D 2.y

p

RD

The corresponding value of S is

iD1

u/

If  D 1=2, then  D 1=2, x D 2u, and (E) and (F) then force u2 D 6=16. This leads to two more critical points

4=3 and

2 2i C : 3 33

D 2.x

From (B) and (D),  D . Then, from (A) and (C), either  D 0 or x D 2u. If  D 0, then  D 0 and (A) and (C) imply x D u and y D v. This is not possible because then (E) and (F) would imply x 2 C 1 D 0. Thus  ¤ 0 and x D 2u. Then A implies u D 0 or  D 1=2. If u D 0, then x D 0, y D 0, v D 1, and  D 2. One critical point is P D .0; 0; 0; 1; 2; 2/.

QD

Together these latter equations imply that  D  D 4=33, so that xi D

@L @x @L @y @L @u @L @v @L @ @L @

0D

4. The Lagrange function here is LD

if i D j ; if i ¤ j

iD1

0

B HDB @

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2

2 0 2 0

0 2 0 2

2 0 2 4 0

1 0 2C C 0 A 2

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 13.5

At Q this Hessian becomes

HQ

0

1 B 0 B D@ 2 0

0 2 0 2

, then the restriction of HP to the tangent space to the constraint manifold at P is   6 2 T HP jT g D E HP E D ; 2 18

1 0 2C C; 0 A 2

2 0 4 0

p which has eigenvalues 6 ˙ 2 37, of opposite sign. Thus P has saddle behaviour.

and its eigenvalues r satisfy ˇ ˇ1 r ˇ ˇ 0 0 D ˇˇ ˇ 2 ˇ 0

0 2

r 0 2

2 0 4 r 0

ˇ 0 ˇˇ 2 ˇˇ 0 ˇˇ 2 rˇ

which, on simplification by minors turns out to be r 2 .r 4/.r 5/ D 0. The eigenvalues are 0; 0; 4; 5, so HQ is not positive or negative definite. We calculate the restriction of HQ to the tangent space Tg to the constraint manifold at Q. Observe p that the vec6ex C ey and tors U1 D 2xex C eyp D 6eu C ev are normal to Tg. U2 D 4ueu C ev D We need two perpendicular unit vectors eachpperpendicular p to both v1 and p vectors V 1 D .ex C 6ey /= 7 and p v2 The V 2 D .eu C 6ev /= 7 will clearly do. Accordingly, let p 1= 7 p B .6=7/ EDB @ 0 0 0

The p minimum distance between p the two curves is the value of S at Q (or R) and is 7=4 units.

Section 13.5 The Method of Least Squares (page 789) 1.

n h X .x iD1

n

0D

X @S D2 .x @x

0 0 C p C: 1= 7 A p .6=7/

n X

13=7 2 2 16=7

2 0 18 0

iD1

n X iD1

xi

!

!

yi :

n n 1X 1X xi D x, and y D yi D y. n n iD1 iD1 Place the power plant at the position whose coordinates are the averages of the coordinates of the machines. P We want to minimize S D niD1 .axi2 yi /2 . Thus



2.

n

0D

X dS D 2.axi2 da

1

0 2C C; 0 A 2

p which has eigenvalues 0, 4, 6 ˙ 2 37, again inconclusive. At P , the normal vectors to the constraint manifold are U_1 D ey and U_2 D ev , so an orthonormal basis for the tangent space is given by vectors V_1 D ex and V_2 D eu . Thus, if 0 1 1 0 B0 0C C EDB @0 1A 0 0

iD1 n X

D2

Proceeding similarly with P , we evaluate 0 2 0 2

yi / D 2 ny

.y

iD1

n X

Thus x D

which p has eigenvalues .29 C 793/=14  4:08 and 793/=14  0:6, both positive. So S has a local .29 minimum at Q, and by symmetry, also at R.

6 B 0 HP D B @ 2 0

xi / D 2 nx

iD1

@S 0D D2 @y

p

0

i y2 /2 :

xi /2 C .y

Thus we must have

1



If the power plant is located at .x; y/, then x and y should minimize (and hence be a critical point of) SD

Then the Hessian restricted to the tangent space at Q is HQjT g D ET H E D

(PAGE 789)

and a D 3.

Pn

iD1

xi2 yi

We minimize S D 0D and a D

4.

Pn

iD1





Pn

.axi4

yi /xi2 xi2 yi /;

iD1

Pn

iD1

iD1 .ae

xi

 xi4 .

yi /2 . Thus

n

X dS D2 .ae xi da

i

yi /e x ;

iD1

yi e xi





Pn

iD1

 e 2xi .

We choose a, b, and c to minimize SD

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n  X axi C byi C c iD1

zi

2

:

511

lOMoARcPSD|6566483

SECTION 13.5 (PAGE 789)

ADAMS and ESSEX: CALCULUS 9

that is,

Thus n

X @S 0D D2 .axi C byi C c @a

zi /xi

.axi C byi C c

zi /yi

.axi C byi C c

zi /:

@S D2 0D @b 0D

@S D2 @c

iD1 n X

iD1 n X iD1

so

P 2 P P P Let APD xi , BPD xi yi , P C D xi , D D P yi2 , ED yi , F D xi zi , G D yi zi , and H D zi . In terms of these quantities the above equations become C C C

Aa Ba Ca By Cramer’s Rule is ˇ ˇF B 1 ˇˇ G D aD  ˇˇ H E ˇ ˇA B 1 ˇˇ B D cD  ˇˇ C E

C C C

Bb Db Eb

D D D

Cc Ec nc

.p

7.

F G H:

ˇ ˇ ˇA F C ˇ ˇ 1 ˇˇ B G E ˇ; bD  ˇˇ C H n ˇˇ ˇ ˇ ˇA B C ˇ ˇ ˇ where  D ˇˇ B D E ˇˇ : ˇC E n ˇ

5. If x D .x1 ; : : : ; xn /, y D .y1 ; : : : ; yn /, z D .z1 ; : : : ; zn /, w D .1; : : : ; 1/, and p D ax C by C cw, we want to choose a, b, and c so that p is the vector projection of z onto the subspace of R3 spanned by x, y and w. Thus p z must be perpendicular to each of x, y, and w: z/  x D 0;

z/  y D 0;

.p

.p

Thus

iD1

.p C qxi2

SD 8.

z/  w D 0:

X @S .p C qxi2 D2 @p

9.

iD1 n

X @S 0D D2 .p C qxi2 @q

pe qxi /2 :

n  X ln.p C qxi / iD1

yi

2

:

The relationship y D px C qx 2 is linear in p and q, so we choose p and q to minimize

yi /xi2 ;

iD1

512

.yi

iD1

These values of p and q are not the same values that minimize the expression SD

yi /

n X

We transform y D ln.p C qx/ into the form e y D p C qx, which is linear in p and q. We let i D e yi and use the regression line  D ax C b obtained from the data .xi ; i /, with a D q and b D p. Using the formulas for a and b obtained in the text, we have P P P n . xi e yi / . xi / . e yi / qDaD P 2 P n x . xi /2 P 2 P i y P P xi . e i / . xi / . xi e yi / pDbD : P 2 P n xi . xi /2

yi /2 :

n

0D

We transform y D pe qx into the form ln y D ln p C qx, which is linear in ln p and q. We let i D ln yi and use the regression line  D a C bx obtained from the data .xi ; i /, with b D q and a D ln p. Using the formulas for a and b obtained in the text, we have P P P n . xi ln yi / . xi / . ln yi / ln p D a D P 2 P 2 n x . xi / P 2 P i P P xi . ln yi / . xi / . xi ln yi / qDbD  P 2 P n xi . xi /2 These values of p and q are not the same values that minimize the expression

6. The relationship y D p C qx 2 is linear in p and q, so we choose p and q to minimize n X

P P 4 P 2  P 2 . yi / xi xi yi xi pD P 4 P 2 2 n x x P 2  iP Pi 2  n xi yi . yi / xi : qD P 4 P 2 2 n xi xi

p D ea :

When written in terms of the components of the vectors involved, these three equations are the same as the equations for a, b, and c encountered in Exercise 4, and so they have the same solution as given for that exercise.

SD

P P 2yi xi yi ;

D D

This is the result obtained by direct linear regression. (No transformation of variables was necessary.)

(Theorem 5 of Section 1.6) the solution ˇ C ˇˇ E ˇˇ ; nˇ ˇ F ˇˇ G ˇˇ ; Hˇ

P 2 P xi4  q xi q

C C

Pnp2  xi p

SD

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n X iD1

.pxi C qxi2

yi /2 :

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

Thus

SECTION 13.5

that is,

n

X @S D2 .pxi C qxi2 0D @p

P

yi /xi

iD1 n

X @S .pxi C qxi2 0D D2 @q

yi /xi2 ;

P 2 P xi3  p xi p

P P x2i yi xi yi ;

so

iD1

so

P 3 P xi4  q xi q

D D

P P 4 P 2  P 3 . xi yi / xi xi yi xi pD P 2 P 4 P 3 2 x x xi P 3 P 2  Pi 2  i P . xi yi / xi xi xi yi qD : P 2 P 4 P 3 2 xi xi xi

This is the result obtained by direct linear regression. (No transformation of variables was necessary.) p 10. We transform y D .px C q/ into the form y 2 D px C q, which is linear in p and q. We let i D yi2 and use the regression line  D ax C b obtained from the data .xi ; i /, with a D p and b D q. Using the formulas for a and b obtained in the text, we have  P P 2 xi yi2 . xi / yi  P 2 P n xi . xi /2  P 2 P 2 P P xi yi . xi / xi yi2 qDbD : P 2 P n xi . xi /2

pDaD

n

 e 2xi p np

11.

iD1

The relationship y D pe x C qe we choose p and q to minimize SD

yi

n  X

x

pe xi C qe

iD1

2

:

yi

Therefore

 P 2  P 2 xi4 xi yi xi P 4 P 2 2 n xi xi 55:18  4051 1984:50  115  0:42 D 2 P 62  4051P 115 P 2  n xi yi . yi / xi qD P 4 P 2 2 n xi xi 6  1984:50 55:18  115  0:50: D 6  4051 1152

pD

.

X @S pe xi C qe D2 @p n

xi

iD1 n

X @S 0D D2 pe xi C qe @q iD1

xi

P

yi /

P

We have (approximately) y D 0:42 C 0:50x 2 . The predicted value of y at x D 5 is 0:42 C 0:50  25  12:1: 13.

Choose a, b, and c to minimize SD

n  X axi2 C bxi C c

yi

iD1

2

:

n

2

:

xi

X @S D2 .axi2 C bxi C c @a

yi /xi2

iD1 n

X @S 0D D2 .axi2 C bxi C c @b @S D2 @c

iD1 n X iD1

.axi2 C bxi C c

yi /xi yi /:

P 4 P 3 P 2 P Let A P D xi , B D xi , D D xi , P xi , C D P 2 H D xi yi , I D xi yi , and J D yi . In terms of these quantities the above equations become

 yi e xi  yi e

0D

0D

Thus 0D

2xi

e

Thus

is linear in p and q, so

xi

P D P e xi yi D e xi yi ;

12. We use the result of Exercise 6. We have n D 6 and X X xi2 D 115; xi4 D 4051; X X yi D 55:18; xi2 yi D 1984:50:

These values of p and q are not the same values that minimize the expression n  X p pxi C q

P nq2x  e i q

This is the result obtained by direct linear regression. (No transformation of variables was necessary.)

P

SD

C C

 P x P . e i yi / n . e xi yi / P 2x  P 2x  e i e i n2 P 2x  P x P x e i . e i yi / n . e i yi / : qD P 2x  P 2x  e i e i n2 P

pD

that is, C C

(PAGE 789)

:

Aa Ba Ca

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C C C

Bb Cb Db

C Cc C Dc C nc

D D D

H I J:

513

lOMoARcPSD|6566483

SECTION 13.5 (PAGE 789)

By Cramer’s Rule is ˇ ˇH B 1 ˇˇ I C aD  ˇˇ J D ˇ ˇA B 1 ˇˇ B C cD  ˇˇ C D 14.

ADAMS and ESSEX: CALCULUS 9

(Theorem 5 of Section 1.6) the solution

x

To minimize I D b so that

ˇ ˇ ˇA H C ˇ ˇ 1 ˇˇ B I D ˇ; bD  ˇˇ C J n ˇˇ ˇ ˇ ˇA B C ˇ ˇ ˇ where  D ˇˇ B C D ˇˇ : ˇC D n ˇ

ˇ C ˇˇ D ˇˇ ; nˇ ˇ H ˇˇ I ˇˇ ; J ˇ

Since y D pe x C q C re

17.

Z

1 0

18. To minimize c so that

Z



1

0D2 0D2

0

16. To maximize I D a so that Z



Z



ax.

0

sin x

x/

2

0

 0

514



120 x. 5

x/

sin x

 dx D 2

Z

Z

x3

ax 2

2

dx D

1 : 448

c/2 dx, choose a, b and

bx

1

.x 3

ax 2

bx

c/. x 2 / dx

.x 3

ax 2

bx

c/. x/ dx

.x 3

ax 2

bx

c/. 1/ dx;

0 1 0 1 0

C C C

b 4 b 3 b 2

C C C

c 3 c 2

1 6 1 5 1 4

D D D

c

0

0D2

Z

Z



.sin x

ax 2

bx/. x 2 / dx

.sin x

ax 2

bx/. x/ dx:

0  0

We omit the details of the evaluation of the integrals. The result of the evaluation is that a and b satisfy 5 a 5 4  a 4

8:

2

.x 3

Z

0D2

0

(We have omited the details of evaluation of these integrals.) Hence a D 120= 5 . The minimum value of I is Z

19.

dx, we choose

 x/ sin x x. x/ dx Z  x/2 dx 2 x. x/ sin x dx

1 16

3 1 3 , and c D . for which the solution is a D , b D 2 5 20 Z  To minimize .sin x ax 2 bx/2 dx we choose a and

b so that

 2 ax.

dI D 0D da Z  0 D 2a x 2 .  5a D 15

 5x 5 C x 6 dx 3 5 1 1 C D : 18 7 252

15x 2 16

a 5 a 4 a 3

Thus a D 5=6, and the minimum value of I is 25x 4 36 5 D 36

2b 1 2a C 5 3 3 1 2a C 2b : x 3 / dx D 3 2 x 3 /x 2 dx D

that is,

0



x 3 /2 dx, we choose a and

0

0D2

Z 1 dI 2.ax 2 x 3 /x 2 dx D 0D da 0  ˇ1 x5 2x 6 ˇˇ 2a 1 D 2a : ˇ D 5 6 ˇ 5 3 1

.ax 2 C b

Solving these two equations, we get a D 15=16 and b D 1=16. The minimum value of I is

0

Z

0

Z 1 @I D 2.ax 2 C b @a 0 Z 1 @I D 2.ax 2 C b 0D @b 0

e x y D p.e x /2 C qe x C r;

15.

1

0D

is equivalent to

we let i D e xi and i D e xi yi for i D 1; 2; : : : ; n. We then have p D a, q D b, and r D c, where a, b, and c are the values calculated by the formulas in Exercise 13, but for the data .i ; i / instead of .xi ; yi /. Z 1 To minimize I D .ax 2 x 3 /2 dx, we choose a so that

Z

C C

4 b 4 3  b 3

D

2

D

for which the solution is

480  0:00227: 5

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20 2 . 5 12 b D 4 .20 

aD

16/  2 /:

;

4

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

20. J D

Z

1

a sin x

.x

SECTION 13.5

and, since

c sin 3x/2 dx.

b sin 2x

1

Z

To minimize J , choose a, b, and c to satisfy



0

@J 0D @a D

2

1

a sin x

.x

b sin 2x

c sin 3x/ sin x dx

an D

1

2 .a 2/  @J 0D @b Z 1 D 2 .x a sin x

22.

b sin 2x

c sin 3x/ sin 2x dx

1

2 .b C 1/  @J 0D @c Z 1 D 2 .x a sin x

0  2

if k ¤ n if k D n D 1; 2; : : :

b sin 2x

c sin 3x/ sin 3x dx

f .x/ cos nx dx

0

We have omitted the details of evaluation of these integrals, but note that 1

sin mx sin nx dx D 0

if m and n are different integers. The equations above imply that a D 2=, b D 1=, and c D 2=.3/. These are the values that minimize J .

The Fourier sine series coefficients for f .x/ D x on .0; / are Z 2  2 bn D x sin.nx/ dx D . 1/n 1  0 n

I D



f .x/

0

n X

a0 2

ak cos kx

kD1

!2

Z



f .x/

0

a0 2

n X

ak cos kx

kD1



Z



f .x/ 0

a0 2

n X

!

!

for n D 1; 2; : : :. Thus 2 a0 D 

Z

1 4 X cos..2n C 1/x/ :  .2n C 1/2

Since the terms of this series are all even functions, and the series converges to x if 0 < x < , it will converge to x D jxj if  < x < 0. 1 2



Remark: since jxj is continuous at x D 0, the series also converges at x D 0 to 0. It follows that

dx;

ak cos kx . cos nx/ dx

kD1

2 sin nx: n

nD0

dx

1C

and @I D2 0D @an

1

Thus the Fourier cosine series is

we require @I 0D D2 @a0

. 1/n

The Fourier cosine series coefficients for f .x/ D x on .0; / are Z 2  a0 D x dx D   0   n Z  2 1 . 1/ 2 an D x cos.nx/ dx D  0 n2  ( 0 if n  2 is even 4 D if n  1 is odd. n2 

To minimize Z

.n D 1; 2; : : :/:

Since x and the functions sin nx are all odd functions, we would also expect the series to converge to x on . ; 0/. 23.

1



nD0

2/:

Z

Z

1 X

1

2 .3c 3

2 

for n D 1; 2; : : :. Thus the series is

D

21.

cos kx cos nx dx D

(

we also have Z

D

D

(PAGE 789)

24.

1 X 1 2 1 1 C 2 C  D D : 2 2 3 5 .2n C 1/ 4 nD0

We are given that x1  x2  x3  : : :  xn . To motivate the method, look at a special case, n D 5 say. x1

x2

x3

x4

x5



f .x/ dx;

Fig. 13.5-24

0

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515

lOMoARcPSD|6566483

SECTION 13.5 (PAGE 789)

ADAMS and ESSEX: CALCULUS 9

5 X iD1

jx

If x D 1 we get

xi j

D .x3 D .x5

x1 / C .x3 x1 / C .x4

x2 / C 0 C .x4 x2 /:

x3 / C .x5

x3 /

iD1

jx

xi j D .x5

x1 / C .x4

x2 / C jx

x3 j:

3.

jx

iD1

xi j D

n=2 X iD1

jxnC1

i

F .x/ D

1.

Z

0 1

1 t dt D xC1 x

xi j;

2.

Z

Z

1

e

1 1

u2

I.x; y/ D

.x > 1/

t x ln t dt D

du D

p



p

4.

dt D

516

1

p

xt 2

e

Z

yt 2

t2 1

dt , where x > 0 and

e

xt 2

dt

Let I.x; y/ D

1

e

xt 2

t2

1

Z

1 0

e

tx

yt 2

p p y dt D 2 

p  x :

ty

dt , where x > 1 and y > ln t Z 1 @I 1 D t x dt D @x xC1 0 1 @I D : @y y C1

Z

dx D ln.x C 1/ C C1 .y/ xC1 1 @I @C1 D D ) C1 .y/ D ln.y C 1/ C C2 yC1 @y @y   xC1 I.x; y/ D ln C C2 : y C1

Let u D xt du D x dt

2xt 2 e

e

1

Thus I.x; y/ D

p  dt D 2 x 1 p Z 1  2 2 : t 2 e x t dt D 2x 3 1

Z

Z

Then

 : x 1 Differentiate with respect to x: e

x2t 2

dt D

But I.x; x/ D 0. Therefore C2 D 0, and

1 .x C 1/2 0 Z 1 2 F 00 .x/ D t x .ln t /2 dt D .x C 1/3 0 :: : Z 1 . 1/n nŠ F .n/ .x/ D : t x .ln t /n dt D .x C 1/nC1 0 F 0 .x/ D

t2

t 2e

p Let xt D s p 1 x dt D ds p Z 1 1  2 D p e s ds D p : x 1 x p  @I D p . Now Similarly, @y y Z p p dx  p D 2 x C C1 .y/ I.x; y/ D x p  @I @C1 p D ) C1 .y/ D 2 y C C2 p D y @y @y p p p  I.x; y/ D 2  y x C C2 :

Section 13.6 Parametric Problems (page 798) 1

1

@I D @x

and the sum will increase if x is outside that interval. In this case the value of x which minimizes the sum is not unique unless it happens that xn=2 D x.n=2/C1 .

Z

Z

Let I.x; y/ D y > 0. Then

Thus the minimum sum occurs P if x D x3 . In general, if n is odd, then niD1 jx xi j is minimum if x D x.nC1/=2 , the middle point of the set of points fx1 ; x2 ; : : : ; xn g. The value of x is unique in this case. If n is even and x satisfies xn=2  x  x.n=2/C1 , then n X

1

2 and let x D 1: p Z 1 3  2 : t 4 e t dt D 4 1

Divide by

If x moves away from x3 in either direction, then 5 X

Z

 . 2 1 Differentiate ./ with respect to x again: p Z 1 3  2 2 2xt 4 e x t dt D : 2x 4 1

If x D x3 , then

t 2 x2

./

But I.x; x/ D 0, so C2 D 0. Thus   Z 1 x xC1 t ty dt D ln I.x; y/ D ln t yC1 0

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1.

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

for x > Z

1 and y >

SECTION 13.6

1.

8.

1

1 5. if x > 0. e xt sin t dt D 1 C x2 0 Multiply by 1 and differentiate with respect to x twice: Z

1

2x .1 C x 2 /2 0 Z 1 2.3x 2 1/ : t 2 e xt sin t dt D .1 C x 2 /3 0

6.

F .x/ D F 0 .x/ D

Z

Z

1 0

1

xt

e

sin t dt D

sin t dt t

xt

e

xt

te

0

sin t dt D

Z

1 1 C x2

.x > 0/:

dx D tan 1 x C C . 1 C x2 Now, make the change of variable xt D s in the integral defining F .x/, and obtain

Therefore F .x/ D

F .x/ D

Z

1

s

e

0

sin.s=x/ ds D s=x x

Z

1

s

e s

0

sin

9.

s ds: x

ˇx ˇ 1  dt 1 t ˇ D tan for x > 0. ˇ D 2 C t2 ˇ x x x 4x 0 0 Differentiate with respect to x: Z x 1  2x dt C D 2 2 2 2x 2 4x 2 0 .x C t /   Z x 1 1  dt D 2 2 2 2x 4x 2 2x 2 0 .x C t / 1  C 3: D 8x 3 4x Differentiate with respect to x again:   Z x 3  1 4x dt 1 C D C 2 2 3 4x 4 x4 8 4 0 .x C t /   Z x 1 3 3 1 dt D 2 2 3 4x 8x 4 4x 4 4x 4 0 .x C t / 3 1 D C 5: 32x 5 4x Z x .x t /n f .t / dt ) f .a/ D 1 f .x/ D 1 C a Z x f 0 .x/ D n .x t /n 1 f .t / dt a Z x f 00 .x/ D n.n 1/ .x t /n 2 f .t / dt

Z

x

a

:: :

Since j sin.s=x/j  s=x if s > 0, x > 0, we have 1 jF .x/j  jxj Hence

1 0

1 e s ds D !0 jxj

In particular,

Z

1 0

e

xt

 sin t dt D t 2

tan

1

x:

Z

1

Z0 1 0

 2x dt D .x 2 C t 2 /2 2x 2  dt D : .x 2 C t 2 /2 4x 3

Differentiate with respect to x again: Z

1

Z0 1 0

4x dt 3 D .x 2 C t 2 /3 4x 4 dt 3 D : 2 2 3 .x C t / 16x 5

.x/ D nŠ

Z

x

f .t / dt a

Z

f .nC1/ .a/ D nŠf .a/ D nŠ:

)

x

f .x/ D C x C D C .x t /f .t / dt ) 0 Z x f 0 .x/ D C C f .t / dt ) f 0 .0/ D C

f .0/ D D

0

R 1 sin t  dt D lim F .x/ D : 0 x!0 t 2

1

.n/

f .nC1/ .x/ D nŠf .x/ 10.

ˇ1 ˇ dt 1  1 t ˇ D tan for x > 0. ˇ D 2 2 ˇ x Ct x x 2x 0 0 Differentiate with respect to x: Z

f

as x ! 1:

  C C D 0, and C D . Therefore 2 2 F .x/ D

7.

Z

(PAGE 798)

11.

f 00 .x/ D f .x/ ) f .x/ D A cosh x C B sinh x D D f .0/ D A; C D f 0 .0/ D B )f .x/ D D cosh x C C sinh x: Z x f .x/ D x C .x 2t /f .t / dt ) f .0/ D 0 0 Z x f .t / dt ) f 0 .0/ D 1 f 0 .x/ D 1 xf .x/ C 0

f 00 .x/ D

xf 0 .x/ C f .x/ D xf 0 .x/: du x2 If u D f 0 .x/, then D x dx, so ln u D C ln C1 . u 2 Therefore 2 f 0 .x/ D u D C1 e x =2 : f .x/

2

We have 1 D f 0 .0/ D C1 , so f 0 .x/ D e x =2 and Z x 2 f .x/ D e t =2 dt C C2 : 0

But 0 D f .0/ D C2 , and so Z f .x/ D

x

e

t 2 =2

dt:

0

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517

lOMoARcPSD|6566483

SECTION 13.6 (PAGE 798)

12.

ADAMS and ESSEX: CALCULUS 9

Z 1 f .x/ D 1 C .x C t /f .t / dt 0 Z 1 f 0 .x/ D f .t / dt D C; say;

From the second equation, y D x tan3 c. Thus x .1 C tan2 c/ D 1 cos c

0

since the integral giving f 0 .x/ does not depend on x. Thus f .x/ D A C C x, where A D f .0/. Substituting this expression into the given equation, we obtain Z

A C Cx D 1 C

0

which implies that x D cos3 c, and hence y D sin3 c. The envelope is the astroid x 2=3 C y 2=3 D 1.

1

17.

.x C t /.A C C t / dt

D 1 C Ax C

We eliminate c from the pair of equations

Cx C A C C : 2 2 3

@ f .x; y; c/ D 1 C 2.c @c

Therefore A 2

C Cx 3

1



 A D 0:

C 2

Thus c D x

This can hold for all x only if A 2

1

C D0 3

and

A D 0:

A 2A D 1, so that A D 2 3 12. Therefore f .x/ D 6 12x. c2

f .x; y; c/ D 2cx

@ f .x; y; c/ D 2x @c

14.

x2

.x

x

yD0

19.

sin c D 0

c/ sin c

cos c D 0:

x/ C 2.c

1D0

y/ D 0:

2

y 2

C

y

2

x 2

D1

Not every one-parameter family of curves in the plane has an envelope. The family of parabolas y D x 2 C c evidently does not. (See the figure.) If we try to calculate the envelope by eliminating c from the equations

Thus c D x and y 0 sin x D 0. The envelope is y D sin x.

f .x; y; c/ D y

x2

@ f .x; y; c/ D 1 D 0; @c

We eliminate c from the pair of equations f .x; y; c/ D x cos c C y sin c 1 D 0 @ f .x; y; c/ D x sin c C y cos c D 0: @c

c/2

p or x y D ˙ 2. These two parallel lines constitute the envelope of the given family which consists of circles of radius 1 with centres along the line y D x.

y D 0. The envelope is

@ f .x; y; c/ D cos c C .x @c

15.

cD0

we fail because the second equation is contradictory. y

Squaring and adding these equations yields x 2 C y 2 D 1, which is the equation of the envelope. x

16. We eliminate c from the pair of equations y x C 1D0 cos c sin c @ x sin c y cos c f .x; y; c/ D D 0: @c cos2 c sin2 c f .x; y; c/ D

518

1 . 4

Thus c D .x C y/=2, and

2c D 0:

c/ cos c

c/2 C .y

@ f .x; y; c/ D 2.c @c

6 and

We eliminate c from the pair of equations f .x; y; c/ D y

x/ D 0:

1 . The envelope is the line y D x 2

f .x; y; c/ D .x

13. We eliminate c from the pair of equations

Thus c D x and 2x 2 y D x2.

yD0

18. We eliminate c from the pair of equations C 2

Thus C D 2A and

C D

c/2

f .x; y; c/ D c C .x

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yDx 2 Cc

Fig. 13.6-19

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 13.6

20. The curve xp2 C.y c/2 D kc 2 is a circle with centre .0; c/ and radius kc, provided k > 0. Consider the system: f .x; y; c/ D x 2 C .y

@ f .x; y; c/ D @c

2.y

c/2 c/

22.

(PAGE 798)

If the family of surfaces f .x; y; z; ; / D 0 has an envelope, that envelope will have parametric equations x D x.; /;

kc 2 D 0

y D y.; /;

z D z.; /;

giving the point on the envelope where the envelope is tangent to the particular surface in the family having parameter values  and . Thus   f x.; /; y.; /; z.; /; ;  D 0:

2kc D 0:

The second equation implies that y c D kc, and the first equation then says that x 2 D k.1 k/c 2 . This is only possible if 0  k  1. The cases k D 0 and k D 1 are degenerate. If k D 0 the “curves” are just points on the y-axis. If k D 1 the curves are circles, all of which are tangent to the x-axis at the origin. There is no reasonable envelope in either case. If 0 < k < 1, the envelope is the pair of lines given p p k by x 2 D y 2 , that is, the lines 1 kx D ˙ ky. 1 k p These lines make angle sin 1 k with the y-axis.

Differentiating with respect to , we obtain f1

@y @z @x C f2 C f3 C f4 D 0: @ @ @

However, since for fixed , the parametric curve x D x.t; /;

y

y D y.t; /;

z D z.t; /

is tangent to the surface f .x; y; z; ; / D 0 at t D , its tangent vector there, TD

circles x 2 C.y c/2 Dkc 2

envelope

@x @y @z iC jC k; @ @ @

is perpendicular to the normal

x

N D rf D f1 i C f2 j C f3 k;

.1 k/x 2 Dky 2

so

@x @y @z C f2 C f3 D 0: @ @ @ @f Hence we must also have D f4 .x; y; z; ; / D 0: @ @f D 0. Similarly, @ The parametric equations of the envelope must therefore satisfy the three equations f1

Fig. 13.6-20

21.

We eliminate c from the equations f .x; y; c/ D y 3

@ f .x; y; c/ D @c

f .x; y; z; ; / D 0 @ f .x; y; z; ; / D 0 @ @ f .x; y; z; ; / D 0: @

.x C c/2 D 0

2.x C c/ D 0:

Thus x D c, and we obtain the equation y D 0 for the envelope. However, this is not really an envelope at all. The curves y 3 D .x C c/2 all have cusps along the x-axis; none of them is tangent to the axis.

The envelope can be found by eliminating  and  from these three equations. 23.

y

x f .x;y;c/Dy 3 .xCc/2 D0

Fig. 13.6-21

To find the envelope we eliminate  and  from the equations x sin  cos  C y sin  sin  C z cos  D 1 x cos  cos  C y cos  sin  z sin  D 0 x sin  sin  C y sin  cos  D 0:

.1/ .2/ .3/

Multiplying (1) by cos  and (2) by sin  and subtracting the two gives z D cos :

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519

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SECTION 13.6 (PAGE 798)

ADAMS and ESSEX: CALCULUS 9

At  D 0 we have y.x; 0/ D

Therefore (2) and (3) can be rewritten

Squaring and adding these equations gives 2

2y2

2

x C y D sin :

2

2

2

2

/2 C z 2 D

2.x

/ D ;

/ D :

2.y

Thus  D 2x,  D 2y, and 27.

x 2 C y 2 C z 2 D 2x 2 C 2y 2 : The envelope is the cone z 2 D x 2 C y 2 . 25.

y C  sin.y/ D x ) y D y.; x/ @y @y C sin.y/ C  cos.y/ D0 @ @  2 @2 y @y @y 2 C 2 cos.y/   sin.y/ @ 2 @ @ @2 y C  cos.y/ 2 D 0: @ If  D 0 then y D x, so y.x; 0/ D x. Also, at  D 0, y .x; 0/.1 C 0/ D that is, y .x; 0/ D

sin.y.x; 0// D

sin.x/; y

26.

y 2 C e

D 1 C x2

y2

2

520

1 2

2.1Cx 2 /

:

x

y D y.x; / D y.x; 0/ C y .x; 0/ C

2 y .x; 0/ C    2Š

D

2  sin.2x/ C    2

2yy C e 2ye y y D 0   2 2 2y 1 e y y C e y D 0     2 2 2 2y 1 e y y 2ye y y C 2y 2ye y y y   2 2 C 2y 1 e y y 2ye y y D 0:

e

32x 2 : 125

Thus

28. y2



1 , and 2

2x D 1 5 1C  4   1 2x 4x 1 2 5 D D  2 2 1 1C 4

y .x; 0/ D

Thus

 sin.x/ C

1 4.1 C x 2 /3=2

x D1 1 C y2 2xyy x D0 2y C 1 C y 2 .1 C y 2 /2   @ 2xyy 4xyy  D 0: 2y .1 C y 2 /2 @ .1 C y 2 /2 At  D 0 we have y.x; 0/ D

y .x; 0/.1 C 0/ D 2 cos.x/y .x; 0/ C 0 D 2 cos.x/ sin.x/ D  sin.2x/:

Dx

1 C x2

C

2y C

sin.x/. Also,

y D y.x; / D y.x; 0/ C y .x; 0/ C

p

y2 1

2 y D y.x; / D y.x; 0/ C y .x; 0/ C y .x; 0/ C    2Š p  .1Cx 2 / 2 p e D 1Cx 2 1 C x2   2 1 1 2 e 2.1Cx / C    : p C 2 4.1 C x 2 /3=2 1 C x2

 2 C 2 . 2 Differentiate with respect to  and : /2 C .y

y2



Thus

the envelope is the sphere of radius 1 centred at the origin. .x

y C 2yy D 0

y .x; 0/ D

x C y C z D sin  C cos  D 1I

24.

y2

4ye

yy D 2yy e

Therefore 2

1 C x 2 , and

p 2 2 1 C x 2 y .x; 0/ C e .1Cx / D 0 1 2 p e .1Cx / y .x; 0/ D 2 1 C x2

x cos  C y sin  D sin  x sin  y cos  D 0: 2

p

1 2

2x 5

2 y .x; 0/ C    2Š

16 2 x 2 C : 125

Let y.x; / be the solution of y C y 5 D

1 . Then we have 2

  y 1 C 5y 4 C y 5 D 0   y 1 C 5y 4 C 20y 3 y2 C 10y 4 y D 0     y 1 C 5y 4 C y 60y 3 y C 15y 4 C 60y3 y 2 C 60y 3 y2 D 0:

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lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 13.7

At  D 0 we have y.x; 0/ D

At  D 0 we have

1 2

x x 1 32   10 1 5 D 2 16 32 16     5 15 60 1 2 D 162 16 8 32

y .x; 0/ D y .x; 0/ D y .x; 0/ D

x0

105 : 4096

x 00 x

1 1 5 1  C  32 100 256 2  1002 105 1 C   4096 6  1003  0:49968847 1 2

with error less than 10

8

C

2y y

x y

00

xD1

in magnitude.

C e C e

For  D D D

2y 0

D

y0

D

2y 00

D

C

C

y

00

 e

3 0:

xD1 yD1

0

x x0

C

2y y0

x 00 x 00

C

2y 00 y 00

C C

e e

x

e e

y

2e 2e

x 0

y

x y0

C C

x 0

y

x y0

e e

x y

D D

D

D D

 3 )xDyD1 0

19 > 1 = 0 e ) x D e 1> ; y0 D 0 e 2 ) 2 00 00 e2 ) x D y D 2 : 3e 0

2 C ; 3e 2

yD1

2 C : 3e 2

1 we have 100

Thus 0

2y y

Thus

29. Let x./ and y./ be the solution of x x

C

x0

1 we have For  D 100 yD

(PAGE 802)

1 1 C C  100e 30; 000e 2 1 C : 30; 000e 2

0 0

.x 0 /2 .y 0 /2

Section 13.7 Newton’s Method

e e

x 00

y

x y 00

D D

0 0:

(page 802)

For each of Exercises 1–6, and 9, we sketch the graphs of the two given equations, f .x; y/ D 0 and g.x; y/ D 0, and use their intersections to make initial guesses x0 and y0 for the solutions. These guesses are then refined using the formulas xnC1 D xn

fg2 f 1 g2

ˇ gf2 ˇˇ ; g1 f2 ˇ.xn ;yn /

ynC1 D yn

f1 g f 1 g2

ˇ g1 f ˇˇ : g1 f2 ˇ.xn ;yn /

NOTE: The numerical values in the tables below were obtained by programming a microcomputer to calculate the iterations of the above formulas. In most cases the computer was using more significant digits than appear in the tables, and did not truncate the values obtained at one step before using them to calculate the next step. If you use a calculator, and use the numbers as quoted on one line of a table to calculate the numbers on the next line, your results may differ slightly (in the last one or two decimal places). 1.

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521

lOMoARcPSD|6566483

SECTION 13.7 (PAGE 802)

ADAMS and ESSEX: CALCULUS 9

y yDe x

xDsin y x

Fig. 13.7-1 f .x; y/ D y g.x; y/ D x

f1 .x; y/ D e x f2 .x; y/ D 1

ex sin y

We start with x0 D 0:9, y0 D 2:0. n 0 1 2 3 4

xn

g1 .x; y/ D 1 . g2 .x; y/ D cos y yn

0:9000000 0:8100766 0:7972153 0:7971049 0:7971049

f .xn ; yn /

2:0000000 2:2384273 2:2191669 2:2191071 2:2191071

Thus x D 0:7971049, y D 2:2191071.

0:4596031 0:0096529 0:0001851 0:0000000 0:0000000

g.xn ; yn / 0:0092974 0:0247861 0:0001464 0:0000000 0:0000000

y

2.

x 2 Cy 2 D1 yDe x

x

f .x; y/ D x 2 C y 2 g.x; y/ D y e x

f1 .x; y/ D 2x f2 .x; y/ D 2y

1

Fig. 13.7-2 g1 .x; y/ D e x . g2 .x; y/ D 1

Evidently one solution is x D 0, y D 1. The second solution is near . 1; 0/. We try x0 D 0:9, y0 D 0:2. n xn yn f .xn ; yn / g.xn ; yn / 0 1 2 3 4

0:9000000 0:9411465 0:9170683 0:9165628 0:9165626

0:2000000 0:3898407 0:3995751 0:3998911 0:3998913

0:1500000 0:0377325 0:0006745 0:0000004 0:0000000

The second solution is x D 0:9165626, y D 0:3998913.

522

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0:2065697 0:0003395 0:0001140 0:0000001 0:0000000

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 13.7

(PAGE 802)

3. y 4

x 4 Cy 2 D16

xyD1 x

2

Fig. 13.7-3

f .x; y/ D x 4 C y 2 g.x; y/ D xy 1

f1 .x; y/ D 4x 3 f2 .x; y/ D 2y

16

g1 .x; y/ D y . g2 .x; y/ D x

There are four solutions as shown in the figure. We will find the two in the first quadrant; the other two are the negatives of these by symmetry. The first quadrant solutions appear to be near .1:9; 0:5/ and .0:25; 3:9/. n xn yn f .xn ; yn / g.xn ; yn /

0 1 2 3 4

n

0 1 2 3

1:9000000 1:9990542 1:9921153 1:9920783 1:9920783

xn

0:5000000 0:5002489 0:5019730 0:5019883 0:5019883

yn

0:2500000 0:2499499 0:2500305 0:2500305

3:9000000 4:0007817 3:9995117 3:9995115

2:7179000 0:2200049 0:0011548 0:0000000 0:0000000

f .xn ; yn /

0:7860937 0:0101569 0:0000016 0:0000000

0:0500000 0:0000247 0:0000120 0:0000000 0:0000000

g.xn ; yn /

0:0250000 0:0000050 0:0000001 0:0000000

The four solutions are x D ˙1:9920783, ˙y D 0:5019883, and x D ˙0:2500305, y D ˙3:9995115.

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523

lOMoARcPSD|6566483

SECTION 13.7 (PAGE 802)

ADAMS and ESSEX: CALCULUS 9

4. y x.1Cy 2 /D1 2

y.1Cx 2 /D2

1 x

2

f .x; y/ D x.1 C y / 2

g.x; y/ D y.1 C x /

f1 .x; y/ D 1 C y f2 .x; y/ D 2xy

1 2

Fig. 13.7-4 g1 .x; y/ D 2xy

2

g2 .x; y/ D 1 C x

The solution appears to be near x D 0:2, y D 1:8. n xn 0 1 2 3

yn

0:2000000 0:2169408 0:2148268 0:2148292

. 2

f .xn ; yn /

1:8000000 1:9113487 1:9117785 1:9117688

0:1520000 0:0094806 0:0000034 0:0000000

g.xn ; yn / 0:1280000 0:0013031 0:0000081 0:0000000

The solution is x D 0:2148292, y D 1:9117688. 5. y yDsin x

1

1 x

1

x 2 C.yC1/2 D2

Fig. 13.7-5 f .x; y/ D y

sin x 2

2

g.x; y/ D x C .y C 1/

2

f1 .x; y/ D cos x f2 .x; y/ D 1

Solutions appear to be near .0:5; 0:3/ and . 1:5; 1/. n xn 0 1 2 3 4

524

0:5000000 0:3761299 0:3727877 0:3727731 0:3727731

g1 .x; y/ D 2x . g2 .x; y/ D 2.y C 1/ yn

0:3000000 0:3707193 0:3642151 0:3641995 0:3641995

f .xn ; yn / 0:1794255 0:0033956 0:0000020 0:0000000 0:0000000

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g.xn ; yn / 0:0600000 0:0203450 0:0000535 0:0000000 0:0000000

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

n

SECTION 13.7

xn

0 1 2 3 4

yn

1:5000000 1:4166667 1:4141680 1:4141606 1:4141606

f .xn ; yn /

1:0000000 0:9916002 0:9877619 0:9877577 0:9877577

g.xn ; yn /

0:0025050 0:0034547 0:0000031 0:0000000 0:0000000

The solutions are x D 0:3727731, y D 0:3641995, and x D 1:4141606, y D

(PAGE 802)

0:2500000 0:0070150 0:0000210 0:0000000 0:0000000

0:9877577.

6. y

.=2;/

y 2 Dx 3

sin x C sin y D 1 .;=2/

=2

x

=2

Fig. 13.7-6 f .x; y/ D sin x C sin y g.x; y/ D y 2

1

x3

f1 .x; y/ D cos x f2 .x; y/ D cos y

g1 .x; y/ D 3x 2 . g2 .x; y/ D 2y

There are infinitely many solutions for the given pair of equations, since the level curve of f .x; y/ D 0 is repeated periodically throughout the plane. We will find the two solutions closest to the origin in the first quadrant. From the figure, it appears that these solutions are near .0:6; 0:4/ and .2; 3/. n xn yn f .xn ; yn / g.xn ; yn / 0 1 2 3 4 n

0:6000000 0:5910405 0:5931130 0:5931105 0:5931105 xn

0:4000000 0:4579047 0:4567721 0:4567761 0:4567761 yn

0:0459392 0:0007050 0:0000015 0:0000000 0:0000000 f .xn ; yn /

0:0560000 0:0032092 0:0000063 0:0000000 0:0000000 g.xn ; yn /

0 1 2 3 4

2:0000000 2:0899016 2:0854887 2:0854779 2:0854779

3:0000000 3:0131366 3:0116804 3:0116770 3:0116770

0:0504174 0:0036336 0:0000086 0:0000000 0:0000000

1:0000000 0:0490479 0:0001199 0:0000000 0:0000000

The solutions are x D 0:5931105, y D 0:4567761, and x D 2:0854779, y D 3:0116770. 7. By analogy with the two-dimensional case, the Newton’s Method iteration formulas are ˇ ˇ ˇ ˇ ˇ f f 2 f 3 ˇˇ ˇ f 1 f f 3 ˇˇ ˇ ˇ ˇ ˇˇ ˇ 1 ˇ 1 ˇ g g2 g3 ˇˇˇˇ g1 g g3 ˇˇˇˇ ynC1 D yn xnC1 D xn ˇ ˇ  ˇ h h h ˇ .xn ;yn ;zn /  ˇh h h3 ˇ .xn ;yn ;zn / 2 3 1 ˇ ˇ ˇ ˇ ˇ f f 2 f ˇˇ ˇ f 1 f 2 f 3 ˇˇ ˇˇ ˇˇ ˇ 1 ˇˇ 1 g1 g2 g ˇˇˇˇ znC1 D zn where  D ˇˇ g1 g2 g3 ˇˇˇˇ ˇ  ˇh h ˇ h1 h2 h3 ˇ .xn ;yn ;zn / h ˇ .xn ;yn ;zn / 1 2 Copyright © 2018 Pearson Canada Inc. Downloaded by ted cage ([email protected])

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SECTION 13.7 (PAGE 802)

8.

f .x; y; z/ D y 2 C z 2 f1 .x; y; z/ D 0 f2 .x; y; z/ D 2y f3 .x; y; z/ D 2z

3

It is easily seen that the system

ADAMS and ESSEX: CALCULUS 9

g.x; y; z/ D x 2 C z 2 g1 .x; y; z/ D 2x g2 .x; y; z/ D 0 g3 .x; y; z/ D 2z

h.x; y; z/ D x 2 z h1 .x; y; z/ D 2x h2 .x; y; z/ D 0 h3 .x; y; z/ D 1

2

f .x; y; z/ D 0; g.x; y; z/ D 0; h.x; y; z/ D 0 p 2. Let us start at the “guess” x0 D y0 D z0 D 2. zn f .xn ; yn ; zn / g.xn ; yn ; zn /

has first-quadrant solution x D z D 1, y D n xn yn 0 1 2 3 4 5 9.

f .x; y/ D y g.x; y/ D y

2:0000000 1:3000000 1:0391403 1:0007592 1:0000003 1:0000000 x2

2:0000000 1:5500000 1:4239564 1:4142630 1:4142136 1:4142136

5:0000000 0:8425000 0:0513195 0:0002313 0:0000000 0:0000000

6:0000000 1:1300000 0:1034803 0:0016104 0:0000006 0:0000000

2:0000000 0:4900000 0:0680478 0:0014731 0:0000006 0:0000000

g1 .x; y/ D 3x 2 g2 .x; y/ D 1

f1 .x; y/ D 2x f2 .x; y/ D 1

x3

2:0000000 1:2000000 1:0117647 1:0000458 1:0000000 1:0000000

h.xn ; yn ; zn /

y

.1;1/ yDx 2 yDx 3 x

n 0 1 2 3 4 5 :: :

xn 0:1000000 0:0470588 0:0229337 0:0113307 0:0056327 0:0028083

yn 0:1000000 0:0005882 0:0000561 0:0000062 0:0000007 0:0000001

Fig. 13.7-9 n 0 1 2 3 4

xn 0:9000000 1:0285714 1:0015038 1:0000045 1:0000000

yn 0:9000000 1:0414286 1:0022771 1:0000068 1:0000000

15 0:0000027 0:0000000 16 0:0000014 0:0000000 17 0:0000007 0:0000000 18 0:0000003 0:0000000 Eighteen iterations were needed to obtain the solution x D y D 0 correct to six decimal places, starting from x D y D 0:1. This slow convergence is due to the fact that the curves y D x 2 and y D x 3 are tangent at .0; 0/. Only four iterations were needed to obtain the solution x D y D 1 starting from x D y D 0, because, although the angle between the curves is small at .1; 1/, it is not 0. The curves are not tangent there.

526

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 13.8

Section 13.8 Calculations with Maple (page 807) 1.

2.

(PAGE 807)

The equation y D sin z can be used to reduce the given system of three equations in three variables to a system of 2 equations in two variables:

The equation z D xy can be used to reduce the given system of three equations in three variables to a system of 2 equations in two variables:

x 4 C sin2 z C z 2 D 1

z C z 3 C z 4 D x C sin z:

The first equation can only be satisfied by points .x; z/ satisfying jxj  1 and jzj  1.

x 2 C y 2 C x 2y 2 D 1 2

6x y D 1:

> Digits := 6:

The first equation can only be satisfied by points .x; y/ satisfying jxj  1 and jyj  1.

> eqns := {x^4+(sin(z))^2+z^2=1,

> Digits := 6:

> z+z^3+z^ 4=x+sin(z)}:

> eqns := {x^2+y^2+(x*y)^2=1, 6*x^2*y=1}:

We use plots[implicitplot] to locate suitable starting points for fsolve. > plots[implicitplot](eqns,x=-1..1, z=-1..1);

We use plots[implicitplot] to locate suitable starting points for fsolve. > plots[implicitplot](eqns,x=-1..1, y=-1..1);

The resulting plot shows two roots in the xz-plane, one near .0:6; 0:7/ and the other near . 0:2; 0:7/. We use fsolve to find them more precisely, and we then calculate the corresponding values for y by substitution.

The resulting plot (omitted here) shows four roots; two in the first quadrant near .:9; :2/ and .:5; :8/, and two more that are reflections of these in the y-axis. We use fsolve to find the two first-quadrant roots and calculate the corresponding values for z by substitution.

> vars := {x=0.6, z=0.7}: > xz := fsolve(eqns,vars);

> vars := {x=0.9, y=0.2}:

> y=evalf(subs(xz,sin(z))); xy WD fz D 0:686259; x D 0:597601g y D 0:633648

> xy := fsolve(eqns,vars); > z=evalf(subs(xy,x*y));

> vars := {x=-0.2, z=-0.7}:

xy WD fx D 0:968971; y D 0:177512g z D 0:172004

> xy := fsolve(eqns,vars);

> vars := {x=0.5, y=0.8}:

> y=evalf(subs(xz,sin(z))); xy WD fz D 0:738742; x D y D 0:673358

> xy := fsolve(eqns,vars); > z=evalf(subs(xy,x*y));

The two solutions are .x; y; z/ D .0:59760; 0:63365; 0:68626/ and .x; y; z/ D . 0:17071; 0:67336; 0:73874/, each rounded to five figures.

xy WD fy D 0:812044; x D 0:453038g z D 0:367887 The four solutions are .x; y; z/ D .˙0:96897; 0:17751; ˙0:17200/ and .x; y; z/ D .˙0:45304; 81204; ˙0:36789/, rounded to five figures.

0:170713g

3.

First define the expression f : > f := (x*y-x-2*y)/(1+x^2+y^2)^2:

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SECTION 13.8 (PAGE 807)

ADAMS and ESSEX: CALCULUS 9

Since h D 1 at .0; 0; 0/ and h ! 1 as x 2 C y 2 C z 2 increases, the maximum value of g will be near .0; 0; 0/.

Because the numerator grows much more slowly than the denominator for large x 2 C y 2 , global max and min values will be near the origin. We plot contours of f on, say, the square jxj  2, jyj  2. > contourplot(f(x,y), x=-2..2, > y=-2..2, contours=16);

We can try various choices of starting points including .0; 0; 0/ itself. It turns out they all lead to the same critical point:

The resulting plot (which we omit here) indicates the only likely critical points are near . 0:3; 0:6/ and .0:2; 0:6/. We determine them using fsolve and use substitution to evaluate f .

> eqns := {diff(h,x),diff(h,y),diff(h,z)}: > vars := x=0,y=0,z=0: > cp := fsolve(eqns,vars); val = evalf(subs(cp,h));

> Digits := 6:

cp WD fx D

> eqns := {diff(f,x), diff(f,y)}:

:28429; y D :372953; z D 0:265109g val = 1:91367

The absolute maximum value of h is 1:91367 (to five decimal places). > vars := {x=-0.3, y=-0.6}: 5. > cp := fsolve(eqns,vars); > val=evalf(subs(cp,f)); cp WD fx D :338532; y D :520621g val = 0:810414 > vars := {x=0.2, y=0.6}:

> Digits := 6:

> cp := fsolve(eqns,vars);

> f := x^2 + y^2 + z^2

> val=evalf(subs(cp,f));

> +0.2*x*y-0.3*x*z+4*x-y: > eqns := {diff(f,x),diff(f,y),diff(f,z)}: > vars := x=0,y=0,z=0: > cp := fsolve(eqns,vars); val = evalf(subs(cp,f));

cp WD fx D 0:133192; y D 0:536823g val = :665721 There are only two critical points and the values of f at them have opposite sign. Since f ! 0 as x 2 C y 2 ! 1, f has absolute maximum value 0:81041 at . 0:33853; 0:52062/ and absolute minimum value 0:66572 at .0:13319; 0:53682/, all numerical values rounded to five figures. 4.

Because of the small coefficients on the xy and xz terms and the fact that without them f would certainly have a minimum value near the origin, we can use fsolve starting with various points near the origin. It turns out they all lead to only one critical point.

cp WD fx D

To confirm that this CP does give a local minimum, you can calculate VectorCalculus[Hessian](f,[x,y,z]) and then evalf the result of LinearAlgebra[Eigenvalues](subs(cp,%)) and observe that all three eigenvalues are positive.

We begin with > Digits := 6: > f := 1 - 10*x^4 - 8*y^4 - 7*z^4:

The minimum value of f is

> g := y*z - x*y*z - x - 2*y + z: 6. > h := f + g:

528

2:11886; y D 0:711886; z D :317829g val = 4:59368

4:59368.

First define the function: > f := (x+1.1y-0.9z+1)/(1+x^2+y^2);

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 13.9

Since f .x; y; z/ ! 0 as x 2 Cy 2 Cz 2 ! 1 we expect f to have maximum and minimum values in some neighbourhood of the origin. If the numerator were instead x C y z, we would expect the extreme values to occur along the line x D y D z by symmetry. Accordingly, we use starting points along this line.

By additivity the entropy of the combined system is SD

> Digits := 6: > f := (x+1.1*y-0.9*z+1)/(1+x^2+y^2+z^2):

2.

> eqns := {diff(f,x),diff(f,y),diff(f,z)}: > vars := x=1,y=1,z=-1: > cp := fsolve(eqns,vars); val = evalf(subs(cp,f));

If the expression is universal, it must apply to each of n > 1 independent subsystems of a larger combined system, each denoted by index i, Si D k ln Wi C C:

i D1

Wi C nC D k ln W C nC:

i D1

@L D k .ln pi @pi

1/ C :

It follows that ln pi D 1 C .=k/ for each i and so all the pi are equal. The constraint equation then gives pi D 1=n for each i; there is only one critical point. Now  @2 L 0 if ¤ j D k n < 0 if i D j . @pi @pj

> vars := x=-0.5,y=-0.5,z=+0.5: > cp := fsolve(eqns,vars); val = evalf(subs(cp,f));

1.

n Y

We must require nC D C to have the same constant in the composite system. Thus C.n 1/ D 0. Since n > 1, C D 0. Pn To Pnextrenize S D k i D1 pi ln pi subject to i D1 pi D 1 we look for critical points of ! ! n n X X pi ln pi C  1 : pi LD k

0D

cp WD fy D 0:366057; z D :299501; x D 0:332779g val = 1:50250

Section 13.9 Entropy in Statistical Mechanics and Information Theory (page 812)

i D1

Si D k ln

At any such critical point we will have

> vars := x=0.5,y=0.5,z=-0.5: > cp := fsolve(eqns,vars); val = evalf(subs(cp,f));

The eigenvalues of the Hessian matrix of f at each of these critical points confirms that the first is a local maximum and gives f its absolute maximum value 1:50250 and the second is a local minimum so the absolute minimum value of f is 0:502494.

n X

i D1

This attempt fails; fsolve cannot locate a solution. We try a guess closer to the origin.

cp WD fx D :995031; z D 0:895528; y D 1:09453g val = :502494

(PAGE 812)

3.

The Hessian matrix for L is diagonal, has (equal) negative eigenvalues, and is negative definite on Rn , so the critical point must provide a local maximum value forPS by Theorem 5 in Section 13.4. Since S D k niD1 ..ln n/=n/ > 0 and S ! 0 as points .p1 ; p2 ; : : : ; pn / approach the P boundary of the region of Rn defined by pi  0, niD1 D 1, the local minimum must, in fact be absolute. P P Since IiD1 pi D 1 and jJD1 qj D 1, we have H1 C H2 D D D

I X

pi log2 pi

i D1

J X

j D1

qj

I X

J X

qj log2 qj

j D1

pi log2 pi

i D1

i D1

I J X X

I X

pi

J X

qj log2 qj

j D1

pi qj log2 pi qj :

j D1 i D1

The probabilities of the combination of independent sub systems are given as the product pi qj D k : Each term can be uniquely accounted for with a single index k D i C I.j 1/ between 1 and K D IJ . Thus K X k log2 k ; D H1 C H2 D kD1

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SECTION 13.9 (PAGE 812)

and

PI

i D1

K X

kD1

4.

pi D 1 and

k D

J I X X

i D1 j D1

ADAMS and ESSEX: CALCULUS 9

PJ

D 1 also imply that

j D1 qj

pi qj D

I X

pi

J X

j D1

i D1



Z

qj D 1:

2 3 3 1 C C C 2 4 8 8



NŠ S D k ln n1 Šn2 Š : : : nM Š M X .ni ln ni  k N ln N N M X

i D1

!

A e N

i D1

L D N ln N

!

and

M X i D1

ni ln ni

i D1

@L D @ni

=2 D

1 p e  2

.u /2 =2 2

D f .u/

2 D

1 Bm

and

1 A p D : N  2

It follows that

ni i D E

˛

M X

ni

i D1

ln ni

1

˛

.1C˛/Cˇ i

ˇ

M X

p N N Bm AD p D p :  2 2



(b) As shown in Section 7.8, the expectation of U 2 for such a normally distributed random variable with mean  D 0 and variance  2 is Z

ni i :

i D1

ˇi ;

D Ae Bi , so that we have ni D e where A D e .1C˛/ and B D ˇ. The values of the Lagrange multipliers ˛ and ˇ, (or, equivalently, the two constants A and B) are determined by the two constraint equations.

530

.u /2 =2 2

ni ln ni :

i D1

For a critical point we require 0D

Bmu2

ni /

we look for a critical point of the Lagrange function M X

1 p e  2

provided  D 0 and

For maximum S (or equivalently S=k subject to the constraints ni D N

p.u/ du D 1

is the density function of a normally distributed random variable with mean  and variance  2 . Evidently, p.u/ D





M X

1

f .u/ D

D 0:875

Using the Modified Stirling approximation, we have

D k N ln N

1

and p.u/ is a probability density function. By Definition 7 in Section 7.8,

An optimal encoding scheme that achieves this is a ! 0, b ! 11, c ! 101, d ! 100. 5.

(a) Z Since n.u/  0 for all real u and 1 n.u/ du D N , p.u/ D n.u/=N satisfies 1

The best compression is 1 2

6.

1 1

u2 p.u/ du D  2 :

Accordingly, the expected value of the part of the kinetic energy of a particle due to motion in 1 1 the x-direction is m 2 D . By symme2 2B try the same result will obtain for the expected value of the part of the kinetic energy due to motion in the other two coordinate directions, so the expected value of the total kinetic energy of 3 the particle is , and that of all N particles is 2B 3N . ED 2B

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INSTRUCTOR’S SOLUTIONS MANUAL

REVIEW EXERCISES 13

(c) Comparing the result of part (b) with the known 3 1 formula E D N kT , we see that B D . kT r2 m and the probability density Thus A D N 2kT for one component of velocity is p.u/ D

 m  21 e 2kT

mu2 2kT

CP .0; 0/ .0; 1/ . 2; 0/ . 23 ; 31 /

3.

p.v/ D p.v1 ; v2 ; v3 / D p.v1 /p.v2 /p.v3 /  m  32 m.v2 Cv2 Cv2 / 3 1 2 2kT D e 2kT  m  32 2 e mjvj =2kT : D 2kT

This is the classical Maxwell-Boltzmann distribution for an ideal gas. Review Exercises 13 (page 813) f .x; y/ D xye

xCy

xy/e

xCy

f2 .x; y/ D .x C xy/e

xCy

f1 .x; y/ D .y

A D f11 D . 2y C xy/e

B D f12 D .1

xCy

D y.1

x/e

D x.1 C y/e

xCy xCy

2.

A 0 e 2

B 1 0

f .x; y/ D x 2 y

f1 .x; y/ D 2xy

C 0 e 2

C 0 0 8

2 3

2 3

8 3

B2

AC 4 4 4 4 3

class saddle saddle saddle loc. min

4 9 1 C C x y 4 x y 1 9 f1 .x; y/ D C 2 x .4 x y/2 9 4 C f2 .x; y/ D 2 y .4 x y/2 18 2 A D f11 D 3 C x .4 x y/3 18 B D f12 D .4 x y/3 8 18 C D f22 D 3 C : y .4 x y/3 2 2 For CP: y D 4x so that y D ˙2x. If y D 2x, then 9x 2 D .4 3x/2 , from which x D 2=3, y D 4=3. If y D 2x, then 9x 2 D .4 C x/2 , from which x D 1 or x D 2. The CPs are .2=3; 4=3/, . 1; 2/, and .2; 4/. f .x; y/ D

xCy

xy/e

xCy

C D f22 D .2x C xy/e xCy : For CP: either y D 0 or x D 1, and either x D 0 or y D 1. The CPs are .0; 0/ and .1; 1/. CP .0; 0/ .1; 1/

B 2 2 2

:

The probability density for the other two components of the velocity are the same, and since the three components are independent, the probability density for the three components of the velocity v D v1 i C v2 j C v3 k is

1.

A 0 2 0

(PAGE 813)

B2

AC 1 e

2xy 2 C 2xy

4

2y 2 C 2y D 2y.x

CP

A

B

C

. 1; 2/ .2; 4/ . 23 ; 34 /

4 3 1 3

2 3 1 12 9 4

5 3 1 24 45 8

9

AC

B2

8 3 1 48 729 16

class saddle saddle loc. min

class saddle loc. min

y C 1/

f2 .x; y/ D x 2 4xy C 2x D x.x 4y C 2/ A D f11 D 2y B D f12 D 2x 4y C 2 C D f22 D 4x: For CP: either y D 0 or x y C 1 D 0, and either x D 0 or x 4y C 2 D 0. The CPs are .0; 0/, .0; 1/, . 2; 0/, and . 2=3; 1=3/.

4.

f .x; y/ D x 2 y.2

f1 .x; y/ D 4xy f2 .x; y/ D 2x

2

3x 2 y x

A D f11 D 4y

B D f12 D 4x

x 3

6xy 3x

2

y/ D 2x 2 y

x 3y

2xy 2 D xy.4

2

2

2x y D x .2 2y

x

x 2y 2 3x

2y/

2y/

2

4xy

2

C D f22 D 2x : .0; y/ is a CP for any y. If x ¤ 0 but y D 0, then x D 2 from the second equation. Thus .2; 0/ is a CP.

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ADAMS and ESSEX: CALCULUS 9

If neither x nor y is 0, then x C 2y D 2 and 3x C 2y D 4, so that x D 1 and y D 1=2. The third CP is .1; 1=2/. CP .0; y/ .2; 0/ .1; 12 /

A 4y

2y

2

0 3 2

B

C

0 4 1

0 8 2

B2

AC

0 16 2

8.

f1 .x; y/ D e

class ? saddle loc. max

6.

f .x; y; z/ D g.s/ D s C .1=s/, where s D x 2 C y 2 C z 2 . Since g.s/ ! 1 as s ! 1 or s ! 0C, g must have a minimum value at a critical point in .0; 1/. For CP: 0 D g 0 .s/ D 1 .1=s 2 /, that is, s D 1. g.1/ D 2. The minimum value of f is 2, and is assumed at every point of the sphere x 2 C y 2 C z 2 D 1. x 2 C y 2 C z 2 xy xz yz 1 D .x 2 2xy C y 2 / C .x 2 2xz C z 2 / 2  C .y 2 2yz C z 2 /  1 D .x y/2 C .x z/2 C .y z/2  0: 2 The minimum value, 0, is assumed at the origin and at all points of the line x D y D z.

7. f .x; y/ lim

x 2 Cy 2 !1

2

f . 1; 1/ < 0, f must have maximum and minimum values and these must occur at critical points. For CP: 0 D f1 D e 0 D f2 D e

x 2 4y 2 x 2 4y 2

.y .x

2x 2 y/ D e

8xy 2 / D e

x 2 4y 2 x 2 4y 2

The CPs are .0; 0/ (where f D 0), ˙

y.1

2x 2 /

x.1

8y 2 /:

1 1 p ; p  2 2 2



1 (where f D 1=4e), and ˙ p1 ; p (where 2 2 2 f D 1=4e). Thus f has maximum value 1=4e and minimum value 1=4e.

532

x 2 Cy 2 2

x 2 Cy 2

2x.4

2

4x 2 C y 2 /

2

a) Since f .0; y/ D y 2 e y ! 1 as y ! ˙1, and since f .x; x/ D 3x 2 e 0 D 3x 2 ! 1 as x ! ˙1, f does not have a minimum or a maximum value on the xy-plane. 2

b) On y D 3x, f .x; 3x/ D 5x 2 e 8x ! 1 as x ! 1. Thus f can have no minimum value on the wedge 0  y  3x. However, as noted in (a), f .x; x/ ! 1 as x ! 1. Since .x; x/ is in the wedge for x > 0, f cannot have a maximum value on the wedge either. 9.

Let the three pieces of wire have lengths x, y, and L x y cm, respectively. The sum of areas of the squares is SD

1 2 x C y 2 C .L 16

x

 y/2 ;

for which we must find extreme values over the triangle x  0, y  0, x C y  L. For critical points: 1 @S D x @x 8 @S 1 0D D y @y 8

0D

.L

x

.L

x

 y/

 y/ ;

from which we obtain x D y D L=3. This CP is inside the triangle, and S D L2 =48 at it. On the boundary segment x D 0, we have SD

2

D xye x 4y satisfies f .x; y/ D 0. Since f .1; 1/ > 0 and

y 2 /e

f2 .x; y/ D e x Cy . 2y/.1 4x 2 C y 2 /: f has CPs .0; 0/, .˙1; 0/. f .0; 0/ D 0. f .˙1; 0/ D 4=e.

The second derivative test is unable to classify the line of critical points along the y-axis. However, direct inspection of f .x; y/ shows that these are local minima if y.2 y/ > 0 (that is, if 0 < y < 2) and local maxima if y.2 y/ < 0 (that is, if y < 0 or y > 2). The points .0; 0/ and .0; 2/ are neither maxima nor minima, so they are saddle points. 5.

f .x; y/ D .4x 2

1 2 y C .L 16

 y/2 ;

.0  y  L/:

At y D 0 or y D L, we have S D L2 =16. For critical points 0D

1 dS D y dy 8

.L

 y/ ;

so y D L=2 and S D L2 =32. By symmetry the extreme values of S on the other two boundary segments are the same. Thus the minimum value of S is L2 =48, and corresponds to three equal squares. The maximum value of S is L2 =16, and corresponds to using the whole wire for one square.

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INSTRUCTOR’S SOLUTIONS MANUAL

10.

REVIEW EXERCISES 13

Let the length, width, and height of the box be x, y, and z in, respectively. Then the girth is g D 2x C 2y. We require g C z  120 in. The volume V D xyz of the box will be maximized under the constraint 2x C 2y C z D 120, so we look for CPs of L D xyz C .2x C 2y C z

12.

120/:

For CPs:

The ellipsoid .x=a/2 C .y=b/2 C .z=c/2 D 1 contains the rectangle 1  x  1, 2  y  2, 3  z  3, provided .1=a2 / C .4=b 2 / C .9=c/2 D 1. The volume of the ellipsoid is V D 4abc=3. We minimize V by looking for critical points of   4 1 4 9 LD abc C  C C 1 : 3 a2 b2 c2 For CPs:

@L @x @L 0D @y @L 0D @z @L 0D @ 0D

D yz C 2

(A)

D xz C 2

(B)

D xy C 

(C)

D 2x C 2y C z

120:

@L @a @L 0D @b @L 0D @c @L 0D @ 0D

(D)

V D .20/.20/.40/ D 16; 000 in3 ;

V D

or, about 9.26 cubic feet. The ellipse .x=a/2 C .y=b/2 D 1 contains the rectangle 1  x  1, 2  y  2, if .1=a2 /C.4=b 2 / D 1. The area of the ellipse is A D ab. We minimize A by looking for critical points of 

1 4 L D ab C  C 2 2 a b

 1 :

For CPs: @L 2 D b @a a3 @L 8 D a 0D @b b3 1 4 @L D 2C 2 0D @ a b

0D

(A)

(C)

Multiplying (A) by a and (B) by b, we obtain 2=a2 D 8=b 2 , so that either  D 0 or b D 2a. Now  D 0 implies b D 0, which is inconsistent with 2 (C). If pb D 2a, then (C) implies that 2=a D 1, so a D 2. The smallest area of the ellipse is V D 4 square units.

(A) (B) (C) 1:

(D)

13.

p p p 4 p . 3/.2 3/.3 3/ D 24 3 cubic units. 3

The box 1  x  1, 2  y  2, 0  z  2 is contained in the region   x2 y2 0za 1 b2 c2 provided that .2=a/ C .1=b 2 / C .4=c 2 / D 1. The volume of the region would normally be calculated via a “double integral” which we have not yet encountered. (See Chapter 5.) It can also be done directly by slicing. A horizontal plane at height z (where 0  z  a) intersects the region in an elliptic disk bounded by the ellipse y2 x2 C D1 b2 c2

(B) 1:

4 2 bc 3 a3 4 8 D ac 3 b3 4 18 D ab 3 c3 1 4 9 D 2C 2C 2 a b c D

Multiplying (A) by a, (B) by b, and (C) by c, we obtain 2=a2 D 8=b 2 D 18=c 2 , so that either  D 0 or b D 2a, c D 3a. Now  D 0 implies bc D 0, which is inconsistent with (D). If b D 2a and cpD 3a, then (D) implies that 3=a2 D 1, so a D 3. The smallest volume of the ellipsoid is

Comparing (A), (B), and (C), we see that x D y D z=2. Then (D) implies that 3z D 120, so z D 40 and x D y D 20 in. The largest box has volume

11.

(PAGE 813)

The area of this disk is  r  r z A.z/ D  b 1 c 1 a

z : a z a



 D bc 1

Thus the region has volume Z a abc z : dz D V D bc 1 a 2 0

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z : a

533

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REVIEW EXERCISES 13 (PAGE 813)

ADAMS and ESSEX: CALCULUS 9

Thus we look for critical points of

For maximum A, we look for critical points:

 abc 2 1 4 LD C C 2C 2 2 a b c

 1 :

0D

For critical points: 0D 0D 0D 0D

@L @a @L @b @L @c @L @

D D D D

 2 bc 2 a2  2 ac 2 b3  8 ab 2 c3 2 1 4 C 2C 2 a b c

0

@A 1 D @L @x 2 C

(A) (B)

D

(C) 0D

(D)

1:

Multiplying (A) by a, (B) by b, and (C) by c, we obtain 2=a D 2=b 2 D 8=c 2 , so that either  D 0 or b 2 D a, c 2 D 4a. Now  D 0 implies bc D 0, which is inconsistent with (D). If b 2 D a and c 2 D 4a, then (D) implies that 4=a D 1, so a D 4. The smallest volume of the region is V D .4/.2/.4/=2 D 16 cubic units.

0

xB B 1 2@ x

2

z2

x

r

2z 2 zC r 4

x2

z2

x A 4 1

C C 2A

x 4

4 z2

1

x2 4

xz @A D xC r : @z x2 2 2 z 4

(A)

(B)

Now (B) p implies that either x D 0 or z D 2 z 2 .x 2 =4/. But x D 0 gives zero area rather than maximum area, so the second p alternative must hold, and it implies that z D x= 3. Then (A) gives   x 1 L D 1C p xC p ; 2 3 2 3 p from which we obtain x D L=.2 C 3/. The maximum area of the window is, therefore,

14.

z

ˇ ˇ Aˇˇ

z

y

L 2

2z C

x

s

p L= p3 Lp ; zD xD 2C 3 2C 3

D

1 L2 p 4 2C 3

 0:0670L2 sq. units:

y

15. x

If $1; 000x widgets per month are manufactured and sold for $y per widget, then the monthly profit is $1; 000P , where

Fig. R-13-14 P D xy

The area of the window is x A D xy C 2

s

x2 ; 4

z2

or, since x C 2y C 2z D L, 0

x A D @L 2 534

x

2z C

s

z2

x 2y 3 27

x:

We are required to maximize P over the rectangular region R satisfying 0  x  3 and 0  y  2. First look for critical points: 1

x2 A : 4

@P Dy @x @P 0D Dx @y 0D

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2xy 3 1 27 x 2y 2 : 9

(A) (B)

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INSTRUCTOR’S SOLUTIONS MANUAL

CHALLENGING PROBLEMS 13

(B) implies that x D 0, which yields zero profit, or xy 2 D 9, which, when substituted into (A), gives y D 3 and x D 1. Unfortunately, the critical point .1; 3/ lies outside of R. Therefore the maximum P must occur on the boundary of R. We consider all four boundary segments of R. On segment x D 0, we have P D 0. On segment y D 0, we have P D x  0. On segment x D 3, 0  y  2, we have P D 3y .y 3 =3/ 3, which has values P D 3 at y D 0 and P D 1=3 at y D 2. It also has a critical point given by dP D 3 y 2; dy p p so y D 3 and P D 2 3 3  0:4641. On segment y D 2, 0  x  3, we have P D x .8x 2 =27/, which has values P D 0 at x D 0 and P D 1=3 at x D 3. It also has a critical point given by 16x dP D1 ; 0D dx 27 so x D 27=16 and P D 27=32  0:84375. It appears that the greatest monthly profit corresponds to manufacturing 27; 000=16  1; 688 widgets/month and selling them for $2 each.

The second gives y .x; 0/ D 2xe y.x;0/ y .x; 0/ D 2x 2 e

18.

0D

16.

The envelope of y D .x c/3 C 3c is found by eliminating c from that equation and 0D

@ Œ.x @c

c/3 C 3c D 3.x

c/2 C 3: 2

This later equation implies that .x c/ D 1, so x c D ˙1. The envelope is y D .˙1/3 C3.x 1/, or y D 3x ˙2.

17. Look for a solution of y C xe y D of a Maclaurin series

2x in the form 2

y D y.x; / D y.x; 0/Cy .x; 0/C

 y .x; 0/C   : 2Š

Putting  D 0 in the given equation, we get y.x; 0/ D 2x. Now differentiate the given equation with respect to  twice: y C xe y C xe y y D 0

y C 2xe y y C xe y y2 C xe y y D 0:

y .x; 0/ D xe

D

xe

2x

:

4x

:

Thus y D 2x 2xe 2x C  2 x 2 e 4x C    : Z 1 tan 1 .xy/ dx a) G.y/ D x Z0 1 x 1 G 0 .y/ D dx Let u D xy x 1 C x 2y 2 0 du D y dx Z  1 1 du D for y > 0. D y 0 1 C u2 2y Z 1 tan 1 .x/ tan 1 x b) dx x 0 Z Z   ln    dy 0 D : D G./ G.1/ D G .y/ dy D 2 1 y 2 1 Challenging Problems 13 (page 813)

1.

To minimize Z " 

In D

f .x/



a0 2

n X

kD1

#2

.ak cos kx C bk sin kx/

dx

we choose ak and bk to satisfy @In @a0 " Z  D f .x/

0D



 D a0

Z

a0 2



f .x/ dx 

@In @am " Z  D 2 f .x/

n X

#

.ak cos kx C bk sin kx/ dx

kD1

0D



D 2am

Z

a0 2

cos mx dx  2

cos mx dx 

@In @bm " Z  D 2 f .x/

n X

kD1

Z

#

.ak cos kx C bk sin kx/



f .x/ cos mx dx 

0D



The first of these equations gives y.x;0/

(PAGE 813)

D 2bm

Z

a0 2

sin mx dx  2

sin mx dx 

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n X

kD1

Z

#

.ak cos kx C bk sin kx/



f .x/ sin mx dx: 

535

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CHALLENGING PROBLEMS 13 (PAGE 813)

ADAMS and ESSEX: CALCULUS 9

The simplifications in the integrals above resulted from the facts that for any integers k and m, Z



Z 

Z

Because of the properties of trigonometric integrals listed in the solution to Problem 1, !2 Z  n X a0 .ak cos kx C bk sin kx/ dx C 2 

cos kx cos mx dx D 0 unless k D m

  

kD1

sin kx sin mx dx D 0 unless k D m, and

D

Z

cos kx sin mx dx D 0:

 

cos2 mx dx D

Z

 

1  Z 1 bm D 

am D

2.





  

0 If f .x/ D x



f .x/ cos mx dx for 0  m  n, and

536

D

Z

a02

kD1 n X

2

C

.ak2 C bk2 /:

kD0

 

!#2 n a0 X C .ak cos kx C bk sin kx/ dx 2 kD1 ! n X 2 a02 C .ak2 C bk2 / f .x/ dx 2 2 kD0

n

f .x/ sin mx dx for 1  m  n: D for   x < 0 , then for 0  x  

Z  1  x dx D a0 D  0 2 Z 1  ak D x cos kx dx  0 U Dx dV D cos kx dx 1 d U D dx V D sin kx ˇ Z k    ˇ 1 D x sin kx ˇˇ sin kx dx k 0 0( 0 if k is even cos k 1 2 D D 2 if k is odd k k 2 Z  1 bk D x sin kx dx  0 U Dx dV D sin kx dx 1 d U D dx cos kx V D k ˇ Z    ˇ 1 D cos kx dx x cos kx ˇˇ k 0 0 . 1/kC1 : D k

.ak2 C bk2 /

Therefore Z " In D f .x/

In is minimized when Z

n X

kD0 ! n a0 X f .x/ C .ak cos kx C bk sin kx/ dx 2 

D sin2 mx dx D ;

2

C



Since Z

a02

3.

Z

X a02 .ak2 C bk2 / C C 2 kD0





2 f .x/ dx

! n X a02 .ak2 C bk2 / : C 2 kD0

In fact, it can be shown that In ! 0 as n ! 1. Z x ln.1 C tx/ Let I.x/ D dt. Then 1 C t2 0 Z x ln.1 C x 2 / t I 0 .x/ D C dt: 2 /.1 C tx/ 1 C x2 .1 C t 0 If we expand the latter integrand in partial fractions with respect to t, we obtain xCt x t D : .1 C t 2 /.1 C tx/ .1 C x 2 /.1 C t 2 / .1 C x 2 /.1 C tx/ Now we have ˇ Z x 2xtan 1 t C ln.1 C t 2 / ˇˇx .x C t/ dt D ˇ 2 2 2.1 C x 2 / 0 .1 C x /.1 C t / 0 2xtan 1 x C ln.1 C x 2 / D 2.1 C x 2 / 1 d D tan 1 x ln.1 C x 2 / 2 dx Z x Z x dt x dt x D 2 2 1 C x 0 1 C tx 0 .1 C x /.1 C tx/ Let u D 1 C tx du D x dt Z 1Cx 2 ln.1 C x 2 / du 1 D : D 1 C x2 1 u 1 C x2

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INSTRUCTOR’S SOLUTIONS MANUAL

CHALLENGING PROBLEMS 13

Thus ln.1 C x 2 / 1 d C tan 1 x ln.1 C x 2 / 2 1Cx 2 dx 1 d D tan 1 x ln.1 C x 2 /: 2 dx

ln.1 C x 2 / 1 C x2

I 0 .x/ D

1 tan 1 x ln.1 C x 2 / C C . Since 2 I.0/ D 0, we have C D 0, and Z x ln.1 C tx/ 1 dx D tan 1 x ln.1 C x 2 /: 2 1 C t 2 0

Therefore, I.x/ D

P1

D1

@S D cos 1 C cos 2 C cos 3 @x @S D sin 1 C sin 2 C sin 3 : 0D @y 0D

2

2 C 2.cos 1 cos 2 C sin 1 sin 2 / D 1;

1 D2

! where i is the angle between PPi and i. Similarly @Di =@y D sin i : To minimize S D D1 C D2 C D3 we look for critical points:

Thus cos 1 C cos 2 D cos 3 and sin 1 C sin 2 D sin 3 . Squaring and adding these two equations we get

4. y

(PAGE 813)

P

3 D3

P2 P3 x

Fig. C-13-4 If Di D jPPi j for i D 1; 2; 3, then Di2 D .x xi /2 C .y yi /2 @Di 2Di D 2.x xi / @x x xi @Di D D cos i @x Di

or cos.1 2 / D 1=2. Thus 1 2 D ˙2=3. Similarly 1 3 D 2 3 D ˙2=3. Thus P ! ! ! should be chosen so that PP1 , PP2 ,and PP3 make ı 120 angles with each other. This is possible only if all three angles of the triangle are less than 120ı . If the triangle has an angle of 120ı or more (say at P1 ), then P should be that point on the side P2 P3 such that PP1 ? P2 P3 .

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SECTION 14.1 (PAGE 820)

ADAMS and ESSEX: CALCULUS 9

CHAPTER 14. MULTIPLE INTEGRATION

Section 14.1 Double Integrals

1.

The solid is split by the vertical plane through the z-axis and the point .3; 2; 0/ into two pyramids, each with a trapezoidal base; one pyramid’s base is in the plane y D 0 and the other’s is in the plane z D 0. I is the sum of the volumes of these pyramids:

(page 820)

I D

f .x; y/ D 5

x y h R D 1  f .0; 1/ C f .0; 2/ C f .1; 1/ C f .1; 2/ i C f .2; 1/ C f .2; 2/

7.

D 4 C 3 C 3 C 2 C 2 C 1 D 15

2.

h R D 1  f .1; 1/ C f .1; 2/ C f .2; 1/ C f .2; 2/ i C f .3; 1/ C f .3; 2/ D3C2C2C1C1C0D9

3.

h R D 1  f .0; 0/ C f .0; 1/ C f .1; 0/ C f .1; 1/ i C f .2; 0/ C f .2; 1/ D 5 C 4 C 4 C 3 C 3 C 2 D 21

4.

8. 9.

J D

figure.

D

h R D 4  1  4 C 4 C 4 C 3 C 0 D 60

h R D 4  1  5 C 5 C 4 C 4 C 2 D 80 R D 1  .e 1=2 C e 1=2 C e 3=2 C e 3=2 C e 5=2 C e 5=2 /  32:63

12.

f .x; y/ D x 2 C y 2 h R D 4  1  f . 12 ; 12 / C f . 32 ; 12 / C f . 52 ; 21 / C f . 72 ; 12 / C f . 92 ; 12 / C f . 12 ; 32 / C f . 32 ; 32 / C f . 52 ; 32 / C f . 72 ; 32 / C f . 92 ; 32 /

C f . 12 ; 52 / C f . 32 ; 52 / C f . 52 ; 52 / C f . 72 ; 52 /

i C f . 12 ; 72 / C f . 32 ; 72 / C f . 52 ; 72 / C f . 12 ; 92 / C f . 23 ; 92 /

13.

D 4 C 3 C 3 C 2 C 2 C 1 D 15 ZZ

ZZ

11.

h

6. I D

   1 5C3 5C2 .3/.2/ C .2/.3/ D 15: 2 3 2

10. J D area of disk D .52 /  78:54

h R D 1  f .1; 0/ C f .1; 1/ C f .2; 0/ C f .2; 1/ i C f .3; 0/ C f .3; 1/

R D 1  f . 12 ; 12 / C f . 12 ; 32 / C f . 23 ; 21 / C f . 32 ; 32 / i C f . 52 ; 12 / C f . 52 ; 32 /



1 dA h R D 4  1  5 C 5 C 5 C 5 C 4 D 96

D 4 C 3 C 3 C 2 C 2 C 1 D 15

5.

1 3

RR

D 918

R

dA D area of R D 4  5 D 20: y

1

1

.5

x

3 x

y/ dA is the volume of the solid in the

D R

z

zD5

x

y

4

Fig. 14.1-13 5 14.

3

ZZ

D

.x C 3/ dA D

2 x

2

3 Fig. 14.1-6

538

y

ZZ

D

x dA C 3

ZZ

dA

D

D 0 C 3.area of D/

22 D3 D 6: 2 The integral of x over D is zero because D is symmetrical about x D 0.

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 14.1

y

(PAGE 820)

y x 2 Cy 2 D1

p yD 4 x 2

2

1 D

x

2

2x

Fig. 14.1-14

15.

Fig. 14.1-17

T is symmetric about the line x C y D 0. Therefore, ZZ .x C y/ dA D 0.

18.

ZZ

x 2 Cy 2 a2

p a2

x2

y 2 dA

D volume of hemisphere shown in the figure   1 4 3 2 D a D a3 : 2 3 3

T

y

.2;2/ . 1;1/

z T

p

a

x

zD

a2 x 2 y 2

.1; 1/ . 2; 2/ a

Fig. 14.1-15

y

x 2 Cy 2 Da2

x

Fig. 14.1-18 16.

ZZ

jxjCjyj1

D0C0





x 3 cos.y 2 / C 3 sin y  dA   area bounded by jxj C jyj D 1

19.

ZZ

x 2 Cy 2 a2

 a

 p x 2 C y 2 dA

D volume of cone shown in the figure 1 D a3 : 3

1 D   4  .1/.1/ D 2: 2 (Each of the first two terms in the integrand is an odd function of one of the variables, and the square is symmetrical about each coordinate axis.)

z a

y

yDa

p

x 2 Cy 2

1

1 1

x

a x

1

y

x 2 Cy 2 Da2

Fig. 14.1-19 Fig. 14.1-16

17.

ZZ

.4x 2 y 3 x 2 Cy 2 1

20.

ZZ

x C 5/ dA

D 0 0 C 5(area of disk) D 5:

By the symmetry of S with respect to x and y we have

S

(by symmetry)

.x C y/ dA D 2

ZZ

x dA S

D 2  .volume of wedge shown in the figure/ 1 D 2  .a2 /a D a3 : 2

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SECTION 14.1 (PAGE 820)

ADAMS and ESSEX: CALCULUS 9

z

2.

Z

1

0

zDx

D

S

Z

Z

.xy C y 2 / dx dy ˇˇxDy  2 x y 2 ˇ C xy ˇ dy ˇ 2

0 1

0

3 D 2

y

y

xD0

Z

1

3 y dy D : 8 3

0

x .a;a;0/

3.

Fig. 14.1-20 21.

ZZ

.1

x

Z

Z



cos y dy dx ˇyDx Z  ˇ ˇ D sin y ˇ dx ˇ 0 0

y/ dA

T

x x

yD x

D volume of the tetrahedron shown in the figure  11 1 D .1/.1/ .1/ D : 3 2 6

Z

D2



sin x dx D

0

z

.0;0;1/ zD1 x y

4.

Z

2

.0;1;0/

x

y

0

y 2 e xy dx ˇxDy ! Z 2 1 xy ˇˇ 2 D y dy e ˇ ˇ y 0 dy

0

0

T

Z

ˇ ˇ ˇ 2 cos x ˇ D 4: ˇ

xD0

y

D

.1;0;0/

Z

2

y.e

0

y2

1/ dy D

ey

ˇ2 y 2 ˇˇ e4 5 : ˇ D ˇ 2 2

2

0

Fig. 14.1-21 22.

ZZ p b2

5.

y 2 dA

R

ZZ

R

.x 2 C y 2 / dA D

zD

a

Z

b

.x 2 C y 2 / dy ˇyDb  Z a y 3 ˇˇ 2 D dx x y C ˇ 3 ˇ 0 yD0  Z a 1 3 2 dx bx C b D 3 0 ˇ ˇa 1 1 3 bx C b 3 x ˇˇ D .a3 b C ab 3 /: D 3 3 0

D volume of the quarter cylinder shown in the figure 1 1 D .b 2 /a D ab 2 : 4 4 z p b

Z

b2 y 2

dx

0

0

y b y x

a

b

Fig. 14.1-22 R

Section 14.2 Iteration of Double Integrals in Cartesian Coordinates (page 827) 1.

Z

1

dx 0

D D

Z

x

0

1

dx 0

5 6

540

Z

Z

1 0

Fig. 14.2-5

.xy C y 2 / dy



y3 xy 2 C 2 3

x 3 dx D

5 : 24

a

x

ˇˇyDx ˇ ˇ ˇ yD0

6.

ZZ

R

x 2 y 2 dA D

Z

D

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a 0 3

x 2 dx

Z

b

y 2 dy

0 3 3

a b a b3 D : 3 3 9

x

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INSTRUCTOR’S SOLUTIONS MANUAL

7.

ZZ D D

S

SECTION 14.2

.sin x C cos y/ dA

Z

Z

Z

=2

dx 0

Z

=2

0

ZZ

R

xy 2 dA D

.sin x C cos y/ dy

0

=2

9.

D

 ˇˇyD=2 dx y sin x C sin y ˇˇ 



sin x C 1 dx ˇ ˇ=2     ˇ cos x C x ˇ D C D : D ˇ 2 2 2

D

2

0

Z

1

x dx 0 1

x dx 0

Z

p x

y 2 dy

x2



1 3 y 3

p

ˇˇyD ˇ ˇ ˇ

0

y

yDx 2

y

 2

xDy 2

.1;1/ yDx 2

R

S

x x

8.

D D

3y/ dA D

.x T

Z

Z

a 0 a 0

 dx xy

  b x

 2 x D b 2 a2 b D 6

Z

a

dx 0

Z

 2

b x3 a 3

Fig. 14.2-9

b.1 .x=a//

.x

0 ˇˇyDb.1 .x=a//

3 2 ˇ y ˇ ˇ 2 yD0  2 3 2 x b 1 a 2

x

x

Fig. 14.2-7

ZZ

x

Z  1 1  5=2 D x x 7 dx 3 0  ˇ1 1 2 7=2 x 8 ˇˇ D x ˇ 3 7 8 ˇ 0   1 2 1 3 : D D 3 7 8 56

yD0

=2

Z

(PAGE 827)

3y/ dy

ZZ

2 

dx ˇa 1 b 2 x 3 ˇˇ ˇ 2 a2 ˇ

D D

0

ab 2 : 2 y

x cos y dA

D

D

x 2x C 2 a a

3 2 3 b2 x2 b xC 2 2 a

10.

D

Z

1

x dx

0

Z

0

Z

Z

1 x2

cos y dy 0

ˇyD1 1 ˇ x dx .sin y/ˇˇ

x2

yD0

1

2

Let u D 1 x 2 du D 2x dx ˇ0 Z 0 ˇ 1 1 cos.1/ 1 ˇ sin u du D cos uˇ D : ˇ 2 1 2 2 x sin.1

x / dx

0

1

y

b

1

x y C D1 a b

yD1 x 2 D 1

T

x x

a

x

Fig. 14.2-8

Fig. 14.2-10

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541

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SECTION 14.2 (PAGE 827)

11.

ADAMS and ESSEX: CALCULUS 9

y

For intersection: xy D 1, 2x C 2y D 5. Thus 2x 2 5x C 2 D 0, or .2x 1/.x 2/ D 0. The intersections are at x D 1=2 and x D 2. We have ZZ

ln x dA D

D

D

Z

Z

D

2

ln x 1=2 2

ln x 1=2





5 2

Z

Z

2

ln x dx 1=2

x

5 2

x





y

.5=2/ x

yDx

dy

T

1=x a

x

dx

dx

dV D

U D ln x dx dU D x



1 x

.a;a/

5 2

2 ˇˇ2 1 ln x ˇˇ 2 1=2 x



Fig. 14.2-12

13.

dx

5 x2 x 2 2 ˇ2     ˇ x2 5 1 1 ˇ 2 2 x D .ln 2/ .ln / C ln x ˇ ˇ 2 2 2 2 1=2  Z 2  5 x dx 2 1=2 2   5 1 15 1 15 C D .5 2/ ln 2 ln 4 8 2 4 16 45 33 ln 2 : D 8 16 V D

Z 1 y Z py e x y x dx e dA D dy y 0 y R y Z 1 1 .1 y/e y dy D 2 0 U D 1 y d V D e y dy d U D dy V D ey " # ˇ1 Z 1 ˇ 1 yˇ y D .1 y/e ˇ C e dy 2

ZZ

0

0

D

1 1 C .e 2 2

e 1/ D 2

1:

y

.1;1/



y



yDx

1 ;2 2

D xyD1

R

yDx 2

  2xC2yD5 1 2; 2

x

Fig. 14.2-13 x

14.

Fig. 14.2-11

12.

ZZ p

a2

T

D

Z

a

.a 0

Da

Z

a 0

y 2 dA D p y/ a2

p a2

Z

a 0

p a2

y 2 dy

y 2 dy Z a p y 2 dy y a2

Z

ZZ

T

Z x x dx y dy 4 0 1Cx 0 Z 1 x3 1 dx D 2 0 1 C x4 ˇ1 ˇ 1 ln 2 D ln.1 C x 4 /ˇˇ D : 8 8

xy dA D 1 C x4

a

dx

y

1

0

y

.1;1/

y 2 dy

0

Let u D a2 y 2 du D 2y dy Z a2 1 0 1=2 Da u du C 4 2 a2 ˇ 2   a3 1 3=2 ˇˇa  1 D u ˇ D a3 : 4 3 4 3 0 542

Z

yDx T 1

Fig. 14.2-14

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INSTRUCTOR’S SOLUTIONS MANUAL

15.

Z

1

dy 0

D

Z Z

Z

1

e

x2

y

1

x2

e

dx

0 1

x2

dx D

Z

x

Z

x2

e

xe

y

R

.1;1/ 1

dy

R

0

yDx

dx

0

0

 1 : e

x

y

Fig. 14.2-17

.1;1/

1

yDx

18.

R 1

x

Z

=2

dy 0

D

Z

=2 0

Z

Z

Z x 1=3 p 1 y 4 dy dx 0 ZZ x p D 1 y 4 dA .R as shown/ R Z 1 p Z 1 p y 3 1 y 4 dy D y 1 y 4 dy 1

0

0

Fig. 14.2-15

16.

(PAGE 827)

(R as shown)

dx

Let u D x 2 du D 2x dx ˇ1  Z 1 1 u ˇˇ 1 1 u e ˇ D 1 e du D D ˇ 2 0 2 2

D

SECTION 14.2

Let v D 1 y 4 Let u D y 2 dv D 4y 3 dy du D 2y dy Z 1p Z 1 1 0 1=2 D 1 u2 du C v dv 2 0 4 1 ˇ0 ˇ  1 1  1  ˇ  12 C v 3=2 ˇ D : D ˇ 2 4 6 8 6

ZZ sin x sin x dx D dA (R as shown) x R x y Z x Z =2 sin x dx dy D sin x dx D 1: x 0 0 =2

1

y

y

.=2;=2/

1

yDx 1=3

.1;1/

R

yDx

yDx R

=2

x

x

Fig. 14.2-18

Fig. 14.2-16

17.

Z

1

dx 0

ZZ

Z

1 x

x2 

y dy C y2

. > 0/

y dA .R as shown/ 2 C y2 x R Z y Z 1 dx y  dy D 2 2 0 x Cy 0  ˇˇxDy Z 1 1 1 x ˇ  tan D y dy ˇ y y ˇ 0 xD0 ˇ1 Z 1 ˇ y ˇ   y  1 dy D : D ˇ D 4 0 4 ˇ 4 D

0

19.

20.

V D

Z

1

dx

0

D

Z

V D

Z

1

Z

dy 0 Z 1 y D 0

x 2 / dy

.1 0

x 2 /x dx D

.1

0

1

x

Z

y

x 2 / dx

.1 0

y3 3

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1 1 D cu. units. 4 4

1 2



dy D

1 2

1 5 D cu. units. 12 12

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lOMoARcPSD|6566483

SECTION 14.2 (PAGE 827)

21.

V D D

Z

Z

Z

1

dx 0

0

.1

 D .1 0 Z 1 2 D 3 0 Z

1

x

2

2

y / dy ˇ  yD1 x y 3 ˇˇ dx x 2 /y ˇ 3 ˇ yD0  .1 x/3 2 x /.1 x/ dx 3  4x 3 1 1 2 2 2x 2 C C D cu. units. dx D 3 3 3 3 3

0

 .1

1

1 x

ADAMS and ESSEX: CALCULUS 9

25.

Vol D D4 D4 D D

22. z D 1 y 2 and z D x 2 intersect on the cylinder x 2 C y 2 D 1. The volume lying below z D 1 y 2 and above z D x 2 is ZZ

V D

.1

x 2 Cy 2 1

D4 D4

Z

Z

8 3

1

dx 0 1 0

Z

Z

D

x 2 / dA

.1

x2

0

Z

x2

.1

2y 2 / dy

0

0 1

1 p .1 2

0

2 .1 x 2 /3=2 p 3 2 2

2 3=2

x /

x 2 /y

1= 2

y 3

ˇ ˇ ˇ

1 x

yD0

Fig. 14.2-25

26.

Vol D

Z

2

dx

x

2 1

ZZ 

Z

2

T a

x a

y dA b .x=a//  2

Z b.1 x y dy dx a b  Z0 a  0     x 2 x 1 2 x b 1 D b 1 dx 2 a a 2b a 0  Z a b x2 4x D C 2 dx 3 2 0 a a  ˇa x 3 ˇˇ 2x 2 2 b C 2 ˇ D ab cu. units: 3x D ˇ 2 a 3a 3 0

dx D ln 2 cu. units.

y

b

x y a C b D1

V D D

Z

 1=4

dy 0

1 3

Z

1 D 12

544

Z

y

x 2 sin.y 4 / dx

0

 1=4 0

Z

 0

dx

0

1

24.

!

x 2 C2y 2 D1

ˇyDp1 x 2 3 ˇ

1 dy x C y 1 00 ˇyDx 1 Z 2 ˇ ˇ A D dx @ln.x C y/ˇ ˇ 1 yD0 Z 2 Z D .ln 2x ln x/ dx D ln 2

V D

x 2 /=2

p Z 4 2 1 .1 x 2 /3=2 dx Let x D sin  3 0 dx D cos  d p p Z   Z 4 2 =2 1 C cos 2 2 4 2 =2 4 d cos  d D 3 3 2 0 0 p Z =2   2 1 C cos 4 d 1 C 2 cos 2 C 3 0 2 ˇ p  ˇ=2 2 3 1  ˇ C sin 2 C sin 4 ˇ D p cu. units. ˇ 3 2 8 2 2 0

D

23.

dx

y 2 / dy

x 2 /3=2 dx

.1

1

2y 2 / dA

p

Let x D sin u dx D cos u du Z Z =2 8 =2 2 D cos4 u du D .1 C cos 2u/2 du 3 0 3 0   Z 2 =2 1 C cos 4u D du 1 C 2 cos 2u C 3 0 2 23  D D cu. units. 32 2 2 D

Z

x2 Z p.1

.1 E

y

p 1 x2

 dx .1

1

y2

D

Z

ZZ

y 3 sin.y 4 / dy

T

Let u D y 4 du D 4y 3 dy

a

1 sin u du D cu. units. 6

Fig. 14.2-26

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INSTRUCTOR’S SOLUTIONS MANUAL

27.

SECTION 14.3

Vol D 8  part in the first octant Z a Z pa2 x 2 p D8 a2 x 2 dy dx 0 0 Z a D8 .a2 x 2 / dx 0  ˇa x 3 ˇˇ 16 3 D 8 a2 x a cu. units: ˇ D 3 ˇ 3

30. ZZ

Since F 0 .x/ D f .x/ and G 0 .x/ D g.x/ on a  x  b, we have f .x/g.x/ dA D

T

D

0

z

D

a

ZZ

x 2 Cz 2 Da2

f .x/g.x/ dA D

T

D

y x 2 Cy 2 Da2

Z

Fig. 14.2-27

D

ZZx

2 C2y 2 8



8

x

a

12 dA

.y

f .x/ dx b

a

Z

b

 f .x/ G.x/

g.y/ dy

a

a

G.u/ du D D D

where C D

Z

Z

Z

x

du a d

dt c

d

Z

Z

Z

b

a

 g.y/ F .b/

F .y/g.y/ dx:

a

Z

f .x/G.x/ dx D F .b/G.b/ F .a/G.a/

b

g.y/F .y/ dy: a

.b;b/

.a;a/

.b;a/

x

Fig. 14.2-30

f1 .u; t / dt 1.

f1 .u; t / du  f .a; t / dt D g.x/

c

ZZ

e

x y

Q

dA D D

C; 2.

ZZ

Q

Z

1

e

G.u/ du D G.x/:

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x

Z

dx

0

1

e

y

dy

0

lim . e

x

R!1

dA D .1 C x 2 /.1 C y 2 /

x a

b

Section 14.3 Improper Integrals and a Mean-Value Theorem (page 832)

the Fundamental Theorem of Calculus we obtain Z

Z

F .b/G.a/

(by symmetry)

f .a; t / dt is independent of x. Applying

d dx

 F .y/ dy

T

d

g 0 .x/ D

F 0 .x/ dx

 4/ dA

c x

f .x; t /

c

b

y

d

a

G.a/F .b/ C G.a/F .a/

y

29. With g.x/ and G.x/ defined as in the statement of the problem, we have Z

Z

b

x 2 C2y 2 8

x

 G.a/ dx

f .x/G.x/ dx

a

Z

x2 y2 D 12  area of ellipse C D1 8p 4 p D 12  .2 2/.2/ D 48 2 cu. units:

Z

G 0 .y/ dy

a

a

Z

x

b

28. The part of the plane z D 8 x lying inside the elliptic cylinder x 2 D 2y 2 D 8 lies above z D 0. The part of the plane z D y 4 inside the cylinder lies below z D 0. Thus the required volume is ZZ

Z

b

Thus

a

Vol D

Z

D F .b/G.b/

a x

(PAGE 832)

ˇR !2 ˇ /ˇˇ D 1 (converges) 0

Z

1

Z

1

dy 1 C y2 ˇR !2 ˇ 2 1 ˇ D lim .tan x/ˇ D R!1 4 0 0

dx 1 C x2

0

(converges)

545

lOMoARcPSD|6566483

SECTION 14.3 (PAGE 832)

3.

ZZ

S

Z

ADAMS and ESSEX: CALCULUS 9

Z 1 dx y dy 2 0 1 1Cx 0 ˇR 1 ˇ 1  ˇ D @ lim tan 1 x/ˇ A D (converges) ! 1 ˇ 2 SR!1 2

y dA D 1 C x2

1

which diverges to infinity. Thus the given double integral diverges to infinity by comparison.

S

4.

ZZ

T

1 p dA D x y

Z

Z

1

2x

dx dy p x x y p Z 1 p 2. 2x x/ dx D x 0 Z 1 p p dx D 2. 2 1/ p D 4. 2 x 0 y 0

7.

ZZ

e 2

.jxjCjyj/

R

dA D 4 D4

ZZ

Z

1

e

.xCy/

x

dx

e

Z

0

0

D4 1/ (converges)

x0 y0

lim

R!1

e

dA 1

ˇR ˇ xˇ ˇ

0

y

e

!2

dy

D4

(The integral converges.)

.1; 2/ 8. y D 2x

T

On the strip S between the parallel lines x C y D 0 and x C y D 1 we have e jxCyj D e .xCy/  1=e. Since S has infinite area,

.1; 1/

ZZ

yDx Since e

x

ZZ

ZZ

x2 C y2 5. dA 2 2 Q .1 C x /.1 C y / ZZ x 2 dA D2 (by symmetry) 2 2 Q .1 C x /.1 C y / Z 1 Z 1 2 Z 1 2 dy x dx x dx D  ; D2 1 C x2 0 1 C y2 1 C x2 0 0 which diverges to infinity, since x 2 =.1 C x 2 /  1=2 on Œ1; 1/. 6.

ZZ

dA D 1CxCy 0

Z

Z

1

1

0

ln.1 C u/ Since lim D 1, we have ln.1 C u/  u=2 on u!0C u some interval .0; u0 /. Therefore  ln 1 C

1 1Cx





1 2.1 C x/

on some interval .x0 ; 1/, and Z

0

546

1

 ln 1 C

1 1Cx



e 2

R

jxCyj

dA >

dx 

Z

1 x0

1 dx; 2.1 C x/

ZZ

e

jxCyj

S

and the given integral diverges to infinity. y xCyD1

S

1 dy 1CxCy

dx 0 1 ˇ Z 1 ˇyD1 @ln.1 C x C y/ˇˇ A dx D ˇ 0 yD0   Z 1  Z 1  1 2Cx dx D dx: ln 1 C D ln 1Cx 1Cx 0 0 H

dA D 1:

> 0 for all .x; y/ in R2 , we have

jxCyj

Fig. 14.3-4

jxCyj

e S

x

xCyD0

Fig. 14.3-8

9.

Z x dx e y=x dy x3 0 1 T 0 ˇyDx 1 Z 1 ˇ dx @ y=x ˇ A D xe ˇ 3 ˇ x 1 yD0 Z 1  dx 1 D 1 e x2 1 0 ˇR 1   ˇ 1 1 1 ˇ A lim @ D1 D 1 ˇ e R!1 xˇ e

ZZ

1 e x3

y=x

dA D

Z

1

1

(The integral converges.)

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 14.3

y

13.

a) I D

yDx

D

T

.1;1/

Z

S 1

0

Z

dA D xCy

1

dx

0

0

c!0C

T

1

Z

.1;1/

1

S

0

T

x

Since e

xy

e

xy

dA >

Q

ZZ

xy

e

dA;

e

xy

dA >

Q

Z

1

dx

1

Z

1=x

e

xy

dy >

0

1 e

Z

1

1

14.

dx D 1: x

1 x Q

R

15. Fig. 14.3-11 ZZ

Z 1 Z 1=x 1 1 1 1 sin dA D sin dx dy x x R x 2= x 0 Z 1 1 1 D sin dx Let u D 1=x 2 x x 2= du D 1=x 2 dx ˇ0 Z 0 ˇ D sin u du D cos uˇˇ D1

(The integral converges.)

ln x/ dx D 2 ln 2

.ln 2x

Z

0

1

dx D 2 ln 2:

0

x

1

=2

ZZ

yD0

1

2xy dA 2 C y2 x S ZZ 2xy D4 dA (T as in #9(b)) 2 C y2 x T Z 1 Z x y dy D4 x dx Let u D x 2 C y 2 2 2 0 0 x Cy du D 2y dy Z 1 Z 2x 2 du D2 x dx u 0 x2 Z 1 D 2 ln 2 x dx D ln 2 cu. units.

Vol D

y

12.

c

Z

c!0C c

The given integral diverges to infinity. yD

ZZ

D 2 lim

R

where R satisfies 1  x < 1, 0  y  1=x. Thus ZZ

Fig. 14.3.13b

Z 1 Z x dA dy D 2 lim c ! 0C dx x C y x Cy T c 0 ˇyDx ! Z 1 ˇ D 2 lim c ! 0C dx ln.x C y/ˇˇ

> 0 on Q we have ZZ

x

Fig. 14.3.13a b) I D 2

11.

.1;1/

x

dy x2 C y2 0 ˇyDx 1 Z 1 ˇ y 1 ˇ A D dx @ tan 1 ˇ ˇ x x 1 yD0 Z  1 dx D D1 4 1 x (The integral diverges to infinity.) dx

c

y

Fig. 14.3-9 Z

iˇˇ1 x ln x ˇˇ

.c C 1/ ln.c C 1/ C c ln c D 2 ln 2:

0

c!0C

dA D x2 C y2

dy xCy

yD0

y

ZZ

1

ˇyD1 ! ˇ dx ln.x C y/ˇˇ

D lim 2 ln 2

10.

Z

h D lim .x C 1/ ln.x C 1/

x

1

ZZ

(PAGE 832)

=2

ZZ

dA D a Dk x converges if k

Z

Z k Z 1 dx x dy D xk a 0 0 0 x a > 1, that is, if k > a 1

16.

ZZ

y b dA D

Z

17.

ZZ

x a dA D

Z

1

Z

xk

Z

a

dx, which 1.

1

x k.bC1/ dx if bC1 Dk 0 0 0 b > 1. This latter integral converges if k.b C 1/ > 1. Thus, the given integral converges if b > 1 and k > 1=.b C 1/.

Rk

dx

1

x a dx

1

converges if k C a
1. Thus, the given integral converges if b > 1 and k > .a C 1/=.b C 1/.

20.

Rk

Z

1

x a dx

1

Z

xk 0

y b dy D

Z

1

1

T

S

D D D D

Z

1

dx

0

Z

dx

0 1

dx

0

Z

1

0

Z

1

0

1

Z

.b

Z

1

0



Z



x y dy .x C y/3

xC1

x

1 u

uDx

dx D .x C 1/2

Other iteration: ZZ

S

x y dA D .x C y/3 D D D D

548

Z

1

dy

0

Z

dy

Z

1

dy

0 1

0

Z

 1 0



1 1 C x x

ˇ1 1 ˇˇ 1 ˇ D : x C 1ˇ 2

yC1

y u2

y .y C 1/2

u

1 a/.d

2y

c/

ZZ

x 2 dA R

D



d

dx

R c

a

0

x y dx .x C y/3

y

0

Z

1

0

1

Z

Z

x

y

x .x C 1/2

1 xC1

Z

Z d Z b 1 dy x 2 dx .b a/.d c/ a c a2 C ab C b 2 1 b 3 a3 D : D b a 3 3

Let u D x C y du D dy

2x u du u3 ˇ  uDxC1 x ˇˇ ˇ u2 ˇ

dx

The average value of x 2 over the rectangle R is

One iteration: x y dA D .x C y/3

1

which diverges to infinity. 22.

ZZ

Z

x y dy 3 0 .x C y/ 0 Let u D x C y du D dy Z 1 Z 2x 2x u du D dx u3 0 x ˇ   uD2x Z 1 1 x ˇˇ D dx ˇ u u2 ˇ 0 uDx Z 1 1 dx D 4 0 x

x aC.bC1/k dx, bC1

if b > 1. This latter integral converges if a C .b C 1/k < 1. Thus, the given integral converges if b > 1 and k < .a C 1/=.b C 1/.

21.

x y dA D .x C y/3

23.

The average value of x 2 C y 2 over the triangle T is 2 a2 D

uDy

1 yC1

1 1 C y y

ˇ1 1 ˇˇ dx D ˇ D .y C 1/2 y C 1ˇ 0

x

Fig. 14.3-22

Let u D x C y du D dx

du u3 ˇ  uDyC1 1 ˇˇ ˇ u ˇ

b



1 : 2

D dy

D D

ZZ

.x 2 C y 2 / dA Z a x Z a 2 .x 2 C y 2 / dy dx a2 0 0  ˇyDa x Z a 2 y 3 ˇˇ 2 dx x y C ˇ a2 0 3 ˇ yD0 Z ah i 2 2 3 3x .a x/ C .a x/ dx 3a2 0 Z ah i a2 2 a3 3a2 x C 6ax 2 4x 3 dx D : 2 3a 0 3 T

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 14.3

y

(PAGE 832)

y a

a

p yD a2 x 2

yDa x Q

T a x

a

x

xCyD0

Fig. 14.3-23

Fig. 14.3-25 24.

The area of region R is Z

1

p . x

x 2 / dx D

0

26.

Let R be the region 0  x < 1, 0  y  1=.1 C x 2 /. If f .x; y/ D x, then Z Z 1 Z 1=.1Cx 2 / Z 1 x dx f .x; y/ dA D x dx dy D 1 C x2 R 0 0 0 which diverges to infinity. Thus f has no average value on R.

27.

If f .x; y/ D xy on the region R of the previous exercise, then ZZ Z 1 Z 1=.1Cx 2 / f .x; y/ dA D x dx y dy R 0 0 Z 1 x dx 1 Let u D 1 C x 2 D 2 0 .1 C x 2 /2 du D 2x dx Z 1 1 1 du D D 4 u2 4 Z 11  dx D : Area D 1 C x2 2 0 2 1 1 Thus f .x; y/ has average value  D on R.  4 2 The integral in Example 2 reduced to  Z 1  1 ln 1 C 2 dx x 1   1 U D ln 1 C 2 d V D dx x V Dx 2 dx dU D x.x 2 C 1/ 3 2  ˇR Z R 1 ˇˇ dx 5 D lim 4x ln 1 C 2 ˇ C 2 2 R!1 x ˇ 1 1Cx 1    ln 1 C .1=R2 /  D2 ln 2 C lim R!1 2 4 1=R .2=R3 /   ln 2 C lim  D R!1 2 1 C .1=R2 / . 1=R2 /

1 sq. units. 3

The average value of 1=x over R is

3

ZZ

R

dA D3 x

Z

1

dx x 0 Z 1 D3 x

Z

p

x

dy x2

1=2

0

 9 x dx D : 2

y

xDy 2

.1;1/ yDx 2

R x

28.

x

Fig. 14.3-24

25. The distance p from .x; y/ to the line x C y D 0 is .x C y/= 2. The average value of this distance over the quarter-disk Q is p ZZ xCy 4 2 p dA D x dA a2 2 Q Q p Z Z pa 2 x 2 4 2 a x dx D dy a2 0 0 p Z a p 4 2 x a2 x 2 dx Let u D a2 x 2 D 2 a 0 du D 2x dx p p Z 2 4 2a 2 2 a 1=2 u du D : D a2 0 3

4 a2

ZZ

D

29.

 2

ln 2:

By the Mean-Value Theorem (Theorem 3), ZZ f .x; y/ dA D f .x0 ; y0 /hk Rhk

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SECTION 14.3 (PAGE 832)

ADAMS and ESSEX: CALCULUS 9

for some point .x0 ; y0 / in Rhk . Since .x0 ; y0 / ! .a; b/ as .h; k/ ! .0; 0/, and since f is continuous at .a; b/, we have ZZ 1 lim f .x; y/ dA .h;k/!.0;0/ hk Rhk D

lim

.h;k/!.0;0/

D

R

Z

f12 .x; y/ dA D a

aCh h

Z

Z

aCh

dx

a

D

Z

b

bCk h

b

D f .a C h; b C k/ Thus

ZZ

R

7.

f12 .x; y/ dy

f12 .x; y/ dA D

ZZ

f .a; b C k/ C f .a; b/:

1.

D

2

2

.x C y / dA D

2

d 0

Q

y dA D

a

ZZ

4.

D

jxj dA D 4

Z

=2

d

Z

=2

d 0

ZZ

a

r sin  r dr a3 a3 D 3 3

ZZ

ex

2 Cy 2

Q

Z

dA D

=2

d 0

 D 2

10.



1 r2 e 2

Z

a

2

e r r dr

0

ˇˇa 2 .e a ˇ ˇ D ˇ 4

1/

0

Z a 2 Z =2 2xy 2r sin  cos  d dA D r dr 2 C y2 x r2 0 Q 0 ˇ =2 Z a2 =2 a2 cos.2 / ˇˇ a2 D sin.2 / d D D ˇ ˇ 2 0 4 2

ZZ

0

11. 2

r r dr

ZZ

S

.x C y/ dA D D

Z

Z

=3

d 0

Z

0

=3 0 3

a

.r cos  C r sin  /r dr

.cos  C sin  / d

Z

a 0

r 2 dr

ˇ=3 ˇ a .sin  cos  /ˇˇ 3 0 " p ! # p 3 1 a3 . 3 C 1/a3 D . 1/ D 2 2 3 6 D

y p yD 3x

a

r cos  r dr

0

0

r 4 cos2  sin2  r dr

0

9.

x 2 Cy 2 Da2

ˇ=2 ˇ a3 4a3 ˇ D 4 sin  ˇ D ˇ 3 3

S =3

a4 ; by symmetry the value of this integral 4 D is half of that in Exercise 1.

550

Z

0 ˇ=2 ˇ

0

5.

a

2a3 ; by symmetry, the value is twice 3 Q that obtained in the previous exercise.

0

Z

Z

.x C y/ dA D

a4 a4 D D 2 4 2 Z 2 Z a ZZ p 2a3 x 2 C y 2 dA D d r r dr D 2. 3 0 0 D Z 2 ZZ Z a dA r dr D 2a D 3. d p 2 2 r x Cy 0 D 0 ZZ

0

ˇ D . cos  /ˇ ˇ

R

Z

d

8.

Section 14.4 Double Integrals in Polar Coordinates (page 842) Z

ZZ

f21 .x; y/ dA:

Divide both sides of this identity by hk and let .h; k/ ! .0; 0/ to obtain, using the result of Exercise 31, f12 .a; b/ D f21 .a; b/:

ZZ

=2

0

i f2 .a; y/ dy

f .a C h; b/

Z

Z a6 =2 2 sin .2 / d 6 0 Z  a6 =2  a6 D 1 cos.4 / d D 12 0 24

b

a

f2 .a C h; y/

x 2 y 2 dA D 4 D

bCk

D f .a C h; b C k/ f .a; b C k/ f .a C h; b/ C f .a; b/ ZZ Z bCk Z aCh f21 .x; y/ dA D dy f21 .x; y/ dx R

D

i f1 .x; b/ dx

f1 .x; b C k/

ZZ

f .x0 ; y0 / D f .a; b/:

30. If R D f.x; y/ W a  x  a C h; b  y  b C kg, then ZZ

6.

a

x 2 dA D

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Fig. 14.4-11

x

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

12.

ZZ

S

x dA D 2 2 D 3

Z

=4

d 0

Z

Z

p 2

0

D 4

ˇ=4 ˇ 2 ˇ tan  ˇ ˇ 3

0

y

=4

S 1

p

ln.x 2 C y 2 / dA D

x

d

0

Z

1

.ln r 2 /r dr

0

r ln r dr

0

The average distance from the origin to points in the disk D: x 2 C y 2  a2 is ZZ p x 2 C y 2 dA D

1 a2

Fig. 14.4-12 16.

D

1 a2

Z

2

d

ZZ

a

0

0

2

r 2 dr D

2a : 3

2

e .x Cy / dA a2 / R Z 2 Z b 1 2 d e r r dr D .b 2 a2 / 0 a Z b2 1 1 e u du .2/ D .b 2 a2 / 2 a2   1 2 2 D 2 e a e b : 2 b a

.b 2

ZZ

17.

Z

p The annular region R: 0 < a  x 2 C y 2  b has 2 2 area .b 2 a2 /. The average value of e .x Cy / over the region is 1

Z =4 Z sec  .x 2 C y 2 / dA D d r 3 dr T 0 0 Z 1 =4 4 sec  d D 4 0 Z 1 =4 D .1 C tan2  / sec2  d Let u D tan  4 0 du D sec2  d Z 1 1 .1 C u2 / du D 4 0  ˇ1 u3 ˇˇ 1 1 uC D ˇ D 4 3 ˇ 3

2

(Note that the integral is improper, but converges since limr!0C r 2 ln r D 0.)

2

15.

13.

Z

(PAGE 842)

U D ln r d V D r dr dr r2 dU D V D r 2 2 3 ˇ1 Z 1 ˇ 2 1 r ˇ D 4 4 ln r ˇ r dr 5 ˇ 2 2 0 0   1 D 4 0 0 D  4

0

2 2 D 3 3

ZZ

x 2 Cy 2 1 Z 1

 sec3  d

 p cos  2 2

ˇ=4 p ˇ 4 2 ˇ D sin  ˇ ˇ 3 4 D 3

14.

r cos  r dr

sec 

=4

SECTION 14.4

Let u D r 2 du D 2r dr

If D is the disk x 2 C y 2  1, then ZZ

dA D 2 .x C y 2 /k

D

Z

2

d

0

Z

1

r

2k

0

r dr D 2

Z

1

r1

2k

dr

0

which converges if 1 2k > 1, that is, if k < 1. In this case the value of the integral is

0

y

.1;1/

ˇ1 r 2 2k ˇˇ  2 : ˇ D 2 2k ˇ 1 k 0

xD1 rDsec 

yDx T =4 1

Fig. 14.4-13

x

18.

ZZ

dA

R2 .1 C x 2 C y 2 /k

D

Z

2

d

0

D

Z

1

0

Z

1

1

u

k

r dr .1 C r 2 /k

du D

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Let u D 1 C r 2 du D 2r dr

 if k > 1: 1 k

551

lOMoARcPSD|6566483

SECTION 14.4 (PAGE 842)



The integral converges to

19.

ZZ

D

Z

xy dA D

Z

=4

d

0

Z

1 2

D

k

1

22.

if k > 1.

a

r cos  r sin  r dr

0

=4

ADAMS and ESSEX: CALCULUS 9

sin 2 d

0

Z

a

r 3 dr

One quarter of the required volume lies in the first octant. (See the figure.) In polar coordinates the cylinder x 2 C y 2 D ax becomes r D a cos  . Thus, the required volume is ZZ p a2 x 2 y 2 dA V D4 D4

0

 ˇ=4 a4 a4 cos 2 ˇˇ D : D ˇ ˇ 8 2 16

D2

0

y

x 2 Cy 2 Da2

=4 a

Z

D =2

0

d 0

Z

=2

4 3

D

4 3 a 3

d 0

Z

Fig. 14.4-19

20.

ZZ

C

y dA D

Z



d 0

1 D 3

Z

1 3

Z

D

r sin  r dr

sin .1 C cos  /3 d

0

0

1Ccos 

0



2

Z

ˇ2 4ˇ

4 u ˇ ˇ D 12 ˇ 3

u3 du D

Let u D 1 C cos  du D sin  d

D

2a3 3

D

2a3 3

2a3 D 3

a2

r 2 r dr

0 a2

u

ˇ ˇ

=2

sin3  / d

.1 0

Z

 2

Let u D a2 r 2 du D 2r dr

u1=2 du 1

2 2 0a sin ˇ 2 ˇa @ 3=2 ˇ

a2 sin2 

A

=2

2

sin .1

cos  / d

0

!

Let v D cos  dv D sin  d Z 4a3 1 .1 v 2 / dv 3 0  ˇ1 4a3 v 3 ˇˇ v ˇ 3 3 ˇ 0

8a3 2 D a3 .3 9 9

0

y

p

a cos 

Z

=2

4 D a3 3

x

Z

d

D

yDx D

Z

4/ cu. units:

z

rD1Ccos  a x 2 Cy 2 Cz 2 Da2

C 2 x

x 2 Cy 2 Dax

Fig. 14.4-20

21.

The paraboloids z D x 2 C y 2 and 3z D 4 x 2 y 2 intersect where 3.x 2 C y 2 / D 4 .x 2 C y 2 /, i.e., on the cylinder x 2 C y 2 D 1. The volume they bound is given by V D D

Z

x 2 Cy 2 1 Z 1 2

d

0

8 D 3 D

552



ZZ

8 3

Z

0

1

.r 0



r2 2

x2 3

4



r2

4 3

y2 

 .x 2 C y 2 / dA

r 2 r dr

r 3 / dr ˇ1 r 4 ˇˇ 2 cu. units: ˇ D 4 ˇ 3 0

D x

a y

a

Fig. 14.4-22 23.

The volume inside the sphere x 2 C y 2 C z 2 D 2a2 and the cylinder x 2 C y 2 D a2 is Z =2 Z ap V D8 d 2a2 r 2 r dr Let u D 2a2 r 2 0 0 du D 2r dr Z 2a2  3 p 4a 2 2 1 cu. units: D 2 u1=2 du D 3 a2

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lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 14.4

(PAGE 842)

z

z p

2a x 2 Cy 2 Cz 2 D2a2

x 2 Cy 2 Da2 a x 2 Cz 2 Da2 xDy

x 2 Cy 2 Da2

a

p 2a

D

a

y

y

x

x

y 2 Cz 2 Da2

Fig. 14.4-25

Fig. 14.4-23

24.

a

Volume D

Z

2

Z

2

.r cos  C r sin  C 4/r dr 0 0 Z 2 Z 2 Z D .cos  C sin  / d r 2 dr C 8 d

0

0

26. 2

r dr

0

V D4

2

D 0 C 4.2 / D 16 cu. units:

D4

D 16

ZZ p

Z

0

a2

D =4

d

ZZ Z

p

y dA

D =2

Z

2 sin 

p

r sin  r dr ˇ2 sin  1 Z =2 p 2 5=2 ˇˇ A sin  d @ r ˇ D4 ˇ 5 0 0 p p Z 64 2 32 2 =2 3 sin d D cu. units: D 5 15 0

25. One eighth of the required volume lies in the first octant. This eighth is divided into two equal parts by the plane x D y. One of these parts lies above the circular sector D in the xy-plane specified in polar coordinate by p 0  r  a, 0    =4, and beneath the cylinder z D a2 x 2 . Thus, the total volume lying inside all three cylinders is V D 16

One quarter of the required volume V is shown in the figure. We have

0

d

0

0

x 2 dA Z

a

p

z

a2

r 2 cos2 r dr

0

Let u D a2 r 2 cos2  du D 2r cos2  dr Z =4 Z a2 d D8 u1=2 du cos2  a2 sin2  0 Z 16a3 =4 1 sin3  D d 3 cos2  0   Z 16a3 =4 1 cos2  D sin  d sec2  3 cos2  0 ˇˇ=4  1 16a3 ˇ cos  ˇ tan  D ˇ 3 cos  0  3  p 16a 1 D 2C1 p C1 1 0 3 2   1 3 D 16 1 p a cu. units: 2

yDz 2

x 2 Cy 2 D2y 2

1

y

D

x

Fig. 14.4-26

27.

By symmetry, we need only calculate the average distance from points in the sector S: 0    =4, 0  r  1 to

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553

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SECTION 14.4 (PAGE 842)

ADAMS and ESSEX: CALCULUS 9

the line x D 1. This average value is 8 

ZZ

.1 S

8 x/ dA D 

Z

=4

d

"0 8  D  8

D1

Z

Z

Let x D au, y D bv. Then

ˇ ˇ ˇ @.x; y/ ˇ ˇ ˇ du dv D ab du dv: dx dy D ˇ @.u; v/ ˇ

1

r cos  /r dr

.1

0 =4

cos  d 0

8 p D1 3 2

Z

1

2

r dr 0

p 4 2 units: 3

#

The region E corresponds to the quarter disk Q: u2 C v 2  1, u, v  0 in the uv-plane. Thus V D 8abc

y

D 1 x

30.

! p 6 3 p ;0 . 4 3 3



1  volume of ball of radius 1 8

We use the same regions and change of variables as in the previous exercise. The required volume is  ZZ  x2 y2 1 dx dy a2 b2 E ZZ D ab .1 u2 v 2 / du dv: Q

Now transform to polar coordinates in the uv-plane: u D r cos  , v D r sin  . V D ab D

31.

Z

0

ab 2

=2

d 

r2 2

2

1

.1 r 2 /r dr ˇ1 ab r 4 ˇˇ cu. units: ˇ D 4 ˇ 8 0

0

1 2 1 2

ˇ ˇ ˇ j du dv D 1 du dv: ˇ 2

Under the above transformation the square jxj C jyj  a corresponds to the square S: a  u  a, a  v  a. Thus ZZ ZZ 1 e u du dv e xCy dA D 2 S jxjCjyja Z Z a 1 a u e du dv D 2 a a D a.e a e a / D 2a sinh a:

2

2 x

Fig. 14.4-28

554

Z

uCv u v Let x D ,y D , so that x C y D u and 2 2 x y D v. We have ˇ1 ˇ dx dy D j ˇˇ 21

29. Let E be the region in the first quadrant of the xy-plane bounded by the coordinate axes and the ellipse x2 y2 C D 1. The volume of the ellipsoid is a2 b2 s ZZ x2 y2 1 V D 8c dx dy: a2 b2 E



V D

y

p 3 =3 1 S

v 2 du dv

4 abc cu. units. 3

Fig. 14.4-27 p 3 3/=3 sq. units. Thus

28. The area of S is .4 ZZ 3 xD x dA p 4 3 3 S Z =3 Z 2 6 D p d r cos  r dr 4 3 3 0 sec  Z =3 2 D cos .8 sec3  / d p 4 3 3 0 p ˇ=3 ! p ˇ 2 6 3 p 4 3 tan  ˇˇ p : D D 4 3 3 4 3 3 0

u2

1

Q

D 8abc 

S

The segment has centroid

ZZ p

32.

The parallelogram P bounded by x C y D 1, x C y D 2, 3x C 4y D 5, and 3x C 4y D 6 corresponds to the square S bounded by u D 1, u D 2,v D 5, and v D 6 under the transformation u D x C y;

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v D 3x C 4y;

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 14.4

v

or, equivalently, x D 4u

yDv

v;

3u: v

y

vD2 vD6 R

uD1

uD1 R uD2 vD5

xCyD1 3xC4yD5

(PAGE 842)

uD4

vD1

3xC4yD6 P

u

Fig. 14.4-33

xCyD2x

u

Fig. 14.4.32a We have

Fig. 14.4.32b

ˇ ˇ 4 @.x; y/ D ˇˇ 3 @.u; v/

ˇ 1 ˇˇ D 1; 1 ˇ

so dx dy D du dv. Also x 2 C y 2 D .4u

v/2 C .v

34.

3u/2 D 25u2

14uv C 2v 2 :

we therefore have

Thus we have ZZ ZZ .x 2 C y 2 / dx dy D .25u2 14uv C 2v 2 / du dv P S Z 2 Z 6 7 D du .25u2 14uv C 2v 2 / dv D : 2 1 5 33. Let u D xy, v D y=x. Then ˇ ˇ y @.u; v/ D ˇˇ y=x 2 @.x; y/

ˇ x ˇˇ y D 2 D 2v; 1=x ˇ x

1 du dv: 2

.x 2 C y 2 / dx dy D Hence, ZZ

.x 2 C y 2 / dx dy D

R

@.x; y/ 1 D . The region D in the first quadrant @.u; v/ 2v of the xy-plane bounded by xy D 1, xy D 4, y D x, and y D 2x corresponds to the rectangle R in the uv-plane bounded by u D 1, u D 4, v D 1, and v D 2. Thus the area of D is given by ZZ ZZ 1 dx dy D du dv 2v D R Z 4 Z 2 1 3 dv D D ln 2 sq. units: du 2 1 v 2 1

so that

Under the transformation u D x 2 y 2 , v D xy, the region R in the first quadrant of the xy-plane bounded by y D 0, y D x, xy D 1, and x 2 y 2 D 1 corresponds to the square S in the uv-plane bounded by u D 0, u D 1, v D 0, and v D 1. Since ˇ ˇ ˇ 2x 2y ˇˇ @.u; v/ D ˇˇ D 2.x 2 C y 2 /; y x ˇ @.x; y/

35.

I D

ZZ

e .y

x/=.yCx/

ZZ

S

1 1 du dv D : 2 2

dA.

T

a) I D

Z

=2

d 0

Z

=2

Z

1=.cos Csin /

cos  sin 

e sin Ccos  r dr

0 cos  sin  e sin Ccos 

d .cos  C sin  /2 0 cos  sin  Let u D sin  C cos  2 d du D .sin  C cos  /2 Z e e 1 1 1 u e du D : D 4 1 4 1 D 2

y y yD2x

v

1 yDx

. 1;1/ xCyD1

D

xyD4

1

.1;1/

T0

T 1

xyD1

x

u

x

Fig. 14.4-35

Fig. 14.4-33

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555

lOMoARcPSD|6566483

SECTION 14.4 (PAGE 842)

b) If u D y

ADAMS and ESSEX: CALCULUS 9

where S is the square 0  s  x, 0  t  x. By symmetry,

x, v D y C x then ˇ ˇ ˇ 1 1ˇ @.u; v/ ˇD D ˇˇ 1 1ˇ @.x; y/

2;



1 du dv. Also, T corresponds 2 to the triangle T 0 bounded by u D v, u D v, and v D 1. Thus

so that dA D dx dy D

I D D D D

ZZ 1 e u=v du dv 2 T0 Z v Z 1 1 e u=v du dv 2 0 v Z  ˇˇv 1 1 dv ve u=v ˇˇ 2 0 v Z 1 1 e e v dv D e e 1 2 4 0

ZZ 2 8 Erf.x/ D e  T

.s 2 Ct 2 /

ds dt;

where T is the triangle 0  s  x, 0  t  s. t

.x;x/

sDt

T x

s

1

:

Fig. 14.4-37 Now transform to polar coordinates in the st -plane. We have

36. The region R whose area we must find is shown in part (a) of the figure. The change of variables x D 3u, y D 2v maps the ellipse 4x 2 C 9y 2 D 36 to the circle u2 C v 2 D 1, and the line 2x C 3y D 1 to the line u C v D 1. Thus it maps R to the region S in part (b) of the figure. Since ˇ ˇ3 dx dy D j ˇˇ 0

the area of R is

AD

ZZ

R

Z Z x sec   2 8 =4 2 e r r dr Erf.x/ D d  0 0 Z  ˇˇx sec  4 =4 r2 ˇ d e D ˇ  0 0 Z =4   4 x 2 = cos2  D 1 e d:  0

ˇ 0 ˇˇ j du dv D 6 du dv; 2ˇ

dx dy D 6

But the area of S is .=4/ square units. y (a)

ZZ

.1=2/, so A D .3=2/

3

v

38.

R 3

1

x

a) €.x/ D

u



556

x

e 0

t2

2 dt D p 

2 4 Erf.x/ D 

ZZ

e

Z

1 2

x

e

s2

ds. Thus

0

.s 2 Ct 2 /

 

1

ds dt;

S

tx

1

t

e

, so

Let t D s 2 dt D 2s ds

dt

0

Z

D2

1

s 2x

1

e

s2

ds:

0

Z

1

e

s2

0

1 € D € 2 Z c) B.x; y/ D 3 2

Fig. 14.4-36

Z

D2 b) €

Z

x2

1 S

2 37. Erf.x/ D p 

e

 2 2 Erf.x/  1 e x p 2 Erf.x/  1 e x :

du dv:

S

(b)

x 2 = cos2 

Since cos2   1, we have e



D

tx

1

1 2 1

ds D 2

p

p  D  2

1p : 2 .1

t /y

1

dt

.x > 0; y > 0/

0

let t D cos2  , dt D 2 sin  cos  d Z =2 D2 cos2x 1  sin2y 1  d: 0

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 14.5

(PAGE 849)

z

d) If Q is the first quadrant of the st -plane,  Z 1  Z 1 2 €.x/€.y/ D 2 s 2x 1 e s ds 2 t 2y 0 0 ZZ 2 2 D4 s 2x 1 t 2y 1 e .s Ct / ds dt

1

e

t2

dt



c x y z C C D1 a b c

Q

(change to polar coordinates) Z =2 Z 1 D4 d r 2x 1 cos2x 1  r 2y 0 0 ! Z =2

D 2

0

cos2x

 Z  2

1

1

 sin2y

r

1

 d

2.xCy/ 1

r2

e

dr

0

D B.x; y/€.x C y/

R 1

1

e

r2

r dr x

 5.

R

B

Z 4 Z 0 z dz y dy x dx 0   2 1 1 4 16 1 15 D D : 2 2 2 2

xyz d V D

Z

1

3. The hemispherical dome x 2 C y 2 C z 2  4, z  0, is symmetric about the planes x D 0 and y D 0. Therefore ZZZ

D

4.

ZZZ

R

.3 C 2xy/ d V D 3

ZZZ

D

dV C 2

ZZZ

xy d V

D

2 D 3  .23 / C 0 D 16: 3

x dV D

Z

a

Z

x b 1 a

Z

x c 1 a

y b

R is the cube 0  x; y; z  1. By symmetry, ZZZ ZZZ .x 2 C y 2 / d V D 2 x2 d V R R Z 1 Z 1 Z D2 x 2 dx dy

x dx

0

x b 1 a

0

1 0

dz D

2 : 3

6.

As in Exercise 5, ZZZ ZZZ 3 .x 2 C y 2 C z 2 / d V D 3 x 2 d V D D 1: 3 R R

7.

The set R: 0  z  1 jxj jyj is a pyramid, one quarter of which lies in the first octant and is bounded by the coordinate planes and the plane x C y C z D 1. (See the figure.) By symmetry, the integral of xy over R is 0. Therefore, ZZZ ZZZ .xy C z 2 / d V D z2 d V R R Z 1 Z 1 z Z 1 z y D4 z 2 dz dy dx 0 0 0 Z 1 Z 1 z D4 z 2 dz .1 z y/ dy 0 0  Z 1  1 .1 z/2 dz D4 z 2 .1 z/2 2 0 Z 1 1 .z 2 2z 3 C z 4 / dz D D2 : 15 0

dz dy 0  Z a Z  x y Dc x dx dy 1 a b 0 0  Z a      x 2 b2 x 2 Dc x b 1 1 dx a 2b a 0 Z a x 2 bc 1 x dx Let u D 1 .x=a/ D 2 0 a du D .1=a/ dx Z a2 bc a2 bc 1 2 u .1 u/ du D : D 2 24 0 0

a

0

(page 849)

R is symmetric about the coordinate planes and has volume 8abc. Thus ZZZ .1 C 2x 3y/ d V D volume of R C 0 0 D 8abc: ZZZ

y

y

Fig. 14.5-4

€.x/€.y/ . €.x C y/

Section 14.5 Triple Integrals

2.

b x

by (a) and (c).

Thus B.x; y/ D

1.

sin2y

z 1 zD1 x y yCzD1 R 1 x

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1

xCyD1

y

Fig. 14.5-7

557

lOMoARcPSD|6566483

SECTION 14.5 (PAGE 849)

ADAMS and ESSEX: CALCULUS 9

z

8. R is the cube 0  x; y; z  1. We have ZZZ D D D

2

xyz

yz e

Z

Z

Z

1

z dz 0

R

xyz

dy . e

0

z dz 0

.1 1 e z

z 1C

3

sin.y / d V D D

Z

Z

ˇxD1 ˇ ˇ /ˇ ˇ

z

yz

e ˇ

1 y

dz

x

yD0

.1;1;0/

1/ dz

Fig. 14.5-10

ˇ1 ˇ 1 zˇ ˇ D 2 0

1 : e

3

sin.y / dy 0 1

2

Z

11.

y

dz 0

Z

R is bounded by z D 1, z D 2, y D 0, y D z, x D 0, and x D y C z. These bounds provide an iteration of the triple integral without our having to draw a diagram. ZZZ

y

dx 0

ˇ1 cos.y 3 / ˇˇ ˇ ˇ 3

3

y sin.y / dy D

z

.0;1;1/ zDy .1;1;1/

R

y xDy .1;1;0/

Fig. 14.5-9 ZZZ

R

y dV D D D D D

558

Z

1

y dy

0

Z

1

y dy

0

Z

1

0

dz

1 y Z 1

 y dy .2 

y .2

0

Z

1

Z

2 y z

dx

0

.2

0

y

z/ dz

1 y

1

0

Z

Z

1

1 2y 2 2

y/z

y/y

z2 2 1 1 2

ˇˇzD1 ˇ ˇ ˇ

zD1 y

.1

 5 : y 3 dy D 24

y/2

yCz

12. We have ZZZ cos x cos y cos z d V ZR Z  x Z  x y D cos x dx cos y dy cos z dz 0 0 0 ˇzD x y Z  Z  x ˇ D cos x dx cos y dy .sin z/ˇˇ zD0 Z0  Z0  x D cos x dx cos y sin.x C y/ dy

1

10.

dV C y C z/3 Z z Z dz dy

R .x Z 2

dx .x C y C z/3 1 0 0 ˇˇxDyCz  Z 2 Z z 1 ˇ D dz dy ˇ 2.x C y C z/2 ˇ 1 0 xD0 Z Z z dy 3 2 dz D 2 8 1 0 .y C z/ ˇˇyDz Z 2 3 1 ˇ D dz ˇ 8 1 y Cz ˇ yD0 Z 2 dz 3 3 D ln 2: D 16 1 z 16 D

0

2 : D 3

x

xCyCzD2

R yCzD1

/ dy !

ˇyD1 ˇ yz ˇ

1

0

.1;0;1/

xD0

1

0

1 0

1

Z

1

Z 1 1 C .e 2 0 1 D 1 e 2

9.

.0;1;1/

dV

R

Z

D

ZZZ

1



dy

0

1 sin.a C b/ C sin.a recall that sin a cos b D Z  Z  x h 2 i 1 D cos x dx sin.x C 2y/ C sin x dy 2 0 0 ˇˇyD  Z  cos.x C 2y/ 1 ˇ C y sin x ˇ cos x dx D ˇ 2 0 2 yD0 Z  2 cos x cos.2 x/ cos x 1 C D 2 0 2 2

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 b/ x

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INSTRUCTOR’S SOLUTIONS MANUAL

1 2

Z

!

C . 

SECTION 14.5

z

x/ cos x sin x dx

.0;1;1/

.1;0;1/

x sin 2x dx 2 U D  x d V D sin 2x dx cos 2x d U D dx V D 2 ˇ # " Z  ˇ  x 1 1 ˇ cos 2x dx cos 2x ˇ D ˇ 4 2 2 0 0 ˇ # " 1 sin 2x ˇˇ  D  D : ˇ 8 2 ˇ 8 D



.1;1;1/

0

y x .1;1;0/

Fig. 14.5-15

16.

0

z

Z 1 p 2 13. By Example 4 of Section 5.4, e u du D . If 1p p k > 0, let u D kt , so that du D k dt . Thus Z

1

e

kt2

1

r

dt D

z D y2

 : k x

ZZZ

3

e

x 2 2y 2 3y 2

ZR1

xCy D1

dV 1

e

3z 2

dz

1

ZZZ

R

f .x; y; z/ d V D D

Let E be the elliptic disk bounded by x 2 C 4y 2 D 4. Then E has area .2/.1/ D 2 square units. The volume of the region of 3-space lying above E and beneath the plane z D 2 C x is V D since

15.

ZZZ

T

RR

E

ZZ

E

.2 C x/ dA D 2

ZZ

E

D D

dA D 4 cu. units,

D

D

Z

Z

1

x dx 0 1

Z

Z

1

dy 1 x 1

Z

Z

Z

Z

Z

Z

1

dx 0 1

dy 0 1

dy 0 1

dz 0 1

dx 0

Z

Z

Z

Z

1 x

dy 0 1 y

dx 0 y2 0 1

p

Z

z

y2

f .x; y; z/ dz f .x; y; z/ dx y

f .x; y; z/ dx

.1 x/2

dz 0

p

f .x; y; z/ dx

0

Z

f .x; y; z/ dz 0

Z

0

Z

dz

y2

Z dz 0 Z 1 dy

Z

1

Z

0 1 y

D

x dA D 0 by symmetry.

x dV D

y

Fig. 14.5-16

Z 1 Z 2 2 e x dx e 2y dy 1 1 r r p    3=2 D p : D  2 3 6 D

.0; 1; 1/

x/2

x D .1

Thus

14.

(PAGE 849)

1

z

0

dx

Z

Z

1 x

p z

f .x; y; z/ dy

1 x

p

f .x; y; z/ dy: z

1

dz 2 x y

x dx .x C y 0 1 x  Z 1 .x 1/2 Cx D x 2 0 Z 1 3 1 x dx D : D 2 8 0

1/ dy  1 dx 2

Z

17. D D

1

dz

0 ZZZ

Z

0

Z

1 z

dy

0

1 0

f .x; y; z/ d V (R is the prism in the figure) Z Z 1 1 1 y dx dy f .x; y; z/ dz: R

0

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0

559

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SECTION 14.5 (PAGE 849)

ADAMS and ESSEX: CALCULUS 9

z 1

20.

.1;0;1/

yCzD1

D

R 1 x

Z

D

y

1 .1;1;0/

1

dy

0 ZZZ

Z

Z p1

18.

Z

1

Z

1

dz

x

1

dx 0

Z

p

0

0

z

xDy 2 Cz 2

y R

1

0

21.

zDy

I D

Z

1

dz 0

1 z

dy 0

Z

zD0

22.

I D

Z

1

dz 0

Z

0

1

dy z

Z

0

f .x; y; z/ dx. 0

f .x; y; z/ dy

0

(R is the tetrahedron in the figure) y

23.

f .x; y; z/ dz:

0  x  y:

I D

Z

1

dz 0

Z

1

dx z

x

Z

0

x z

f .x; y; z/ dy. 0

The given iteration corresponds to z

0  z  1;

.1;0;1/

1

24.

x y

Fig. 14.5-19

0yx

z:

I D

Z

1

dy 0

Z p1 0

0

0

0

.1;1;0/

z  x  1;

Thus 0  x  1, 0  y  x, 0  z  x y, and Z x y Z x Z 1 f .x; y; z/ dz: dy dx I D

zDx y

560

z  y  1;

Thus 0  x  1, x  y  1, 0  z  y, and Z 1 Z 1 Z y I D dx dy f .x; y; z/ dz:

x z

0

0

0

y

0  z  1; dz dx 0 z 0 ZZZ D f .x; y; z/ d V R Z x Z x Z 1 dy dx D

0  x  1:

z;

The given iteration corresponds to

Fig. 14.5-18

Z

f .x; y; z/ dx. 0

0y1

0

y yD1

yDx

1

1

Thus 0  x  1, 0  y  1 0 D 1, 0  z  1 y, and Z 1 Z 1 Z 1 y I D dx dy f .x; y; z/ dz:

xD0

.1;1;0/

Z

0  z  1;

R

Z

x

The given iteration corresponds to

.1;1;1/

x

y

Fig. 14.5-20 .0;1;1/

1

f .x; y; z/ dx

(R is the paraboloid in the figure) p Z x y2 x f .x; y; z/ dz: dy

z

Z

1

f .x; y; z/ d V R

dz dy f .x; y; z/ dx 0 z 0 ZZZ D f .x; y; z/ d V (R is the pyramid in the figure) R Z 1 Z 1 Z y D dx dy f .x; y; z/ dz: 0

19.

Z

y 2 Cz 2

0

Fig. 14.5-17

Z

y2

y2

dz

Z

1

f .x; y; z/ dx.

y 2 Cz 2

The given iteration corresponds to p 0  y  1; 0  z  1 y 2 ;

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y 2 C z 2  x  1:

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INSTRUCTOR’S SOLUTIONS MANUAL

Thus 0  x  1, 0  y  I D

25. I D

Z

Z Z

1

dy

0

1

dx

p

p x

Z

dy

1

dz

y

Z

Z px

y2

p

(PAGE 849)

z

y 2 , and

x

.1;0;1/

zDx

f .x; y; z/ dz: .1;1;1/

0

0

0

x, 0  z 

SECTION 14.5

yD0

z

yDx

R

xD1

f .x; y; z/ dx.

.1;0;0/ x

0

The given iteration corresponds to

y

0  y  1;

y  z  1;

0  x  z:

zD0

Fig. 14.5-27

Thus 0  x  1, x  z  1, 0  y  z, and Z

I D

1

dx

0

Z

1

dz x

Z

26.

.1;1;0/

28.

z

Z

1

dx 0

ZZZ

f .x; y; z/ dy:

Z

1 x

dy 0

Z

1

y

sin.z/ dz z.2 z/

sin.z/ D dV (R is the pyramid in the figure) z/ R z.2 Z z Z 1 y Z 1 sin.z/ dz dy dx D z/ 0 0 0 z.2 Z z Z 1 sin.z/ dz .1 y/ dy D z/ 0 0 z.2   Z 1 z2 sin.z/ z dz D z/ 2 0 z.2 Z 1 1 1 D sin.z/ dz D : 2 0 

0

z

.0; 1; 1/ .1; 1; 1/

z

.0;0;1/

.0; 1; 0/

x

zD1 xD0 .0;1;1/

.1;0;1/

y

yD0

Fig. 14.5-26 zDy

I D

Z

0

1

dx

Z

1

dy x

Z

y

f .x; y; z/ dz D

x

ZZZ

y

1

dz

0

27.

Z

z

yD1 x

Fig. 14.5-28 29.

z

dy

.1;0;0/

P

where P is the triangular pyramid (see the figure) with vertices at .0; 0; 0/, .0; 1; 0/, .0; 1; 1/, and .1; 1; 1/. If we we reiterate I to correspond to the horizontal slice shown then Z Z Z 1

x

f .x; y; z/ d V;

f .x; y; z/ dx:

0

Z 1 Z x 3 dz dx e x dy 0 z 0 ZZZ 3 D ex d V (R is the pyramid in the figure) R Z 1 Z x Z x 3 D e x dx dy dz 0 0 0 Z 1 e 1 3 : D x 2 e x dx D 3 0

The average value of f .x; y; z/ over R is ZZZ 1 f .x; y; z/ d V: f D volume of R R If f .x; y; z/ D x 2 C y 2 C z 2 and R is the cube 0  x; y; z  1, then, by Exercise 6, ZZZ 1 f D .x 2 C y 2 C z 2 / d V D 1: 1 R

1

30.

If the function f .x; y; z/ is continuous on a closed, bounded, connected set D in 3-space, then there exists a point .x0 ; y0 ; z0 / in D such that ZZZ f .x; y; z/ d V D f .x0 ; y0 ; z0 /  .volume of D/: D

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SECTION 14.5 (PAGE 849)

ADAMS and ESSEX: CALCULUS 9

4 Apply this with D D B .a; b; c/, which has volume  3 , 3 to get

z r 2 Cz 2 D2

ZZZ

4 f .x; y; z/ d V D f .x0 ; y0 ; z0 /  3 3 B .a;b;c/

p zD r y

for some .x0 ; y0 ; z0 / in B .a; b; c/. Thus 3 !0 4 3 lim

ZZZ

x

f .x; y; z/ d V

B .a;b;c/

Fig. 14.6-2

D lim f .x0 ; y0 ; z0 / D f .a; b; c/ !0

since f is continuous at .a; b; c/. 3.

Section 14.6 Change of Variables in Triple Integrals (page 855)

1.

V D

Z

Z

2

d 0  2a3 1 D 3

Z

=4

The paraboloids z D 10 r 2 and z D 2.r 2 1/ intersect where r 2 D 4, that is, where r D 2. The volume lying between these surfaces is V D

a

sin  d R2 dR 0  1 cu. units. p 2

0

Z

2

d 0

D 2

Z

2

Z

2

Œ10

r2

2.r 2

1/r dr

0

3r 3 / dr D 24 cu. units:

.12r

0

z

z

zD10 r 2

RDa

2

=4

y

x

zD2.r 2 1/ y

Fig. 14.6-1 Fig. 14.6-3 p

2

2

2. The surface z D r intersects the sphere r C z D 2 where r 2 C r 2 D 0. This equation has positive root r D 1. The required volume is V D D

Z

Z

2

d 0

Z

1

r dr 0

Z 1 p

2

d 0 0 Z 1 p r 2 D 2 0

D D

562

Z

2 1

p

2 r2

p r

r2

r 2 dr

dz p  r r dr  2 Let u D 2 r 2 5 du D 2r dr

4 5 p  4 4 2 D 1 5 3

u1=2 du

2  p 2 2 3

2

Z

4.

The paraboloid z D r 2 intersects the sphere r 2p C z 2 D 12 where r 4 C r 2 12 D 0, that is, where r D 3. The required volume is

V D

Z

d

0

D 2 D

22 cu. units: 15

2

D

Z

p 3

Z

0

p 3 p

p

r 12

0

Z

12

9

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r 2 dr

r2

 r 2 r dr

9 2

Let u D 12 r 2 du D 2r dr

9 2  9 p D 16 3 27 2

u1=2 du

2  3=2 12 3

12

45 cu. units. 2

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 14.6

(PAGE 855)

and between the planes y D 0 and y D x. Under the transformation

2

x D au;

y D bv;

z D cw;

R corresponds to the region S in the first octant of uvwspace, inside the sphere

zDx 2 Cy 2

u2 C v 2 C w 2 D 1; and between the planes v D 0 and bv D au. Therefore, the volume of R is ZZZ ZZZ V D dx dy dz D abc du dv dw:

x 2 Cy 2 Cz 2 D12

Fig. 14.6-4

R

Using spherical coordinates in uvw-space, S corresponds to

5. One half of the required volume V lies in the first octant, inside the cylinder with polar equation r D 2a sin  . Thus V D2

Z

D 2a

=2

d

0

Z

D 4a3

Z

=2

.2a

4a2 sin2  d

0

Z

=2

r/r dr 2 3

Z

cos 2 / d

.1 0

32a3 cu. units. 9

D 2a3

0  R  1;

2a sin 

0

S

0

 ; 2

0    tan

1

a : b

Thus

=2

8a3 sin3  d 0 Z 16a3 =2 3 sin  d 3 0

V D abc D 8.

Z

tan

1 .a=b/

d

0

1 abc tan 3

1

Z

=2

sin  d

Z

1

R2 dR

0

0

a cu. units: b

One eighth of the required volume V lies in the first octant. Call this region R. Under the transformation

z

x D au;

y D bv;

z D cw;

R corresponds to the region S in the first octant of uvwspace bounded by w D 0, w D 1, and u2 C v 2 w 2 D 1. Thus V D 8abc  .volume of S/:

zD2a r

rD2a sin 

2a y

x

The volume of S can be determined by using horizontal slices: Z 1 8  .1 C w 2 / dw D abc cu. units. V D 8abc 3 0 4

Fig. 14.6-5 z

6. The required volume V lies above z D 0, below z D 1 r 2 , and between  D =4 and  D =3. Thus Z Z =3

V D

D

1

d

=4

7 12



.1 r 2 /r dr  1 7 cu. units. D 4 48 0

1 2

a

7.

Let R be the region in the first octant, inside the ellipsoid

x

x2 y2 z2 C 2 C 2 D 1; 2 a b c

b

y

x2 y2 z2 C C D1 a2 b 2 c 2

Fig. 14.6-8

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SECTION 14.6 (PAGE 855)

ADAMS and ESSEX: CALCULUS 9

9. Let x D au, y D bv, z D w. The indicated region R corresponds to the region S above the uv-plane and below the surface w D 1 u2 v 2 . We use polar coordinates in the uv-plane to calculate the volume V of R: ZZZ ZZZ V D d V D ab du dv dw R S Z 2 Z 1 ab cu. units. D ab d .1 r 2 /r dr D 2 0 0 10.

ZZZ

15.

ZZZ

R

12.

13.

R 2

tan

Z

1 .1=c/

R 2

D D D

Z

d 0

2a5 5

2a 5

5

Z

Z

564

1 .1=c/

3

sin  d

0 tan

1 .1=c/

Z

a

1

c=

.1

p

p

17.

c=

c

C1

Z

1

.2

r dr 0

r2

p

2 r2

z dz r2

r 4 /r dr D

0

7 : 12

ZZZ

R

ZZZ

z dV Z =2 Z a D d cos  sin  d R3 dR 0 0 0   a4  1 a4 D : D 2 2 4 16

x dV D

Z

Z

d 0

Dh

R

Z

R =2

=2

Z

=2

Z

a

r dr 0

cos  d

0 =2

Z

Z

Z

0

h.1 .r=a//

r cos  dz

0 a

 r2 1

r ha3 ; dr D a 12

Z h.1 .r=a// d r dr z dz 0 0 0 Z   a r 2 h2 1 r dr D 4 0 a  ˇa r 4 ˇˇ a2 h2 h2 r 2 2r 3 C 2 ˇ D : D 4 2 3a 4a ˇ 48

z dV D

a

0

18. If

p

c c2 C 1



:

y D bv;

z D cw;

then the volume of a region R in xyz-space is abc times the volume of the corresponding region S in uvw-space. If R is the region inside the ellipsoid x2 y2 z2 C 2 C 2 D1 2 a b c

R dR Let u D cos  du D sin  d

and above the plane y C z D b, then the corresponding region S lies inside the sphere u2 C v 2 C w 2 D 1

u2 / du

ˇˇ1 ˇ ˇ p ˇ

c2

R

x D au;

c 2 C1

u3 3

0

Z

1

0

0

Z

d

Z

ZZZ

x dV D

4

cos2 / d

sin .1

 2a u D 5  2a5 2 D 5 3 5

tan

ZZZ

a

d sin  d R4 dR 0 0 0     2a5 1 2a5 D 1 cos tan 1 D 1 5 c 5 ZZZ .x 2 C y 2 / d V D

14.

Z

Z

z dV D

2

2 D 0,

By symmetry, both integrals have the same value:

R Z 2

11.

Z

D

16.

.x 2 C y 2 C z 2 / d V Z a Z h D d r dr .r 2 C z 2 / dz 0 0 0  Z a 1 r 3 h C rh3 dr D 2 3 0  4 2 3 a h a h a2 h3 a4 h D 2 C C : D 4 6 2 3 ZZZ .x 2 C y 2 / d V B Z 2 Z  Z a D d sin  d R2 sin2  R2 dR 0 0 0 Z a Z  R4 dR sin3  d D 2 0 0   5 8a5 4 a D : D 2 3 5 15 ZZZ .x 2 C y 2 C z 2 / d V B Z 2 Z  Z a 4a5 : D d sin  d R4 dR D 5 0 0 0 ZZZ .x 2 C y 2 C z 2 / d V

p z D r 2 and z D 2 r 2 intersect where r 4 C r 2 that is, on the cylinder r D 1. Thus

and above the plane bv C cw D b. The distance from the origin to this plane is c 2 C1

C

c3 3.c 2 C 1/3=2



:

DD p

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b b2

C c2

(assuming b > 0)

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 14.7

Substituting these expressions into the expression for u given in the statement of this exercise in terms of spherical coordinates, we obtain the expression in terms of cylindrical coordinates established in the previous exercise:

by Example 7 of Section 1.4. By symmetry, the volume of S is equal to the volume lying inside the sphere u2 C v 2 C w 2 D 1 and above the plane w D D. We calculate this latter volume by slicing; it is Z



1

.1

D

 w 2 / dw D  w D



2 3

w3 3

ˇˇ1 ˇ ˇ ˇ

D

D3 DC 3



@2 u 2 @u cot  @u 1 @2 u 1 @2 u C C C 2 2 C 2 2 2 2 @R R @R R @ R @ R sin  @ 2 2 2 2 1 @u @ u 1 @ u @ u C 2 2 C 2 D 2 C @r r @r r @ @z @2 u @2 u D C 2 D u @x 2 @y

:

Hence, the volume of R is abc



2 3

p

b b2 C c 2

C

by Exercise 33. b3 2 3.b C c 2 /3=2



21. cu. units:

z D z.u; v; w/;

@x @y @z ! PR D iC jC k @v @v @v @x @y @z ! PS D iC jC k @w @w @w

@2 u to both sides. @z 2

span a parallelepiped in xyz-space corresponding to a rectangular box with volume du dv dw in uvw-space. The parallelepiped has volume ˇ ˇ ˇ @.x; y; z/ ˇ ! ! ! ˇ ˇ du dv dw: j.PQ  PR/  PSj D ˇ @.u; v; w/ ˇ

20. Cylindrical and spherical coordinates are related by r D R sin :

(The  coordinates are identical in the two systems.) Observe that z; r; R, and  play, respectively, the same roles that x, y, r, and  play in the transformation from Cartesian to polar coordinates in the plane. We can exploit this correspondence to avoid repeating the calculations of partial derivatives of a function u, since the results correspond to calculations made (for a function z) in Example 10 of Section 3.5. Comparing with the calculations in that Example, we have

Thus

ˇ ˇ ˇ @.x; y; z/ ˇ ˇ ˇ du dv dw: d V D dx dy dz D ˇ @.u; v; w/ ˇ

Section 14.7 Applications of Multiple Integrals (page 864) 1.

@u @u @u D cos  C sin  @R @z @r @u @u @u D R sin  C R cos  @ @z @r 2 @ u @2 u @2 u @2 u D cos2  2 C 2 cos  sin  C sin2  2 2 @R @z @z@r @r 2 @2 u @ u @u D R C R2 sin2  2 @ 2 @R @z ! 2 @2 u 2 @ u C cos  2 : 2 cos  sin  @z@r @r

y D y.u; v; w/;

and let P be the point in xyz-space corresponding to u D a, v D b, w D c. Fixing v D b, w D c, results in a parametric curve (with parameter u) through P . The vector @x @y @z ! iC jC k PQ D @u @u @u and corresponding vectors

@2 u @2 u 1 @u 1 @2 u @2 u C D C : C @x 2 @y 2 @r 2 r @r r 2 @ 2 The required result follows if we add

Consider the transformation x D x.u; v; w/;

19. By Example 10 of Section 3.5, we know that

z D R cos ;

(PAGE 864)

@z @z D2D z D 2x C 2y; @x @y p dS D 1 C 22 C 22 dA D 3 dA ZZ SD 3 dA D 3.12 / D 3 sq. units. x 2 Cy 2 1

2.

z D .3x s

dS D

SD

1C ZZ

4y/=5;

@z 3 D ; @x 5

@z 4 D @y 5

p 32 C 42 dA D 2 dA 52 p p p 2 dA D 2.2/.1/ D 2 2 sq. units.

.x=2/2 Cy 2 1

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SECTION 14.7 (PAGE 864)

3.

zD @z D @x

p a2 p

s

x2 x

a2

ADAMS and ESSEX: CALCULUS 9

y2

x2

y2

6. ;

@z D @y

p

y a2

x2

y2

x2 C y2 a dA D p dA x2 y2 a2 x 2 y 2 ZZ a dA p (use polars) SD 2 2 2 2 a x2 y2 x Cy a Z 2 Z a r dr p Da d Let u D a2 r 2 0 0 a2 r 2 du D 2r dr Z a2 D a u 1=2 du D 2a2 sq. units.

dS D

1C

a2

D

D 2

Z

4 D p 3

=3 0

Z

0

Z

5

1

1/

sq. units.

The triangle is defined by 0  y  1, 0  x  y. p @z D 2y; dS D 1 C 4y 2 dA z D y2; @y Z 1 Z yp 1 C 4y 2 dx SD dy 0 0 Z 1 p D y 1 C 4y 2 dy Let u D 1 C 4y 2 0 du D 8y dy p  ˇ5 Z 5 1 1 2 3=2 ˇˇ 5 5 1 1=2 D u sq. units. u du D ˇ D ˇ 8 1 8 3 12 r @z 1 1 D p ; dS D 1 C dA z D x; @x 4x 2 x p r r Z 1 Z x Z 1 1 4x C 1 p SD 1C dy D x dx dx 4x 4x 0 0 0 Z 1 p 1 4x C 1 dx Let u D 4x C 1 D 2 0 du D 4 dx p  ˇ5 Z 5 1 1 2 3=2 ˇˇ 5 5 1 1=2 D u du D u sq. units. ˇ D ˇ 8 1 8 3 12 p

1

.1 C cos 2v/ dv

@z @z x @z y 3z 2 D x 2 C y 2 ; 6z D 2x; D ; D @x @x 3z @y 3z s s x2 C y2 9z 2 C 3z 2 2 dA D dA D p dA dS D 1 C 9z 2 9z 2 3 ZZ 2 24 2 p dA D p .12/ D p sq. units. SD 3 3 3 x 2 Cy 2 12

566

8.

2 dv .2 cos2 v/ p 3

ˇ=3  4 2 4 sin 2v ˇˇ D p C  sq. units. D p vC ˇ ˇ 2 3 3 3 0

5.

 16

Let u D 1 C 4r 2 du D 8r dr

1 C 4r 2 r dr

d

0

1

=3 0

x 2 Cy 2 1; x0; y0 Z 1p =2

1

7.

p z D 2 1 x2 y2 @z 2x 2y @z D p D p ; @x @y 1 x2 y2 1 x2 y2 s s 1 C 3.x 2 C y 2 / 4.x 2 C y 2 / dS D 1 C dA D dA 2 2 1 x y 1 x2 y2 ZZ SD dS x 2 Cy 2 1 s Z 2 Z 1 1 C 3r 2 r dr Let u2 D 1 r 2 D d 1 r2 0 0 u du D r dr Z 1p p 4 3u2 du Let 3u D 2 sin v D 2 p 0 3 du D 2 cos v dv

Z

u1=2 du p  ˇ5  2 3=2 ˇˇ .5 5 D u ˇ D ˇ 16 3 24

D

0

4.

@z @z D 2x; D 2y z D 1 x2 y2; @x @y p dS D 1 C 4x 2 C 4y 2 dA ZZ p SD 1 C 4.x 2 C y 2 / dA

9.

@z @z x z 2 D 4 x 2 ; 2z D 2x; D @x @x z s 2 2 2 x dA dS D 1 C 2 dA D dA D p z z 4 x2 (since z  0 on the part of the surface whose area we want to find) Z 2 Z x 2 p SD dx dy 0 0 4 x2 Z 2 2x p D dx Let u D 4 x 2 4 x2 0 du D 2x dx ˇ4 Z 4 ˇ p ˇ 1=2 D u du D 2 uˇ D 4 sq. units. ˇ 0

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 14.7

z

10. The area elements on z D 2xy and z D x 2 C y 2 , respectively, are dS1 D dS2 D

p

p

1 C .2y/2 C .2x/2 dA D

1 C .2x/2 C .2y/2 dA D

p

p

(PAGE 864)

1 C 4x 2 C 4y 2 dx dy; 1 C 4x 2 C 4y 2 dx dy:

Since these elements are equal, the area of the parts of both surfaces defined over any region of the xy-plane will be equal. 11.

p If z D 12 .x 2 C y 2 /, then dS D 1 C x 2 C y 2 dA. Oneeighth of the part of the surface above 1  x  1, 1  y  1, lies above the triangle T : given by 0  x  1, 0  y  x, or, in polar coordinates, by 0    =4, 0  r  1= cos  D sec  . Thus S D8 D8 D4

ZZ p

Z

Z

T =4

Fig. 14.7-12

d 0

sec 

0

Z

=4

d 0

p 1 C r 2 r dr

1Csec2 

p

Z  Z a AR2 dR d sin  d 2 0 0 B CR  Z a 0 B 1 D 4A dR R2 C B 0   p a units. D 4A a B tan 1 p B 2

Mass D

14.

A slice of the ball at height z, having thickness dz, is a p circular disk of radius a2 z 2 and areal density  dz. As calculated in the text, this disk attracts mass m at .0; 0; b/ with vertical force

Let u D 1 C r 2 du D 2r dr

u du

0

Z i 8 =4 h .1 C sec2  /3=2 1 d 3 0 Z 8 =4 2 D : .1 C sec2  /3=2 d 3 0 3 D

Using a TI-85 numerical integration routine, we obtain the numerical value S  5:123 sq. units. 12. As the figure suggests, the areap of the canopy is the area of a hemisphere of radius 2 minus four times the area of half of a spherical cap cut off from the sphere x 2 C y 2 C z 2 D 2 by a plane at distance 1 from the origin, p say the plane z D 1. Such a spher2 x 2 y 2 , lies above the disk ical cap, z D @z @z D x=z and D y=z x 2 C y 2  2 1 D 1. Since @x @y on it, the area of the spherical cap is ZZ

Z

13. 1 C x 2 C y 2 dA Z

y

x

x 2 Cy 2 1

p Z D 2 2

s 1

1C

x2 C y2 dA z2

r dr p 2 r2

Let u D 2 r 2 du D 2r dr p p p Z 2 1=2 u du D 2 2. 2 1/ D 4 D 2 0

p 2 2:

1

dF D 2kmdz 1

b

p a2

z

z 2 C .b

z/2

!

:

Thus the ball attracts m with vertical force Z

a

 1

b

z



p dz a2 C b 2 2bz let v D a2 C b 2 2bz; dv D 2b dz

F D 2km

a

a2 C b 2 v b 2 a2 C v zDb D 2b #2b Z .bCa/2 2 b a2 C v 1 p dv D 2km 2a 4b 2 .b a/2 v "  b 2 a2  b C a .b a/ D 2km 2a 2 2b #   1 3 3 .b C a/ .b a/ 6b 2 then b "

D

4kma3 kmM D ; 3b 2 b2

Thus the area of the canopy is p p p 1 S D 2. 2/2 4 .4 2 2/ D 4. C 2/ 8 sq. units. 2

where M D .4=3/a3  is the mass of the ball. Thus the ball attracts the external mass m as though the ball were a point mass M located at its centre.

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SECTION 14.7 (PAGE 864)

ADAMS and ESSEX: CALCULUS 9

z

z .0;0;b/ b r a

zDb

z

a

y

x ab

y

x

Fig. 14.7-14

Fig. 14.7-16 17.

15.

The force is F D 2km

Z

F D 2km

h

1 0

p

b

z

a2 C .b

z/2

!

Let u D a2 C .b z/2 du D 2.b z/ dz ! Z 2 2 1 a Cb du D 2km h p 2 a2 C.b h/2 u  p p a2 C b 2 C a2 C .b D 2km h

Z

a

 1

p

b

z



dz a2 C b 2 2bz use the same substitution as in Exercise 2) ! Z a2 Cb2 2 b a2 C v 1 p dv D 2km a 4b 2 .b a/2 v  b 2 a2 p 2 D 2km a a C b 2 .b a/ 2 2b !  1  2 2 3=2 3 .a C b / .b a/ 6b 2  p 2km  3 3 2 2 2 C b2 : D a 2b C a .2b a / 3b 2

The force is

dz

 h/2 :

0

z z

.0;0;b/

.0;0;b/ h

p

zD

z

a

a2 x 2 y 2

y

x

y

x

Fig. 14.7-15

Fig. 14.7-17 18. 16. The force is

F D 2km D 2km

Z

b

1

0

Z

0

b



 D 2kmb 1

568

1

p a2 .b

p

1

a2

b

z/2 C .b  dz

C1 : p a2 C 1 1

z z/2

!

dz

Z

Z a dy .x 2 C y 2 C z 2 / dz 0 0 0 Z a Z a Z a dz D a5 dy x 2 dx D3 0 0 0 Z a Z a Z a D x dx dy .x 2 C y 2 C z 2 / dz 0 0 0  Z a Z a a3 2 2 D x dx a.x C y / C dy 3 0 0  Z a 4 6 7a 2a C a2 x 2 x dx D : D 3 12 0

mD

MxD0

Z

a

dx

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a

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INSTRUCTOR’S SOLUTIONS MANUAL

7a . 12

Thus x D MxD0 =m D

SECTION 14.7

22. 



7a 7a 7a ; ; . 12 12 12   1 1 19. Since the base triangle has centroid ; ; 0 , the cen3 3   1 1 1 troid of the prism is ; ; . 3 3 2 By symmetry, the centre of mass is

(PAGE 864)

The cube has centroid .1=2; 1=2; 1=2/. The tetrahedron lying above the plane x C y C x D 2 has centroid .3=4; 3=4; 3=4/ and volume 1=6. Therefore the part of the cube lying below the plane has centroid .c; c; c/ and volume 5=6, where 3 1 1 5 c C  D  1: 6 4 6 2

z

1

Thus c D 9=20; the centroid is z



 9 9 9 ; ; . 20 20 20

P 1

x

y

1

1

Z

20. Volume of region D

Fig. 14.7-19 Z 1 2 d e

0

r2

0

r dr D . By

1 x

symmetry, the moments about x D 0 and y D 0 are both zero. We have MzD0 D

Z

2

d 0

D

21.

Z

1 0

Z

re

1

r dr

0 2r 2

Z

Fig. 14.7-22 e

r2

z dz

0

dr D

Z

23.

 : 4

The centroid is .0; 0; 1=4/.   a3 1 4 3 a D . By symmetry, the The volume is 8 3 6 moments about all three coordinate planes are equal. We have Z =2 Z a d sin  d R cos  R2 dR 0 0 0 Z a4 a4 =2 sin  cos  d D : D 8 0 16

MzD0 D

24.

=2

25.

Thus z D MzD0=volume D 3a=8.  3a 3a 3a ; ; The centroid is . 8 8 8 z 1

rDa2 z

26. y

x

Fig. 14.7-21

y

1

The model still involves angular acceleration to spin the ball — it doesn’t just fall. Part of the gravitational potential energy goes to producing this spin as the ball falls, even in the limiting case where the fall is vertical. I D

Z

I D

Z

Z a Z h d r 3 dr dz 0 0  4 0 ha4 a D : D 2h 4 2 p a D D I =m D p : m D a2 h; 2 Z 2 Z a Z h I D d r dr .x 2 C z 2 / dz 0 0 0  Z 2 Z a h3 r dr D d hr 2 cos2  C 3 0 0  Z 2  4 h3 a2 ha D cos2  C d 4 6 0   2  4 3 2 ha h a a h2 C C D D a2 h 4 3 4 3 s p a2 h2 D D I =m D m D a2 h; C : 4 3 2

2

0

D 2h

d Z a 0

a2 h ; mD 3

Z

a

0

r 3 dr

 r3 1

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Z

r

h.1 .r=a//

dz

0 4

a h ; dr D a 10 r p 3 D D I =m D a: 10 569

lOMoARcPSD|6566483

SECTION 14.7 (PAGE 864)

ADAMS and ESSEX: CALCULUS 9

z

The moment of inertia of the cube about this line is  Z a .x y/2 dy C z 2 dz 2 0 0 0  Z a Z a a3 a D dx .x y/2 C dy Let u D x 2 3 0 0 du D dy Z Z x a a a5 C dx D u2 du 3 2 0 x a Z a a a5 .3ax 2 3a2 x C a3 / dx C D 3 6 0   a 3a4 5a5 a5 C C a4 D ; a4 D 3 6 2 12 r p 5 m D a3 ; D D I =m D a: 12

h

I D

z r C D1 h a

a

a

x

y

Fig. 14.7-26 27.

28.

Z

Z

Z h.1 .r=a// r dr .x 2 C z 2 / dz 0 0 0 " Z 2 Z a  r 2 r cos2  D d h 1 a 0 0 # r 3 h3  1 r dr C 3 a  Z a Z r4 2h3 a  r 3 r3 D h dr C r 1 dr a 3 h 0 0 in the second integral put u D 1 .r=a/ Z 2a2 h3 1 a4 h C .1 u/u3 du D 20 3 0 a4 h 2a2 h3 a2 h D C D .3a2 C 2h2 /; 20 60 60 s p a2 h 3a2 C 2h2 ; : mD D D I =m D 3 20 ZZZ I D .x 2 C y 2 / d V I D

D 2

2

Z

3

d

Q a

m D a ;

Z

a

Z

a

30.

dy

a

dx

Z

.x

ZZZ

ZZZ

5

Q

x2 d V D

Q

xy d V D

 yz :

xz

Q

y2 d V D

Q

yz d V D

ZZZ

ZZZ

Q

z2 d V D

a5 3

Q

xz d V D

a5 : 4

ZZZ

a5 3 4



D

a5 : 6

The mass of Q is m D a3 , so the radius of gyration is DD

y x

Fig. 14.7-28

31.

29. The distance s from .x; y; z/ to the line x D y, z D 0 satisfies s 2 D u2 C z 2 , where u is the distance from .x; y; 0/ to the line x D y in pthe xy-plane. By Example 7 of Section 1.4 u D jx yj= 2, so

570

ZZZ

 2 a5 I D 3 3 3

a

2

xy

x/2

Therefore, the moment of inertia of Q about L is

a

y/2

z/2 C .z

We have

a

.x

y/2 C .y

3 2 2 2 x C y C z2 D 3

z

s2 D

a

C z2:

y

The line L through the origin parallel to the vector v D i C j C k is a diagonal of the cube Q. By Example 8 of Section 1.4, the distance from the point with position vector r D xi C yj C zk to L is s D jv  rj=jvj. Thus, the square of the distance from .x; y; z/ to L is s2 D

2a ; dz D 3 0 0 r p 2 D D I =m D a: 3

x 2 dx

0

a

Z

Z

p

a I =m D p : 6

Z b Z c dx dy .x 2 C y 2 / dz a b c  Z a 2b 3 dx D 2c 2bx 2 C 3 a 8abc 2 D .a C b 2 /; 3 s p a2 C b 2 m D 8abc; D D I =m D : 3 I D

a

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INSTRUCTOR’S SOLUTIONS MANUAL

32.

I D

Z

2

d 0

m D c.b 2

Z

c

dz 0

a2 /;

Z

SECTION 14.7

b

c.b 4 r 3 dr D 2 a s 2 2 b Ca DD : 2

a4 /

(PAGE 864)

where m is its mass. Following the method of Example 4(b), the kinetic energy of the cylinder rolling down the inclined plane with speed v is

;

1 2 mv C 2 1 D mv 2 C 2

KE D

z

1 I 2 2 3 1 2 v2 ma 2 D mv 2 : 4 a 4

c

The potential energy of the cylinder when it is at height h is mgh, so, by conservation of energy,

rDa rDb

3 2 mv C mgh D constant. 4 y

x

Differentiating this equation with respect to time t , we obtain dv dh 3 C mg 0 D mv 2 dt dt dv 3 C mgv sin ˛: D mv 2 dt

Fig. 14.7-32 33.

m D 2

Z

2

d 0

Z

a

Z

a

r dr b

p r a2

Z

p

a2 r 2

dz 0

Let u D a2 r 2 du D 2r dr Z a2 b 2 p 4 2 u du D D 2 .a b 2 /3=2 ; 3 0 p Z 2 Z a Z a2 r 2 dz I D 2 r 3 dr 0 0 Z a bp D 4 r 3 a2 r 2 dr Let u D a2 r 2 b du D 2r dr Z a2 b 2 p 2 D 2 .a u/ u du  0 2 2 2 2 2 a .a b 2 /3=2 .a b 2 /5=2 D 2 3 5 1 2 2 3=2 1 2 D 4.a b / .2a C 3b 2 / D m.2a2 C 3b 2 /: 15 5 D 4

r 2 dr

Thus the cylinder rolls down the plane with acceleration

b

z

dv 2 D g sin ˛: dt 3

35.

By Exercise 35, the ball with hole has moment of inertia I D

m .2a2 C 3b 2 / 5

about the axis of the hole. The kinetic energy of the rolling ball is 1 2 m v2 mv C .2a2 C 3b 2 / 2 2  10 a 2a2 C 3b 2 7a2 C 3b 2 2 1 : C D mv 2 D mv 2 2 10a 10a2

KE D

By conservation of energy, b

mv 2

a y

7a2 C 3b 2 C mgh D constant. 10a2

x

Differentiating with respect to time, we obtain dv 7a2 C 3b 2 mv C mgv sin ˛ D 0: 5a2 dt Fig. 14.7-33 34. By Exercise 26, the cylinder has moment of inertia I D

Thus the ball rolls down the plane (with its hole remaining horizontal) with acceleration 5a2 dv g sin ˛: D 2 dt 7a C 3b 2

ma2 a4 h D ; 2 2

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SECTION 14.7 (PAGE 864)

ADAMS and ESSEX: CALCULUS 9

36. The kinetic energy of the oscillating pendulum is KE D

1 I 2



d dt

2

where m is the mass of B and I0 is the moment about L0 . z

: L0 Lk

The potential energy is mgh, where h is the distance of C above A. In this case, h D a cos  . By conservation of energy, 1 I 2



d dt

B

2

mga cos  D constant.

x

k y

Differentiating with respect to time t , we obtain I



d dt



d 2 C mga sin  dt 2



d dt



Fig. 14.7-37

D 0;

or

mga d 2 C sin  D 0: dt 2 I For small oscillations we have sin    , and the above equation is approximated by

38.

The moment of inertia of the ball about the point where it contacts the plane is, by Example 4(b) and Exercise 39,   8 4 a5 C a3 a2 15 3   7 2 C 1 ma2 D ma2 : D 5 5

I D

d 2 C ! 2  D 0; dt 2 where ! 2 D mga=I . The period of oscillation is s I 2 T D D 2 : ! mga

The kinetic energy of the ball, regarded as rotating about the point of contact with the plane, is therefore

KE D

7 7 v2 1 I 2 D ma2 2 D mv 2 : 2 10 a 10

A 

a

39.

C

Fig. 14.7-36 37. If the centre of mass of B is at the origin, then ZZZ MxD0 D x d V D 0: B

If line L0 is the z-axis, and Lk is the line x D k, y D 0, then the moment of inertia Ik of B about Lk is ZZZ   Ik D .x k/2 C y 2  d V ZZZB D .x 2 C y 2 C k 2 2kx/  d V B

D I0 C k 2 m

572

By Example 7 of Section 1.4, the distance from the point with position vector r D xi C yj C zk to the straight line L through the origin parallel to the vector a D Ai C Bj C C k is ja  rj sD : jaj The moment of inertia of the body occupying region R about L is, therefore, 1 jaj2

ZZZ

ja  rj2  d V ZZZ h 1 .Bz Cy/2 C .C x Az/2 D 2 A C B2 C C 2 R i C .Ay Bx/2  d V h 1 .B 2 C C 2 /Pxx C .A2 C C 2 /Pyy D 2 2 2 A CB CC

I D

R

C .A2 C B 2 /Pzz

2kMxD0 D I0 C k 2 m;

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2ABPxy

2ACPxz

i 2BCPyz :

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

REVIEW EXERCISES 14

y

Review Exercises 14 (page 865)

1.

(PAGE 865)

By symmetry, ZZ

R

.x C y/ dA D 2 D2

ZZ Z

R 1

x dA D 2

.x

3=2

Z

Z

1

x dx

p x

yDx

dy

x2

0

S

3

x / dx ˇ1  x 4 ˇˇ 2 ˇ D2 4 ˇ 5

0



2 5=2 x D2 5

0

y

1 4



4.

p

Z

Z p4

3

dy

0 ZZ

x2 y2

e

y2

e

p y= 3

x2 y2

dx

dA

R

where R is as shown in the figure. y

yD x x D y2 R

a) I D D

.1; 1/

p

x

2 Fig. R-14-3

3 D 10

y D x2

p

yD

x

3x r D2

Fig. R-14-1 R 2.

ZZ

P

D

Z

Z

.x 2 C y 2 / dA D 1 0



1

Z

1

dy

0 ˇˇxD2Cy

x3 ˇ C xy 2 ˇ ˇ 3

Z

2Cy

y

.x 2 C y 2 / dx

dy

xDy

b) I D



.2 C y/3 y3 D C y 2 .2 C y/ y 3 dy 3 3 0  Z 1 8 4 8 C 4y C 4y 2 dy D C 2 C D 6 D 3 3 3 0 y

Z

dx 0

C c) I D

Z

yDx

.3; 1/

P 2 Fig. R-14-2

3.

ZZ

D

y dA D x

Z

=4

d

0

Z

x D2Cy

V D D

2

tan  r dr

0

dx

x2 y2

e

dy

0

1

=3

d e

dy

p 4 x2

Z

2

0

x2 y2

e

Z

2

r2

e

r dr

0

!ˇ2 ˇ .1 e ˇ ˇ D ˇ 2 6 r2

4

/

0

p The cone z D k x 2 C y 2 has semi-vertical angle 0 D tan 1 .1=k/. Thus the volume inside the cone and inside the sphere x 2 C y 2 C z 2 D a2 is

x

Z

2

d 0

Z

0

2a3 .1 3

0

ˇ=4 ˇ2 ˇ p r 2 ˇˇ ˇ D ln sec  ˇ ˇ D 2 ln 2 D ln 2 ˇ 2ˇ 0

5.

Z

p 3x

Z

1

 d) I D 3 .1; 1/

x

1 2 Fig. R-14-4

0

V D

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a

0

To have

0

Z

R2 dR   2a3 k : cos 0 / D 1 p 3 k2 C 1 sin  d

1 4



4 3 a 3



D

a3 ; 3

573

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REVIEW EXERCISES 14 (PAGE 865)

ADAMS and ESSEX: CALCULUS 9

we need to ensure that

8.

 2 1

p

k k2 C 1



D 1:

dV D 

p Thus k 2 C 1 D .2k/2 , and so 3k 2 D 1, and k D 1= 3.

a

0

6.

I D D

Z

2

dy

0 ZZ

y

f .x; y/ dx C

0

Z

dy 2

Z

p

6 y

f .x; y/ dx 0

dx 0

y 6

Z

6 x2

0

f .x; y/ dy: x

9.

yD6

R

x

z/2 dz 20z 3 C z 4 / dz

 50; 000 C 20; 000  78; 540 kg:

0

f .x; y/ dA;

2

is

2

.2; 2/

0

Thus the moment of inertia about the whole solid cone is Z 10 Z 2 Z .10 z/=2 I D 30z 2 dz d r 3 dr:

R

Z

dz m3 :

b) The moment of inertia (about its central axis) of the disk-shaped slice at height z is Z 2 Z .10 z/=2 dI D 30z 2 dz d r 3 dr:

where R is as shown in the figure. Thus

I D

4

a) The mass of the object Z 10  mD 30z 2 .10 4 0 Z 15 10 .100z 2 D 2 0  15 100; 000 D 2 3

z D kr

6

z/2

.10

The density of the slice is  D kz 2 kg/m3 . Since  D 3; 000 when z D 10, we have k D 30.

Fig. R-14-5 Z

A horizontal slice of the object at height z above the base, and having thickness dz, is a disk of radius r D 21 .10 z/ m. Its volume is

f .t / D

Z

a

e t

Z

x2

0

0

dx

Z Z a 1 1 a 2 f D f .t / dt D dt e x dx a 0 a 0 Z Zt Z x 1 a x2 1 a 2 D e dx xe x dx dt D a 0 a 0 0 !ˇa 2 2 e x ˇˇ 1 e a 1 D ˇ D ˇ a 2 2a a

0

yDx x Fig. R-14-6

7.

J D

Z

1

dz

0

Z

z

dy

0

Z

10. If f .x; y/ D bx C yc, then f D 0, 1, or 2, in parts of the quarter disk Q, as shown in the figure. y

3

y

f .x; y; z/ dx 0

corresponds to the region 2 0  z  1;

0  y  z;

0  x  y;

0  x  1; Thus J D

574

Z

0

1

dx

Z

x  y  1;

1

dy x

Z

f D2

1

which can also be expressed in the form y  z  1:

f D1 f D0 1

1

f .x; y; z/ dz.

Q 2 Fig. R-14-10

y

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3

x

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INSTRUCTOR’S SOLUTIONS MANUAL

REVIEW EXERCISES 14

Thus ZZ

Q

13.

f .x; y/ dA D 0 1 

and f D 11.

 2

    1 3 C1 C 2 . 2 2

5 2



5 ; 2

2/ D 2

5 . 2

D2

The sphere x 2 C y 2 C z 2 D 6a2 and the paraboloid z D .x 2 Cy 2 /=a intersect where z 2 Caz 6a2 D 0, that is, where .z C 3a/.z 2a/ D 0. Only z D 2a is possible; the plane z D 3a does not intersect the sphere. If z D 2a, 2 then x 2 C y 2 D r 2 D 6a2 4a2 D 2a p , so the intersection is on the vertical cylinder of radius 2a with axis on the z-axis. We have, ZZZ

D

D

Z

.x 2 C y 2 / d V

2

d 0

D 2

Z

Z

p 2a

0

p 2a

r 3 dr

0

 p r 3 6a2

Z

p

dz r5 a

r2



D D

Z

S

.x 2 C y 2 / d V D



0

32a 5

d 5 Z

Z

2a sin 

0 

.1

Z



d 0

r 4 dr D

Z

32a5 5

cos2  /2 sin  d

0

Z



y Cz D2 .0; 1; 1/

.0; 0; 0/

dr

r 3 dr

0

Z 32a5 1 .1 2u2 C u4 / du 5 1   1 2 512a5 64a5 C : 1 D D 5 3 5 75

D

2a sin 

.0; 0; 1/

2x C z D 2 .1; 0; 0/ x

14.

12. The solid S lies above the region in the xy-plane bounded by the circle x 2 C y 2 D 2ay, which has polar equation r D 2a p sin  , .0    /. It lies below the cone z D x 2 C y 2 D r. The moment of inertia of S about the z-axis is ZZZ

z

. 12 ; 0; 1/

Let u D 6a2 r 2 du D 2r dr Z 6a2 p  p 6 D .6a2 u/ u du . 2a/ 3a 4a2  ˇ6a2 8 5 2 5=2 ˇˇ 2 3=2 u a D  4a u ˇ ˇ 2 3 5 4a p 8 D .18 6 41/a5 15

I D

A horizontal slice of D at height z is a right triangle with legs .2 z/=2 and 2 z. Thus the volume of D is Z 7 1 1 : .2 z/2 dz D V D 4 0 12 Its moment about z D 0 is Z 1 1 MzD0 D z.2 z/2 dz 4 0 Z 1 1 11 D .4z 4z 2 C z 3 / dz D : 4 0 48 The z-coordinate of the centroid of D is , 7 11 11 zD D : 48 12 28

6a2 r 2

r 2 =a

(PAGE 865)

Z

r

dz 0

sin5  d

0

Let u D cos  du D sin  d

2x C y C z D 2

.0; 2; 0/ y

Fig. R-14-13 Z 1 Z 1 y Z 2 y 2z V D dV D dy dz dx S 0 0 0 Z 1 Z 1 y D dy .2 y 2z/ dz 0 0 Z 1 D Œ.2 y/.1 y/ .1 y/2  dy 0 Z 1 1 D .1 y/ dy D 2 0 ZZZ Z 1 Z 1 y Z 2 y 2z MxD0 D x dV D dy dz x dx S 0 0 0 Z 1 Z 1 y 1 dy Œ.2 y/2 4.2 y/z C 4z 2  dz D 2 0 0 Z " 1 1 .2 y/2 .1 y/ 2.2 y/.1 y/2 D 2 0 # 4 3 C .1 y/ dy Let u D 1 y 3 du D dy  Z 1 1 4 D .u C 1/2 u 2.u C 1/u2 C u3 du 2 0 3  Z  1 1 1 3 7 D u C u du D 2 0 3 24 , 7 1 7 D xD 24 2 12 ZZZ

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ADAMS and ESSEX: CALCULUS 9

z

The area of that part of the paraboloid is Z =2 Z 2 cos  p SD d 1 C 4r 2 r dr Let u D 1 C 4r 2 =2 0 du D 8r dr Z 1C16 cos2  Z 1 =2 u1=2 du d D 8 =2 1 Z 1 =2 2 Œ.1 C 16 cos2  /3=2 1 d D 4 0 3 Z 1 =2 D Œ.1 C 16 cos2  /3=2 1 d 6 0  7:904 sq. units.

.0; 0; 1/ y Cz D1 S

.0; 1; 0/ 2

x

y

.1; 1; 0/

.2; 0; 0/

xD2

y

2z

Fig. R-14-14

15.

ZZZ

Z

1

Z

1Cz

Z

(using a TI-85 numerical integration function).

z dV D z dz dy 0 0 0 Z 1Cz D z dz .1 C z y/ dy 0 0  Z 1  .1 C z/2 dz D z .1 C z/2 2 0 Z 1 17 1 .z C 2z 2 C z 3 / dz D D 2 0 24 z S

Z

1

y2 z2 x2 C C D 1 18. The region R inside the ellipsoid 36 9 4 and above the plane x C y C z D 1 is transformed by the change of variables

1Cz y

dx

x D 6u;

to the region S inside the sphere u C v 2 C w 2 D 1 and above the plane 6u C 3v C 2w D 1. The distance from the origin to this plane is DD p

y D 1Cz .0; 1; 0/

.1; 0; 0/ x

D

1 ; 7

1=7

Since [email protected]; y; z/[email protected]; v; w/j D 6  3  2 D 18, the volume of R is 18  .180=343/ D 3240=343  29:68 cu. units.

y xCy

1 62 C 32 C 22

so, by symmetry, the volume of S is equal to the volume inside the sphere and above the plane w D 1=7, that is,  ˇ1 Z 1 w 3 ˇˇ 180 2 .1 w / dw D  w D units3 . ˇ 3 ˇ 343 1=7

.0; 2; 1/

S

z D 2w 2

.0; 0; 1/

.2; 0; 1/

y D 3v;

zD1

Challenging Problems 14 (page 866) Fig. R-14-15

1.

16. The plane z D 2x intersects the paraboloid z D x 2 C y 2 on the circular cylinder x 2 C y 2 D 2x, (that is, .x 1/2pC y 2 D 1), which p has radius 1. Since dS D 1 C 22 dA D 5 dA on the plane, the area of the part of the plane inside p the paraboloid (and therefore 5 times the area of a circle of inside the cylinder) is p radius 1, that is, 5 square units. 17.

As noted in the previous exercise, the part of the paraboloid z D x 2 C y 2 that lies below the plane z D 2x is inside the vertical cylinder x 2 C y 2 D 2x, which has polar equation r D 2 cos  . =2    =2/. On the paraboloid: dS D

576

p p 1 C .2x/2 C .2y/2 dA D 1 C 4r 2 r dr d:

This problem is similar to Review Exercise 18 above. The x2 y2 z2 region R inside the ellipsoid 2 C 2 C 2 D 1 and above a b c y z x the plane C C D 1 is transformed by the change of a b c variables x D au; y D bv; z D cw to the region S inside the sphere u2 C v 2 C w 2 D 1 and above the plane u C v C w D 1. The distance from the 1 origin to this plane is p , so, by symmetry, the volume 3 of S is equal to the p volume inside the sphere and above the plane w D 1= 3, that is,  ˇ1 Z 1 w 3 ˇˇ 2 w / dw D  w ˇ p .1 3 ˇ p 1= 3 1 3 p 2.9 4 3/ cu. units. D 27

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INSTRUCTOR’S SOLUTIONS MANUAL

CHALLENGING PROBLEMS 14

Since [email protected]; p y; z/[email protected]; v; w/j D abc, the volume of R is 2.9 4 3/ abc cu. units. 27 2. The plane .x=a/ C .y=b/ C .z=c/ D 1 intersects the ellipsoid .x=a/2 C .y=b/2 C .z=c/2 D 1 above the region R in the xy-plane bounded by the ellipse x2 y2  C C 1 a2 b2

Remark: The series for 1=.1 xy/ converges for jxyj < 1.R Therefore the outer integral is improper (i.e., c analysis of the limc!1 0 dx). We cannot do a detailedP convergence here, but the convergence of 1=n2 shows that the iterated double integral must converge. b) Similarly, 1 X 1 . xy/n D 1 xy C .xy/2    D 1 C xy nD1 Z 1Z 1 dx dy 1 C xy 0 0 Z 1 Z 1 1 X x n 1 dx y n 1 dy D . 1/n 1

y 2 D 1; b

x a

or, equivalently, y2 xy x2 C 2 C 2 a b ab

x a

y D 0: b

SD D

s

1C

R p a2 b 2

c2 c2 C dx dy a2 b2

C a2 c 2 C b 2 c 2 .area of R/: ab

2

2

v/2 C .u2

v2/

3u C v 2u D 0   2 1 1 3 u2 uC C v2 D 3 9 3 v2 .u 1=3/2 C D 1; 1=9 1=3

.u C v/

.u

v/ D 0

D 4.

we have

Z

0

1

Z

1 0

1 X 1 D 1 C xy C .xy/2 C    D .xy/n 1 xy nD1 Z 1 1 Z 1 X dx dy x n 1 dx D y n 1 dy 1 xy 0 0

D

nD1 1 X

nD1

1 : n2

yn

nD1 1 X

nD1

0

. 1/n n3

1

dy

0

1

dx

Z

1 0

Z

1

zn

1

dz

0

yn

1

dy

Z

1

zn

1

dz

0

1

:

Under the transformation u D a  r, v D b  r, w D c  r, where r D xi C yj C zk, the parallelepiped P corresponds to the rectangle R specified by 0  u  d1 , 0  v  d2 , 0  w  d3 . If a D a1 iCa2 jCa3 k and similar expressions hold for b and c, then ˇ ˇ ˇ a1 a2 a3 ˇ ˇ ˇ @.u; v; w/ D ˇˇ b1 b2 b3 ˇˇ D a  .b  c/: @.x; y; z/ ˇ c1 c2 c3 ˇ

Therefore

2 p 2 2 SD p a b C a2 c 2 C b 2 c 2 sq. units. 3 3 a)

1

dx dy 1 C xyz 0 0 0 Z 1 1 X . 1/n 1 xn D

p p an ellipse with area .1=3/.1= 3/ D =.3 3/ sq. units. Since ˇ ˇ ˇa a ˇ ˇ j du dv D 2ab du dv; dx dy D j ˇˇ b bˇ

3.

nD1 0 1 X

1

0

1 n3 nD1 Z 1Z 1Z 1 D

Under the transformation x D a.u C v/, y D b.u v/, R corresponds to the ellipse in the uv-plane bounded by .u C v/2 C .u

0

nD1 1 X

. 1/n 1 n2 nD1 Z 1Z 1Z 1 dx dy xyz 0 1 0 0 Z 1 Z 1 X D x n 1 dx D

Thus the area of the part of the plane lying inside the ellipsoid is ZZ

(PAGE 866)

1

ˇ ˇ ˇ @.x; y; z/ ˇ ˇ du dv dw D du dv dw ; dx dy dz D ˇˇ @.u; v; w/ ˇ ja  .b  c/j and we have ZZZ .a  r/.b  r/.c  r/ dx dy dz P ZZZ uvw D du dv dw R ja  .b  c/j Z d2 Z d3 Z d1 1 u du v dv w dw D ja  .b  c/j 0 0 0 2 2 2 d1 d2 d3 D : 8ja  .b  c/j

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CHALLENGING PROBLEMS 14

(PAGE 866)

ADAMS and ESSEX: CALCULUS 9

we have 5. The volume V0 removed from the ball is eight times the part in the first octant, which is itself split into two equal parts by the plane x D y: V0 D 16 D 16 D8

Z

Z

Z

1

dx 0 =4

Z

0

d

0

0

d

=4

p 4

x

Z

Z

sec 

x2 p

4

y 2 dy r 2 r dr

0

4

Let u D 4 r 2 du D 2r dr

u1=2 du

4 sec2 

Z i 16 =4 h 8 .4 sec2  /3=2 d 3 0 Z 32 16 =4 .4 cos2  1/3=2 D d: 3 3 0 cos3  D

7.

Now the volume of the whole ball is .4=3/23 D 32=3, so the volume remaining after the hole is cut is 32 V0 3 Z =4 16 .3 4 sin2  /3=2 cos  d D 3 0 .1 sin2  /2 Z p 16 1= 2 .3 4v 2 /3=2 D dv: 3 0 .1 v 2 /2

Z

Z  Z a1=3 cos2  sin2  d sin5  cos2  d R8 dR 0 0 0 Z 2 Z  sin2 .2 / D 3a3 d .1 cos2 /2 cos2  sin  d 4 0 0 Let t D cos , dt D sin  d Z 2 Z 1 1 cos.4 / D 3a3 d .1 t 2 /2 t 2 dt 8 0 1 Z 1 4a3 3a3 .2/2 cu. units. .t 2 2t 4 C t 6 / dt D D 8 35 0

V D 27

2

One-eighth of the required volume lies in the first octant. Under the transformation x D u6 , y D v 6 , z D w 6 , the region first-octant R bounded by the surface x 1=3 C y 1=3 C z 1=3 D a1=3 and the coordinate planes gets mapped to the first octant part B of the ball bounded by u2 C v 2 C w 2  a1=3 . Assume that a > 0. Since @.x; y; z/ D 63 u5 v 5 w 5 ; @.u; v; w/

V D

Let v D sin  dv D cos  d

V D 8.63 /

We submitted this last integral to Mathematica to obtain V D

4 32sin 3

1

11tan

r

1

2 3

23=2 C 11tan

1

3

3

6. Under the transformation x D u , y D v , z D w 3 , the region R bounded by the surface x 2=3 C y 2=3 C z 2=3 D a2=3 gets mapped to the ball B bounded by u2 C v 2 C w 2 D a2=3 . Assume that a > 0. Since @.x; y; z/ D 27u2 v 2 w 2 ; @.u; v; w/ the volume of R is V D 27

Now switch to spherical coordinates ŒR; ;   in uvwspace. Since

we have V D 1; 728

Z

Z

=2 0



Z

.cos  sin  /5 d

a1=6

u v w du dv dw:

B

Z

=2

.sin2  cos /5 sin  d

0

R17 dR

0 =2

Z =2 sin5 .2 / sin11 .1 sin2 /2 cos  d d 32 0 0 Let s D sin , ds D cos  d Z =2 Z 1 D 3a3 .1 cos2 .2 //2 sin.2 / d s 11 .1 s 2 /2 ds D 96a3

0

2

Now switch to spherical coordinates ŒR; ;   in uvwspace. Since

0

Let t D cos.2 /, dt D 2 sin.2 / d Z Z 1 3a3 1 .1 2t 2 C t 4 / dt .s 11 2s 13 C s 15 / ds D 2 1 0    1 1 1 1 a3 2 C C D cu. units. D 3a3 1 3 5 12 7 16 210

uvw D .R sin  cos  /.R sin  sin  /.R cos /;

578

u5 v 5 w 5 du dv dw:

B

uvw D .R sin  cos  /.R sin  sin  /.R cos /;

!

2 2

ZZZ

23=2 /

.3

.3 C 23=2 /  18:9349:

ZZZ

the required volume is

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 15.1

CHAPTER 15. VECTOR FIELDS

4.

F D i C sin xj. The field lines satisfy dx D

dy . sin x

dy Thus D sin x. The field lines are the curves dx y D cos x C C .

Section 15.1 Vector and Scalar Fields (page 873) 1.

(PAGE 873)

y

F D xi C xj.

dy dx D , i.e., dy D dx. The field The field lines satisfy x x lines are y D x C C , straight lines parallel to y D x. y

x

x

Fig. 15.1-4

5. Fig. 15.1-1

F D ex i C e

x

j.

The field lines satisfy

dx dy D x. ex e

dy D e 2x . The field lines are the curves dx 1 2x e C C. yD 2

2. F D xi C yj.

Thus

dx dy The field lines satisfy D . x y Thus ln y D ln x C ln C , or y D C x. The field lines are straight half-lines emanating from the origin.

y

y

x x

Fig. 15.1-5 Fig. 15.1-2 3. F D yi C xj.

dx dy The field lines satisfy D . y x Thus x dx D y dy. The field lines are the rectangular hyperbolas (and their asymptotes) given by x 2 y 2 D C .

6.

F D r.x 2

y/ D 2xi j. dx dy The field lines satisfy D . They are the curves 2x 1 1 ln x C C . yD 2

y

y

x

x

Fig. 15.1-3

Fig. 15.1-6

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SECTION 15.1 (PAGE 873)

7.

ADAMS and ESSEX: CALCULUS 9

2xi C 2yj . x2 C y2 dx dy The field lines satisfy D . Thus they are radial x y lines y D C x (and x D 0)

x C C2 . The streamlines C1 are the spirals in which the surfaces x D C1 sin.z C2 / intersect the cylinders x 2 C y 2 D C12 . This implies that z D sin

F D r ln.x 2 C y 2 / D

y

12. v D

1

xi C yj . .1 C z 2 /.x 2 C y 2 /

dx dy D . Thus x y z D C1 and y D C2 x. The streamlines are horizontal half-lines emanating from the z-axis.

The streamlines satisfy dz D 0 and x

13.

v D xzi C yzj C xk. The field lines satisfy dx dy dz D D ; xz yz x

Fig. 15.1-7 8. F D cos yi

or, equivalently, dx=x D dy=y and dx D z dz. Thus the field lines have equations y D C1 x, 2x D z 2 C C2 , and are therefore parabolas.

cos xj.

dy dx D , that is, cos y cos x cos x dx C cos y dy D 0. Thus they are the curves sin x C sin y D C .

The field lines satisfy

14.

v D e xyz .xi C y 2 j C zk/. The field lines satisfy dy dz dx D 2 D ; x y z

y

so they are given by z D C1 x, ln jxj D ln jC2 j equivalently, x D C2 e 1=y ). x

15.

v.x; y/ D x 2 i yj. The field lines satisfy dx=x 2 D dy=y, so they are given by ln jyj D .1=x/ C ln jC j, or y D C e 1=x .

16.

v.x; y/ D xi C .x C y/j. The field lines satisfy dy dx D x xCy xCy dy D dx x

Fig. 15.1-8

Let y D xv.x/ dv dy DvCx dx dx x.1 C v/ dv D D 1 C v: vCx dx x

9. v.x; y; z/ D yi yj yk. The streamlines satisfy dx D dy D dz. Thus y C x D C1 , z C x D C2 . The streamlines are straight lines parallel to i j k. 10. v.x; y; z/ D xi C yj

xk. dy dz dx D D . Thus The streamlines satisfy x y x z C x D C1 , y D C2 x. The streamlines are straight halflines emanating from the z-axis and perpendicular to the vector i C k.

11.

v.x; y; z/ D yi

xj C k. dx dy The streamlines satisfy D D dz. Thus y x x dx C y dy D 0, so x 2 C y 2 D C12 . Therefore, dz 1 1 : D D q dx y C12 x 2 580

.1=y/ (or,

Thus dv=dx D 1=x, and so v.x/ D ln jxj C C . The field lines have equations y D x ln jxj C C x. 17.

F D rO C r O . The field lines satisfy dr D d , so they are the spirals r D  C C .

18. F D rO C  O . The field lines satisfy dr D r d= , or dr=r D d= , so they are the spirals r D C  . 19.

F D 2Or C  O . The field lines satisfy dr=2 D r d= , or dr=r D 2d= , so they are the spirals r D C  2 .

20.

F D r rO O . The field lines satisfy dr=r D r d , or dr=r 2 D d , so they are the spirals 1=r D  C C , or r D 1=. C C /.

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INSTRUCTOR’S SOLUTIONS MANUAL

21.

If V .x; y/ D V .x; y/ D x

x2

2 1 2y

SECTION 15.2

xy C y 2 , then C > 0 except at .0; 0/ and

If x 2 < 1=2, then 1 Therefore, dV > x2 C y2 dt

Section 15.2 Conservative Fields (page 882)

3 2 4y

 dV D .2x y/y C .2y x/ x C y.1 dt D y 2 C x 2 C 2y 2 .1 x 2 / xy.1 x 2 > 1=2 and jxy.1 

jxyj D jxj

jyj 2

2

 x2/

x 2 /:

x 2 /j  jxyj.

1.

F D xi have

2yj C 3zk, F1 D x, F2 D

22. For  D 0 the corresponding vector field is F D yi For V .x; y/ D x 2 C y 2 we have

Therefore, F may be conservative. If F D r, then

V 0 D 2rr 0 D 2y 2 .x 2 1/  0 when jxj < 1, thus r.t / is a decreasing function except at critical points where y D 0, which is the nullcline for x 0 D 0. Since r(t) decreases to the critical point and continues to decrease after passing the critical point, the concavity has to be opposite in sign on opposite sides of the critical point. Thus the critical points of r.t / are also points of inflection, so they do not halt the asymptotic decline in distance to (0,0). Therefore the fixed point is asymptotically stable.

25. x 0 D y 0 D 0 occurs at .0; 0/ confirming that the origin is a fixed point. Then V is positive and it vanishes at .0; 0/. d V =dt D x.x 0 /Cy.y 0 / D x.y/Cy. x x 2 y/ D x 2 y 2 : If  > 0 then V 0 < 0 except at the origin. Thus the origin is stable. However if  < 0 then V 0 > 0 trajectories are away from the origin and it is an unstable point. Thus the sign of  determines stability. 26.

F D x 0 i C y 0 j D yi .x C x 2 y/j: x 0 D 0 implies y D 0 as a nullcline, for vertical vectors, while y 0 D 0 implies x D 0 and y D =x are nullclines for horizontal vectors.

2y;

@ D 3z: @z

x2 3z 2 y2 C is a potential for F. 2 2 3 Thus F is conservative on R . Evidently .x; y; z/ D

2xy D 0:

2.

F D yi C xj C z 2 k, F1 D y, F2 D x, F3 D z 2 . We have

23. The second nullcline corresponds to y 0 D 0, that is x . x C y.x 2 1/ D 0, or y D 2 x 1 24.

@ D @y

@ D x; @x

xj.

All trajectories are everywhere tangent to the level curves of V . Thus the trajectories are circles about .0; 0/ and the fixed point is weakly stable, but not asymptotically stable. For  D 0, the Van der Pol equation is just the equation of simple harmonic motion.

2y, F3 D 3z. We

@F1 @F2 D0D ; @y @x @F1 @F3 D0D ; @z @x @F2 @F3 D0D : @z @y

3y 2 C >0 4

provided .x; y/ ¤ .0; 0/. This implies that the trajectories of F cross all the level curves of V that are sufficiently close to the origin (they are ellipses) in an outward direction, so the origin is an unstable fixed point of F and therefore of the Van der Pol equation with  D 1.

dV D rV  F D 2xy dt

(PAGE 882)

@F2 @F1 D1D ; @y @x @F3 @F1 D0D ; @z @x @F2 @F3 D0D : @z @y Therefore, F may be conservative. If F D r, then @ D y; @x

@ D x; @y

@ D z2: @z

Therefore,

.x; y; z/ D

Z

y dx D xy C C1 .y; z/

@ @C1 @C1 DxC ) D0 @y @y @y C1 .y; z/ D C2 .z/; .x; y; z/ D xy C C2 .z/ xD

z2 D

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@ z3 D C20 .z/ ) C2 .z/ D : @z 3

581

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SECTION 15.2 (PAGE 882)

Thus .x; y; z/ D xy C conservative on R3 .

3. F D

ADAMS and ESSEX: CALCULUS 9

z3 is a potential for F, and F is 3

xi yj x , F1 D 2 , F2 D x2 C y2 x C y2 @F1 D @y

2xy ; .x 2 C y 2 /2

Therefore, .x; y; z/ D

y . We have x2 C y2

@F2 2xy : D 2 @x .x C y 2 /2

@F2 2xy D : .x 2 C y 2 /2 @x

6.

2

2

Z

@ y : D 2 @y x C y2

x ln.x 2 C y 2 / dx D C C1 .y/ 2 Cy 2 @ y y D D 2 C c10 .y/ ) c10 .y/ D 0: 2 2 x Cy @y x C y2

@F2 @F1 2 2 2 D 2xyze x Cy Cz D ; @y @x @F1 2 2 2 D .x C 2xz 2 /e x Cy Cz ; @z @F3 @F1 2 2 2 D .y C 2x 2 y/e x Cy Cz ¤ : @x @z

x2

Thus F cannot be conservative. 7.

Thus we can choose C1 .y/ D 0, and .x; y/ D

1 ln.x 2 C y 2 / 2

D

z 2 /i C .2yz C x 2 /j .2zx y 2 /k, z 2 , F2 D 2yz C x 2 , F3 D y 2 2zx. We have

@r .r r0 /  2 @x jr r0 j3 jr r0 j 2.x x0 / : jr r0 j4

F D r D D

@ D 2yz C x 2 ; @y

h 2 .x jr r0 j4 r r0 : 2 jr r0 j4

x0 /i C .y

y0 /j C .z

i z0 /k

This is the vector field whose scalar potential is .

Therefore, F may be conservative. If F D r, then

582

r0 j

Since similar formulas hold for the other first partials of , we have

@F1 @F2 D 2x D ; @y @x @F3 @F1 D 2z D ; @z @x @F2 @F3 D 2y D : @z @y

@ D 2xy z 2 ; @x @ D y 2 2zx: @z

1 jr r0 j2 @ @ 2 D jr 3 @x jr r0 j @x

.r/ D

D

is a scalar potential for F, and F is conservative everywhere on R2 except at the origin. 5. F D .2xy F1 D 2xy

2

F D e x Cy Cz .xzi C yzj C xyk/. 2 2 2 2 2 2 F1 D xze x Cy Cz , F2 D yze x Cy Cz , x 2 Cy 2 Cz 2 F3 D xye . We have

Therefore, .x; y/ D

xz 2 C C1 .y; z/

Thus .x; y; z/ D x 2 y xz 2 C y 2 z is a scalar potential for F, and F is conservative on R3 .

Therefore, F may be conservative. If F D r, then x @ ; D 2 @x x C y2

z 2 / dx D x 2 y

@C1 @ D x2 C @y @y @C1 ) D 2yz ) C1 .y; z/ D y 2 z C C2 .z/ @y .x; y; z/ D x 2 y xz 2 C y 2 z C C2 .z/ @ D 2xz C y 2 C C20 .z/ y 2 2zx D @z ) C20 .z/ D 0:

xi C yj x y , F1 D 2 , F2 D 2 . We have x2 C y2 x C y2 x C y2 @F1 D @y

.2xy

2yz C x 2 D

Thus F cannot be conservative. 4. F D

Z

8.

@r @ 1 r  @x x ln jrj D D 2 @x jrj jrj jrj xi C yj C zk r r ln jrj D D 2: 2 jrj jrj

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 15.2

2y x2 C y2 2x iC j k, z z z2 2y x2 C y2 2x . We have , F2 D , F3 D F1 D z z z2

9. F D

@F1 @F2 D0D ; @y @x @F3 2x @F1 D D ; @z z2 @x @F3 2y @F2 D D : @z z2 @y

or x 2 C y 2 C 2z 2 D B, where B is a second arbitrary constant. The field lines of F are the ellipses in which the vertical planes containing the z-axis intersect the ellipsoids x 2 C y 2 C 2z 2 D B. These ellipses are orthogonal to all the equipotential surfaces of F. 2x 2y x2 C y2 k D G C k, iC j z z z2 where G is the vector field F of Exercise 9. Since G is conservative (except on the plane z D 0), so is F, which has scalar potential

10. F D

Therefore, F may be conservative in R3 except on the plane z D 0 where it is not defined. If F D r, then @ 2x D ; @x z

@ 2y D ; @y z

@ D @z

x2 C y2 : z2

Therefore, Z

x2 2x .x; y; z/ D dx D C C1 .y; z/ z z 2y @ @C1 y2 D D ) C1 .y; z/ D C C2 .z/ z @y @y z x2 C y2 C C2 .z/ .x; y; z/ D z 2 2 x Cy @ x2 C y2 D D C C20 .z/ z2 @z z2 ) C2 .z/ D 0: x2 C y2 is a potential for F, and F is z 3 conservative on R except on the plane z D 0.

Thus .x; y; z/ D

The equipotential surfaces have equations x2 C y2 D C; z

or

C z D x2 C y2:

Thus the equipotential surfaces are circular paraboloids. The field lines of F satisfy dx dy D D 2x 2y z z

dz : x C y2 z2 2

dx dy D , so y D Ax for an x y arbitrary constant A. Therefore

so

z dz D .x 2 C y 2 /

z dz ; C A2 /

x 2 .1

2

.1 C A /x dx D 2z dz. Hence 1 C A2 2 B x C z2 D ; 2 2

.x; y; z/ D

x2 C y2 x2 C y2 C z2 Cz D ; z z

x2 C y2 is a potential for G and z is a potential for z the vector k. since

The equipotential surfaces of F are .x; y; z/ D C , or x2 C y2 C z2 D C z which are spheres tangent to the xy-plane having centres on the z-axis. The field lines of F satisfy dy dx D D 2x 2y 1 z z

dz : x2 C y2 z2

As in Exercise 9, the first equation has solutions y D Ax, representing vertical planes containing the z-axis. The remaining equations can then be written in the form dz z2 D dx

x2 y2 z2 D 2xz

.1 C A2 /x 2 : 2zx

This first order DE is of homogeneous type (see Section 9.2), and can be solved by a change of dependent variable: z D xv.x/. We have dz x 2 v 2 .1 C A2 /x 2 dv D D dx dx 2x 2 v dv v 2 .1 C A2 / v 2 C .1 C A2 / x D vD dx 2v 2v 2v dv dx D v 2 C .1 C A2 / x   2 2 ln v C .1 C A / D ln x C ln B vCx

From the first equation,

dx D 2x

(PAGE 882)

B x z2 B 2 C1CA D x2 x z 2 C x 2 C y 2 D Bx: v 2 C 1 C A2 D

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SECTION 15.2 (PAGE 882)

ADAMS and ESSEX: CALCULUS 9

These are spheres centred on the x-axis and passing through the origin. The field lines are the intersections of the planes y D Ax with these spheres, so they are vertical circles passing through the origin and having centres in the xy-plane. (The technique used to find these circles excludes those circles with centres on the y-axis, but they are also field lines of F.) Note: In two dimensions, circles passing through the origin and having centres on the x-axis intersect perpendicularly circles passing through the origin and having centres on the y-axis. Thus the nature of the field lines of F can be determined geometrically from the nature of the equipotential surfaces. 11.

The scalar potential for the two-source system is .x; y; z/ D .r/ D

jr

m `kj

m : jr C `kj

Hence the velocity field is given by v.r/ D r.r/ m.r `k/ m.r C `k/ D C jr `kj3 jr C `kj3 m.xi C yj C .z C `/k/ m.xi C yj C .z `/k/ C 2 : D 2 Œx C y 2 C .z `/2 3=2 Œx C y 2 C .z `/2 3=2 Observe that v1 D 0 if and only if x D 0, and v2 D 0 if and only if y D 0. Also v.0; 0; z/ D m



z ` zC` C jz `j3 jz C `j3



k;

which is 0 if and only if z D 0. Thus v D 0 only at the origin. At points in the xy-plane we have v.x; y; 0/ D

Thus, the speed in the xy-plane is greatest at points of the circle x 2 C y 2 D `2 =2. 12. The scalar potential for the source-sink system is 2 1 .x; y; z/ D .r/ D C : jrj jr kj Thus, the velocity field is r k 2r v D r D 3 jrj jr kj3 xi C yj C .z 1/k 2.xi C yj C zk/ : D 2 .x C y 2 C z 2 /3=2 .x 2 C y 2 C .z 1/2 /3=2 For vertical velocity we require 2x x D 2 ; 2 2 2 3=2 2 .x C y C z / .x C y C .z 1/2 /3=2 and a similar equation for y. Both equations will be satisfied at all points of the z-axis, and also wherever  3=2  3=2 2 x 2 C y 2 C .z 1/2 D x2 C y2 C z2   22=3 x 2 C y 2 C .z 1/2 D x 2 C y 2 C z 2 x 2 C y 2 C .z 2=3

K/2 D K 2

K;

2=3

where K D 2 =.2 1/. This latter equation represents a sphere, S, since K 2 K > 0. The velocity is vertical at all points on S, as well as at all points on the z-axis. Since the source at the origin is twice as strong as the sink at .0; 0; 1/, only half the fluid it emits will be sucked into the sink. By symmetry, this half will the half emitted into the half-space z > 0. The rest of the fluid emitted at the origin will flow outward to infinity. There is one point where v D 0.pThis point (which is easily calculated to be .0; 0; 2 C 2/) lies inside S. Streamlines emerging from the origin parallel to the xy-plane lead to this point. Streamlines emerging into z > 0 cross S and approach the sink. Streamlines emerging into z < 0 flow to infinity. Some of these cross S twice, some others are tangent to S, some do not intersect S anywhere.

2m.xi C yj/ : C y 2 C `2 /3=2

z

.x 2

The velocity is radially away from the origin in the xy-plane, as is appropriate by symmetry. The speed at .x; y; 0/ is v.x; y; 0/ D where s D

p

p 2ms 2m x 2 C y 2 D 2 D g.s/; .x 2 C y 2 C `2 /3=2 .s C `2 /3=2 x 2 C y 2 . For maximum g.s/ we set

0 D g 0 .s/ D 2m D

584

3 2 s.s C `2 /1=2 2s 2 .s 2 C `2 /3

.s 2 C `2 /3=2

2m.`2 2s 2 / : .s 2 C `2 /5=2

x

Fig. 15.2-12

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 15.2

13. Fluid emitted by interval z in time interval Œ0; t  occupies, at time t , a cylinder of radius r, where

Now 2y @r 2xy @ D 3 D @x r @x r4 y r 2 2yr 2 @ x2/ r D .y D  : 4 4 @y r r Thus   2xyi C .y 2 F D r D 2 .x C y 2 /2

 r 2 Z D vol. of cylinder D 2 mt z: dr Thus r 2 D 2mt , and r D m. The surface of this dt cylinder is moving away from the z-axis at rate dr m m ; D D p dt r x2 C y2

16.

so the velocity at any point .x; y; z/ is

m  unit vector in direction xi C yj x2 C y2 m.xi C yj/ D : x2 C y2

vD p

14.

For v.x; y/ D

@v2 2mxy D ; .x 2 C y 2 /2 @x

so v may be conservative, except at .0; 0/. We have Z

m x dx D ln.x 2 C y 2 / C C1 .y/ x2 C y2 2 @ my dC1 my D D 2 C : x2 C y2 @y x C y2 dy

.x; y/ D m

Thus we may take C1 .y/ D 0, and obtain .x; y/ D

m ln.x 2 C y 2 / D m ln jrj; 2

as a scalar potential for the velocity field v of a line source of strength of m. 15.

The two-dimensional dipole of strength  has potential .x; y/ D

D

D D

   !  !# m ` 2 ` 2 2 2 lim ln x C y C ln x C y `!0 2 2 2 m`D   2 ! 2 ! ` ` ln x 2 C y C ln x 2 C y 2 2  lim 2 `!0 ` (apply l’H^opital’s Rule)     ` ` y yC  2 2 lim 2    2 `!0 ` ` 2 x2 C y x2 C y C 2 2 y y D : x2 C y2 r2

 x 2 /j :

The equipotential curves for the two-dimensional dipole have equations y D 0 or 1 y D x2 C y2 C x 2 C y 2 C Cy D 0   2 C 2 C 2 D : x2 C y C 2 4

m.xi C yj/ , we have x2 C y2 @v1 D @y

(PAGE 882)

These equipotentials are circles tangent to the x-axis at the origin. 17.

All circles tangent to the y-axis at the origin intersect all circles tangent to the x-axis at the origin at right angles, so they must be the streamlines of the two-dimensional dipole. As an alternative derivation of this fact, the streamlines must satisfy dx dy D 2 ; 2xy y x2 or, equivalently, y2 x2 dy D : dx 2xy This homogeneous DE can be solved (as was that in Exercise 10) by a change in dependent variable. Let y D xv.x/. Then dy v2x2 x2 dv D D dx dx 2vx 2 2 dv v 1 v2 C 1 x D vD dx 2v 2v dx 2v dv D v2 C 1 x 2 ln.v C 1/ D ln x C ln C

"

vCx

C ) x x2 C y2 D C x v2 C 1 D

.x

C y2 C1D x2 x

C /2 C y 2 D C 2 :

These streamlines are circles tangent to the y-axis at the origin.

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SECTION 15.2 (PAGE 882)

ADAMS and ESSEX: CALCULUS 9

18. The velocity field for a point source of strength m dt at .0; 0; t / is   m xi C yj C .z t /k v t .x; y; z/ D  3=2 : x 2 C y 2 C .z t /2 Hence we have Z 1 v t .x; y; z/ dt 1 Z 1 xi C yj C .z t /k Dm  3=2 dt 1 x 2 C y 2 C .z t /2 Z 1 dt D m.xi C yj/  3=2 1 2 2 x C y C .z t /2 p Let z t D x 2 C y 2 tan  p dt D x 2 C y 2 sec2  d Z m.xi C yj/ =2 cos  d D x2 C y2 =2 2m.xi C yj/ D ; x2 C y2

Also,

xi C yj D .cos  /i C .sin  /j r yi C xj O D D .sin  /i C .cos  /j: r rO D

Therefore, @ 1 @ O rO C  @r  r @  @ @ D cos2  C sin  cos  i @x @y   @ @ C sin2  j C cos  sin  @x @y   @ @ C sin2  sin  cos  i @x @y   @ @ C cos  sin  C cos2  j @x @y @ @ D iC j D r: @x @y

20.

If F D Fr .r;  /Or C F .r;  /O is conservative, then F D r for some scalar field .r;  /, and by Exercise 19,

which is the velocity field of a line source of strength 2m along the z-axis. The definition of strength of a point source in 3-space was made to ensure that the velocity field of a source of strength 1 had speed 1 at distance 1 from the source. This corresponds to fluid being emitted from the source at a volume rate of 4. Similarly, the definition of strength of a line source guaranteed that a source of strength 1 gives rise to fluid speed of 1 at unit distance 1 from the line source. This corresponds to a fluid emission at a volume rate 2 per unit length along the line. Thus, the integral of a 3-dimensional source gives twice the volume rate of a 2-dimensional source, per unit length along the line.

@ D Fr ; @r

For the equality of the mixed second partial derivatives of , we require that @Fr @ @F D .rF / D F C r ; @ @r @r that is, 21.

The potential of a point source m dt at .0; 0; t / is .x; y; z/ D

p

m x 2 C y 2 C .x

t /2

:

This potential cannot be integrated to give the potential for a line source along the z-axis because the integral Z 1 dt p m 1 x 2 C y 2 C .z t /2 does not converge, in the usual sense in which convergence of improper integrals was defined.

19. Since x D r cos  and y D r sin  , we have @ @ @ D cos  C sin  @r @x @y @ @ @ D r sin  C r cos  : @ @x @y

586

1 @ D F : r @

@Fr @

r

@F D F . @r

If F D r sin.2 /Or C r cos.2 /O D r.r;  /, then we must have 1 @ @ D r sin.2 /; D r cos.2 /: @r r @ Both of these equations are satisfied by .r / D

1 2 r sin.2 / C C; 2

so F is conservative and this  is a potential for it. 22.

If F D r 2 cos  rO C ˛r ˇ sin  O D r.r;  /, then we must have 1 @ @ D r 2 cos ; D ˛r ˇ sin : @r r @ From the first equation .r;  / D

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r3 cos  C C. /: 3

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 15.3

The second equation then gives C 0 . /

Thus Z

r3 @ sin  D D ˛r ˇ C1 sin : 3 @

z ds D

C

Section 15.3 Line Integrals

(page 887)

C is given by r D at i C bt j C ct k;

0  t  m. Thus

dr D ai C bj C ck ˇ dtˇ p ˇdrˇ ˇ ˇ D a2 C b 2 C c 2 ˇ dt ˇ Z Z m p .x C y/ ds D .at C bt / a2 C b 2 C c 2 dt C 0 Z m p t dt D .a C b/ a2 C b 2 C c 2 0 p .a C b/ a2 C b 2 C c 2 2 D m 2 2

4.

q ds D a .cos2 t sin2 t /2 C 4 sin2 t cos2 t C sin2 t dt p D a cos2 2t C sin2 2t C sin2 t dt p D a 1 C sin2 t dt:

Z

Z

1 0

p 1 C u2 du

=4

Let u D sin t du D cos t dt

Let u D tan  du D sec2  d

sec3  d

0

C: x D t cos t , y D t sin t , z D t , .0  t  2/. We have p .cos t t sin t /2 C .sin t C t cos t /2 C 1 dt p D 2 C t 2 dt:

ds D Thus Z

C

z ds D

Z

D

1 2

2

t 0

Z

p 2 C t 2 dt

2C4 2

Let u D 2 C t 2 du D 2t dt

u1=2 du

2

ˇ2C4 2 1 3=2 ˇˇ .2 C 4 2 /3=2 D u ˇ D ˇ 3 3

23=2

:

2

5.

Wire: r D 3t i C 3t 2 j C 2t 3 k;

.0  t  1/

v D 3i C 6t j C 6t 2 k p v D 3 1 C 4t 2 C 4t 4 D 3.1 C 2t 2 /: If the wire has density ı.t / D 1 C t g/unit length, then its mass is mD3

Z

0

1

.1 C 2t 2 /.1 C t / dt

ˇ1  2t 3 t 4 ˇˇ t2 C C D3 tC ˇ D 8 g: 2 3 2 ˇ

3. C: r D a cos t sin t i C a sin2 t j C a cos t k, 0  t  =2. Since

for all t , C must lie on the sphere of radius a centred at the origin. We have

0

ˇ iˇ=4 a2 h ˇ sec  tan  C ln j sec  C tan j ˇ D ˇ 2 0  2 p p a D 2 C ln.1 C 2/ : 2

2. C is given by r D t i C t j C t k, for 0  t  1. Thus

jrj2 D a2 .cos2 t sin2 t C sin4 t C cos2 t / D a2

p a cos t a 1 C sin2 t dt

=2

D a2

2

dr D 2t i C j C 2t k ˇ dtˇ p p ˇdrˇ ˇ ˇ D 4t 2 C 1 C 4t 2 D 1 C 8t 2 ˇ dt ˇ Z Z 1 p Let 1 C 8t 2 D u t 1 C 8t 2 dt y ds D 0 C Z 9 p 1 D u du 16 1 ˇ 1 2 3=2 ˇˇ9 27 1 13 D  u ˇ D D 16 3 24 12 1

Z

D a2

This equation can be solved for a function C. / independent of r only if ˛ D 1=3 and ˇ D 2. In this case, C. / D C (a constant). F is conservative if ˛ and ˇ have these values, and a potential for it is  D 13 r 3 cos  C C .

1.

(PAGE 887)

0

6.

The wire of Example 3 lies in the first octant on the surfaces z D x 2 and z D 2 x 2 2y 2 , and, therefore, also on the surface x 2 D 2 x 2 2y 2 , or x 2 C y 2 D 1, a circular cylinder. Since it goes from .1; 0; 1/ to .0; 1; 0/ it can be parametrized r D cos t i C sin t j C cos2 k; .0  t  =2/ v D sin t i C cos t j 2 cos t sin t k q p v D 1 C sin2 .2t / D 2 cos2 .2t /:

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SECTION 15.3 (PAGE 887)

ADAMS and ESSEX: CALCULUS 9

Since the wire has density ı D xy D sin t cos t D its mass is 1 mD 2 D

1 4

Z

1 2

Thus ds D

sin.2t /,

0

Z

p 2

p

1

cos2 .2t / sin.2t / dt

v 2 dv D

2

1

t

1 2

Z

1

p

2

Let v D cos.2t / dv D 2 sin.2t / dt

D

v 2 dv;

p

p

ds D

1 C 2e 2t dt:

C

Z

2

et

0

1 D p 2

Z

p 1 C 2e 2t dt

tD2

11.

r D cos t i C sin t j C t k;

588

MxD0 MyD0

tD0

r D 3t i C t j

2t k;

.0  t  1/:

.0  t  2/:

.0  t  2/ p 2:

p Z 2 p 2 t dt D 2 2 2 0 p Z 2 t cos t dt D 0 D 2 0 Z 2 p p t sin t dt D 2 2 D 2 0 p p Z 2 2 8 3 2 t dt D D 2 : 3 0

mD

sec3  d

9. The line of intersection of the planes x y C z D 0 and x C y C 2z D 0 from .0; 0; 0/ to .3; 1; 2/ can be parametrized

0

p 9t 2 dt D 3 14:

v D sin t i C cos t j C k; v D If the density is ı D z D t , then

p Let 2e t D tan  p t 2e dt D sec2  d

ˇ iˇtD2 1 h ˇ D p sec  tan  C ln j sec  C tan  j ˇ ˇ 2 2 tD0 ˇ2 p t p p tp 2t 2e 1 C 2e C ln. 2e C 1 C 2e 2t / ˇˇ p D ˇ ˇ 2 2 0 p p 2 4 e 1 C 2e 3 D 2 p p 2e 2 C 1 C 2e 4 1 p p : C p ln 2 2 2C 3

1

p p sin2 t C 4 sin2 t cos2 t C cos2 t dt D 1 C sin2 2t dt:

8. C is the same curve as in Exercise 5. We have e z ds D

Z

We have Z p 1 C 4x 2 z 2 ds C Z 2 p p D 1 C 4 cos2 t sin2 t 1 C sin2 2t dt 0 Z 2 D .1 C sin2 2t / dt 0  Z 2  1 cos 4t 1C D dt 2 0 3 D .2/ D 3: 2

sin t /2 C e 2t .sin t C cos t /2 C 1 dt

3

14

Thus

t

e 2t .cos t

p

r D cos t i C cos2 t j C sin t k;

0

The moment of inertia of C about the z-axis is Z I D ı .x 2 C y 2 / ds C Z 2 p Dı e 2t 1 C 2e 2t dt Let u D 1 C 2e 2t 0 du D 4e 2t dt Z 1C2e4 p ı D u du 4 3 ˇ1C2e4 ˇ i ıh ı ˇ .1 C 2e 4 /3=2 33=2 : D D u3=2 ˇ ˇ 6 6 Z

x 2 ds D

10. The curve C of intersection of x 2 C z 2 D 1 and y D x 2 can be parametrized

C: r D e cos t i C e sin t j C t k, 0  t  2/. ds D

14 dt and

Z

C

=2

which is the same integral obtained in Example 3, and has value . C 2/=8. 7.

p

MzD0

(We have omitted the details of the  evaluationof these 1 4 ; . integrals.) The centre of mass is 0;  3 12. Here the wire of Exercise 9 extends only from t D 0 to t D : p p Z  2 2 mD 2 t dt D 2 0 Z  p p MxD0 D 2 t cos t dt D 2 2 0 p Z  p MyD0 D 2 t sin t dt D  2 0 p p Z  2 3 2 : MzD0 D 2 t dt D 3 0

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 15.3



 4 2 2 ; ; . 2  3 p r D e t i C 2t j C e t k; .0  t  1/ p v D e t i C 2j e t k p v D e 2t C 2 C e 2t D e t C e t Z Z 1 .x 2 C z 2 / ds D .e 2t C e 2t /.e t C e t / dt C 0 Z 1 .e 3t C e t C e t C e 3t / dt D

The centre of mass is 13.

0 3

D mD

14.

Z

1

e Ce 3

1 e

.e t C e t / dt D

e

Hence ds D We have Z 17.

1 : 3e 3

2

Z

.0  t  =2/:

C

D a2

Z

=2

cos t 0

Z

tD=2

p 1 C sin2 t dt

tD0

ˇ iˇ=2 p p a ˇ 2 2 D sin t 1 C sin t C ln j sin t C 1 C sin t j ˇ ˇ 2 0 i 2 hp p a D 2 C ln.1 C 2/ : 2 2h

16. On C, we have zD

p 1

x2

y2 D

p 1

x2

x/2 D

.1

Thus C can be parametrized r D t i C .1

t /j C

p 2.t

t 2 /k;

p 2.x

.0  t  1/:

x 2 /:

0

p

2.t

dt t 2/ p D 1: 2.t t 2 /

x/2 D z 2 D x 2 C y 2 D x 2 C t 2 1

2x D t 2

)

xD

1

t2

r D t i C t 2 j C t 4 k; .0  t  2/: p Since ds D 1 C 4t 2 C 16t 6 dt , we have Z Z 2 p xyz ds D t 7 1 C 4t 2 C 16t 6 dt: C

19.

tD0

ˇ iˇtD=2 a2 h ˇ D sec  tan  C ln j sec  C tan  j ˇ ˇ 2

1

18. C: y D x 2 , z D y 2 , from .0; 0; 0/ to .2; 4; 16/. Parametrize C by

Let sin t D tan  cos t dt D sec2  d

sec3  d

Z

dt .1 2t /2 dt D p : 2.t t 2 / 2.t t 2 /

2 1 C t2 : ) zD1 xD 2 p p Thus ds D t 2 C 1 C t 2 dt D 1 C 2t 2 dt , and Z 1 p Z 1 C 2t 2 ds D dt 2 3=2 2 .2t C 1/3=2 C .2y C 1/ Z11 dt D2 1 C 2t 2 0 ˇ p ˇ1 p  p  D 2 tan 1 . 2t /ˇˇ D 2 D p : 2 2 0

p We have ds D a 1 C sin2 t dt , so x ds D a2

z ds D

)

1

r D a cos t i C a sin t j C a cos t k;

1C1C

The parabola z 2 D x 2 Cy 2 , xCz D 1, can be parametrized in terms of y D t since

1

The first octant part C of the curve x 2 C y 2 D a2 , z D x, can be parametrized

15.

C

s

.1

e e2 C 1 MxD0 D e t .e t C e t / dt D 2 0 p Z 1p 2.e 1/ 2 t t MyD0 D 2t .e C e / dt D e 0 Z 1 2 3e 1 MzD0 D e t .e t C e t / dt D 2 2e 0 ! p e 3 C e 2 2 3e 2 1 The centroid is ; ; . 2e 2 2 e C 1 2e 3 2e 0

Z

(PAGE 887)

0

Helix: x D a cos t , y D b sin t , z D ct .0 < a < b/. p ds D a2 sin2 t C b 2 cos2 t C c 2 dt q D c 2 C b 2 .b 2 a2 / sin2 t dt p p b 2 a2 D b 2 C c 2 1 k 2 sin2 t dt .k 2 D 2 /: b C c2

One complete revolution of the helix corresponds to 0  t  2, and has length Z 2 p p L D b2 C c 2 1 k 2 sin2 t dt 0 Z =2 p p D 4 b2 C c 2 1 k 2 sin2 t dt 0 1 0s 2 2 p p b a A units: D 4 b 2 C c 2 E.k/ D 4 b 2 C c 2 E @ b2 C c 2

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SECTION 15.3 (PAGE 887)

ADAMS and ESSEX: CALCULUS 9

The length of the part of the helix from t D 0 to t D T < =2 is LD D

Z p b2 C c 2

T 0

p 1

5.

k 2 sin2 t dt 0s

p p b 2 C c 2 E.k; T / D b 2 C c 2 E @

Z

1

b 2 a2 A ; T units. b2 C c 2

20. The straight line L with p equation p Ax C By D C , .C ¤ 0/, lies at distance D D jC j= A2 C B 2 from the origin. So does the line L1 with equation y D D. Since x 2 C y 2 depends only on distance from the origin, we have, by symmetry, Z

Z ds ds D L1 x 2 C y 2 L x2 C y2 Z 1 dx D 2 C D2 x 1 ˇ1 ˇ 2  2 1 x ˇ tan D ˇ D D Dˇ D 2 p 0 2 2   A CB D D : D jC j

6.

0



7.

C

2.

r D t i C t 2 j; .0  t  1/: Z 1 F  dr D Œt 3 t 2 .2t / dt D 0

 yj D r sin x

Z

 y2 F D cos xi : 2 C W y D sin x from (0,0) to .; 0/. ˇ.;0/  Z y 2 ˇˇ F  d r D sin x D 0: ˇ 2 ˇ C

F D yi C zj xk: C W r D t i C t j C t k; Z Z 1 F  dr D .t C t C

C

F  dr D

W D

0

t 3 dt D

1 : 4

8.

C

Z

1

C

Œt 3

0

2D

.0;0;0/

F  dr D



x2 C z2 C y.x 2

Z

Z

2. 3/

x 2 y 2 dx C x 3 y dy D 0

C2

x 2 y 2 dx C x 3 y dy D

ZC3

x 2 y 2 dx C x 3 y dy D 2 2

ˇˇ.0; ˇ z/ ˇ ˇ

2;3/

.1;0; 1/

19 .1 C 0/ D units: 2

C1

C4

0

590

Z

Z

0

t 2 .2t / C 2t .3t 2 / dt ˇ1 Z 1 5 5t 4 ˇˇ 3 D 5t dt D ˇ D : 4 ˇ 4 0

F  dr D

ˇˇ.1;1;1/ ˇ D1 .x C y/z ˇ ˇ

x2 C y2 2

C is made up of four segments as shown On C1 , y D 0, dy D 0, and x goes from On C2 , x D 1, dx D 0, and y goes from On C3 , y D 1, dy D 0, and x goes from On C4 , x D 0, dx D 0, and y goes from Thus

4. F D zi yj C 2xk: C: r D t i C t 2 j C t 3 k, .0  t  1/. Z



9 D 2 1

0 D 0:

F D .x C y/i C .x z/j C .z y/k   2 x C z2 C y.x z/ : Dr 2 The work done by F in moving an object from .1; 0; 1/ to .0; 2; 3/ is

.0  t  1/: ˇ1 1 t 2 ˇˇ t / dt D ˇ D : 2ˇ 2

0

. 1;0;0/

z/i C .y z/j .x C y/k  x2 C y2 .x C y/z : Dr 2 C is a given polygonal path from (0,0,0) to (1,1,1) (but any other piecewise smooth path from the first point to the second would do as well).

.0;0/

3.

ˇ.1;0;0/ ˇ ˇ F  d r D xyz ˇ D0 ˇ C



x 2 j:

F D xyi CW Z

F D .x

Z

Section 15.4 Line Integrals of Vector Fields (page 894) 1.

F D yzi C xzj C xyk D r.xyz/. C: a curve from . 1; 0; 0/ to .1; 0; 0/. (Since F is conservative, it doesn’t matter what curve.)

Z

in the figure. 0 to 1. 0 to 1. 1 to 0. 1 to 0.

1

y dy D

0

Z

0

1

1 2

x 2 dx D

1 3

3

x y dx C x y dy D 0:

Finally, therefore, Z

C

x 2 y 2 dx C x 3 y dy D 0 C

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1 2

1 1 C0D : 3 6

1:

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 15.4

y

C3

If A D 2 and B D 3, then F D r where  D x 2 ln z C y 3 z. If C is the straight line x D t C 1, y D 1, z D t C 1, .0  t  1/, from .1; 1; 1/ to .2; 1; 2/, then

.1;1/

C2

Z

C4

2x ln z dx C 2y 2 z dy C y 3 dz Z Z x2 dz D r  d r y 2 z dy C z C C ˇ.2;1;2/ Z ˇ 1 ˇ D .x 2 ln z C y 3 z/ˇ Œ.t C 1/.0/ C .t C 1/ dt ˇ 0 .1;1;1/ ˇˇ1  2 t 1 ˇ C t ˇ D 4 ln 2 : D 4 ln 2 C 2 1 ˇ 2 2 C

C1 x

Fig. 15.4-8 9. Observe that if  D e xCy sin.y C z/, then   r D e xCy sin.y C z/i C e xCy sin.y C z/ C cos.y C z/ j

0

C e xCy cos.y C z/k:

Thus, for any piecewise smooth path from .0; 0; 0/ to 1; 4 ; 4 , we have Z

C

12.

F D .y 2 cos x C z 3 /i C .2y sin x

C e xCy cos.y C z/ dz

ˇ.1;=4;=4/ ˇ ˇ D r  d r D .x; y; z/ˇ D e 1C.=4/ : ˇ C

W D

.0;0;0/

,

aD2

,

bD1

,

0 D 0:

C

,

0D0

,

AD2

,

B D 3:

ˇ.=2; ˇ 4y C 2z/ˇˇ

1;2/

.0;1; 1/

0

0 C 4 C 2 D 15 C 4:

.2x sin.y/

e z / dx

i C .x 2 cos.y/ 3e z / dy xe z dz Z Z   D r x 2 sin.y/ xe z  d r 3 e z dy C

C

Z 1 ˇˇ.1;1;ln 2/ 3 D x 2 sin.y/ xe z ˇˇ .1 C x/ dx 0 .0;0;0/  ˇ1 9 13 x 2 ˇˇ D 2 3 xC D : ˇ D 2 2 ˇ 2 2 

@C1 C x 2 D F2 D x 2 ) C1 .y; z/ D C2 .z/ @y dC2 C x D F3 D x C 2z ) C2 .z/ D z 2 C C: dz

@F2 @F1 D @y @x @F1 @F3 D @z @x @F2 @F3 D @z @y

F  dr

For z D ln.1 C x/, y D x, from x D 0 to x D 1, we have Z h

If a D 2 and b D 1, then F D r where Z  D .2xy C z/ dx D x 2 y C xz C C2 .y; z/

11.

C

D 1 C 4 C 4 C 4 13.

Thus  D x 2 y C xz C z 2 C C is a potential for F.  2  x F D Ax ln zi C By 2 zj C C y 3 k is conservative if z

Z

D .y 2 sin x C xz 3

10. F D .axy C z/i C x 2 j C .bx C 2z/k is conservative if @F2 @F1 D @y @x @F3 @F1 D @z @x @F3 @F2 D @z @y

4/j C .3xz 2 C 2/k

D r.y 2 sin x C xz 3 4y C 2z/: The curve C: x D sin 1 t , y D 1 2t , z D 3t 1, .0  t  1/, goes from .0; 1; 1/ to .=2; 1; 2/. The work done by F in moving a particle along C is

  e xCy sin.y C z/ dx C e xCy sin.y C z/ C cos.y C z/ dy

Z

(PAGE 894)

0

14.

a) S D f.x; y/ W x > 0; y  0g is a simply connected domain. b) S D f.x; y/ W x D 0; y  0g is not a domain. (It has empty interior.) c) S D f.x; y/ W x ¤ 0; y > 0g is a domain but is not connected. There is no path in S from . 1; 1/ to .1; 1/.

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591

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SECTION 15.4 (PAGE 894)

ADAMS and ESSEX: CALCULUS 9

d) S D f.x; y; z/ W x 2 > 1g is a domain but is not connected. There is no path in S from . 2; 0; 0/ to .2; 0; 0/. e) S D f.x; y; z/ W x 2 C y 2 > 1g is a connected domain but is not simply connected. The circle x 2 C y 2 D 2, z D 0 lies in S, but cannot be shrunk through S to a point since it surrounds the cylinder x 2 C y 2  1 which is outside S.

18. C is made up of four segments as shown On C1 , y D 0, dy D 0, and x goes from On C2 , x D 1, dx D 0, and y goes from On C3 , y D 1, dy D 0, and x goes from On C4 , x D 0, dx D 0, and y goes from I

f) S D f.x; y; z/ W x 2 C y 2 C z 2 > 1g is a simply connected domain even though it has a ball-shaped “hole” in it. 15.

I

C

C

x dy D

I

C

C

x dy D y dx D

Z

2

0

Z

C1

Z

I

C

x dy D

C

y dx D

D0C0C

C

x dy D

a sin t . a sin t / dt D

C3

C4

dx C 0 D

1

1:

.1;1/

C2

C1 x

Fig. 15.4-18

a cos t b cos t dt D ab 2

b sin t . a sin t / dt D

ab:

C1

x dy C Z



Z

x dy

C2

a2 ; D0C a2 cos2 t dt D 2 0 I Z Z y dx D y dx C y dx C1

D0C

Z

0

C2



. a2 cos2 t / dt D

a2 : 2

C is made up of three segments as shown in the figure. On C1 , y D 0, dy D 0, and x goes from 0 to a. On C2 , y D bt , x D a.1 t /, and t goes from 0 to 1. On C3 , x D 0, dx D 0, and y goes from b to 0. I

C

x dy D

Z

C1

C Z

Z

C2

C

1

Z

C3

ab D0C a.1 t / b dt C 0 D 2 0Z I Z Z y dx D C C C

C1

D0C

y

Z

0

C2

C3

1

bt . a dt / C 0 D

y b

C2

C3 C1 a

C2 C1

ax

a

Fig. 15.4-17

592

C4

0

a :

2

0

C

Z

C4

0

Z

Z

C3

C consists of two parts: On C1 , y D 0, dy D 0, and x goes from a to a. On C2 , x D a cos t , y D a sin t , t goes from 0 to . I

C3

C

2

19. 17.

1

Z

y

2

Z

Z

C2

C

C2

16. C is the curve r D a cos t i C b sin t j, .0  t  2/. I

Z

C1

a cos t a cos t dt D a2

0

C

D0C dy C 0 C 0 D 1 0Z Z Z Z y dx D C C C

C is the curve r D a cos t i C a sin t j, .0  t  2/. I

Z

in the figure. 0 to 1. 0 to 1. 1 to 0. 1 to 0.

Fig. 15.4-19

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x

ab : 2

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 15.4

20. Conjecture: If D is a domain in R2 whose boundary is a closed, non-self-intersecting curve C, oriented counterclockwise, then I x dy D area of D; IC y dx D area of D:

22.

a) C: x D a cos t , x D a sin t , 0  t  2. 1 2

Proof for a domain D that is x-simple and y-simple: Since D is x-simple, it can be specified by the inequalities c  y  d; f .y/  x  g.y/:

y

Z

C2

C3

d

C4

Z

1

I

C

y dx D

C4 C1 a

1 x

1 x

C3 C2

1

Fig. 15.4.22(a)

Fig. 15.4.22(b)

c

D0C g.y/ dy C 0 C f .y/ dy c d   D g.y/ f .y/ dy D area of D: The proof that

y

C

Let C consist of the four parts shown in the figure. On C1 and C3 , dy D 0. On C2 , x D g.y/, where y goes from c to d . On C2 , x D f .y/, where y goes from d to c. Thus I Z Z Z Z x dy D C C C C1

I

x dy y dx 2 2 C x Cy Z 2 2 a cos2 t C a2 sin2 t 1 dt D 1: D 2 0 a2 cos2 t C a2 sin2 t

C

C

(PAGE 894)

(area of D) is similar, and

uses the fact that D is y-simple.

b) See the figure. C has four parts. On C1 , x D 1, dx D 0, y goes from 1 to 1. On C2 , y D 1, dy D 0, x goes from 1 to 1. On C3 , x D 1, dx D 0, y goes from 1 to 1. On C4 , x D 1, dx D 0, y goes from 1 to 1.

y

C3 xDf .y/

C2 C4

D

C1

c

xDg.y/

x

21.

Fig. 15.4-20     @g @f @g @f r.fg/ D C f C g iC f C g j @x @x @y @y   @g @f C f C g k @z @z D grf C f rg: Thus, since C goes from P to Q, Z Z f rg  d r C grf  d r C C ˇQ Z ˇ ˇ D r.fg/  d r D .fg/ˇ ˇ C

I

x dy y dx x2 C y2 "Z Z 1 1 1 dy dx D C 2 C1 2 1 1 C y 2 x 1 # Z 1 Z 1 dx dy C 2 2 1 x C1 1 1Cy Z 1 2 dt D  1 1 C t2 ˇ1 ˇ 2 2   1 ˇ D tan t ˇ D C D ˇ   4 4

1 2

d

C

1:

1

y

C2 C4 C3 2

C1 1

1

2

x

P

D f .Q/g.Q/

f .P /g.P /:

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Fig. 15.4-22

593

lOMoARcPSD|6566483

SECTION 15.4 (PAGE 894)

ADAMS and ESSEX: CALCULUS 9

c) See the figure. C has four parts. On C1 , y D 0, dy D 0, x goes from 1 to 2. On C2 , x D 2 cos t , y D 2 sin t , t goes from 0 to . On C3 , y D 0, dy D 0, x goes from 2 to 1. On C4 , x D cos t , y D sin t , t goes from  to 0. I 1 x dy y dx 2 C x 2 C y 2 " Z  1 4 cos2 t C 4 sin2 t dt D 0C 2 2 2 0 4 cos t C 4 sin t # Z 0 cos2 t C sin2 t dt C0C 2 2  cos t C sin t 1 D . / D 0: 2

we have 1 2

C

x dy y dx 1 D x2 C y2 2

I

C

r  d r

ˇtDb ˇ 1 ˇ D w.C/: .x; y/ˇ D ˇ 2 tDa

Section 15.5 Surfaces and Surface Integrals (page 905) 1.

The polar curve r D g. / is parametrized by x D g. / cos ;

y D g. / sin :

Hence its arc length element is

23. Although @ @y



y x2 C y2



@ D @x



x x2 C y2

s

 2  2 dy dx ds D C d d d r  2  2 D g 0 . / cos  g. / sin  C g 0 . / sin  C g. / cos  d r   



for I all .x; y/ ¤ .0; 0/, Theorem 1 does not imply that x dy y dx is zero for all closed curves C in R2 . 2 2 C x Cy The set consisting of points in R except the origin is not simply connected, and the vector field FD

2

D

g. /

C g 0 . /

2

d:

The area element on the vertical cylinder r D g. / is

yi C xj x2 C y2

r

2  2 g. / C g 0 . / d dz:

dS D ds dz D

is not conservative on any domain in R2 that contains the origin in its interior. (See Example 5.) However, the integral will be 0 for any closed curve that does not contain the origin in its interior. (An example is the curve in Exercise 22(c).) 24.

I

2.

The area element dS is bounded by the curves in which the coordinate planes at  and  C d and the coordinate cones at  and  C d intersect the sphere R D a. (See the figure.) The element is rectangular with sides a d and a sin  d . Thus

If C is a closed, piecewise smooth curve in R2 having equation r D r.t /, a  t  b, and if C does not pass through the origin, then the polar angle function    D  x.t /; y.t / D .t / can be defined so as to vary continuously on C. Therefore,

dS D a2 sin  d d: z 

ˇtDb ˇ ˇ .x; y/ˇ D 2  w.C/; ˇ

d a sin 

tDa

where w.C/ is the number of times C winds around the origin in a counterclockwise direction. For example, w.C/ equals 1, 1 and 0 respectively, for the curves C in parts (a), (b) and (c) of Exercise 22. Since

dS a  y

@ @ r D iC j @x @y yi C xj D 2 ; x C y2

594

x

d

Fig. 15.5-2

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 15.5

3. The plane Ax C By C C z D D has normal n D Ai C Bj C C k, and so an area element on it is given by jnj dS D dx dy D jn  kj

p

z 2a

z 2 D4a2 x 2 y 2

A2 C B 2 C C 2 dx dy: jC j

Hence the area S of that part of the plane lying inside the elliptic cylinder

2a

y2 x2 C 2 D1 2 a b

y 2a

x

rD2a sin 

is given by

Fig. 15.5-4 p

ZZ

SD

A2 C B 2 C C 2 dx dy jC j

x2 y2 C 1 a2 b 2 p ab A2 C B 2

D

jC j

C C2

5.

sq. units.

6. 4. One-quarter of the required area is shown in the figure. It lies above the semicircular disk R bounded by x 2 C y 2 D 2ay, or, in terms of polar coordinates, r D 2a sin  . On the sphere x 2 C y 2 C z 2 D 4a2 , we have 2z

@z D @x

2x;

or

@z D @x

x : z

y @z D , so the surface area element on the @y z sphere can be written s

1C

x2 C y2 2a dx dy dx dy D p : 2 z 4a2 x 2 y 2

S D4

2a dx dy p 2 4a x2 y2 R Z =2 Z 2a sin  r dr D 8a d p 0 0 4a2 r 2 Z =2 Z 4a2 D 4a d u 1=2 du

D 8a

y2

Z

2a

p

Z p4a2

a dy

2ay

dz 2ay y 2 0 p Z 2a Z 2a p 2a.2a y/ dy dy D 4 2a3=2 D 4a p p y y.2a y/ 0 0 ˇ2a p p ˇ D 4 2a3=2 .2 y/ˇˇ D 16a2 sq. units.

ZZ

Z

The cylinder x 2 C y 2 D 2ay intersects the sphere x 2 C y 2 C z 2 D 4a2 on the parabolic cylinder 2ay C z 2 D 4a2 . By Exercise 5, the area element on x 2 C y 2 2ay D 0 is

The area of the part of the cylinder inside the sphere is 4 times the part shown in Figure 15.23 in the text, that is, 4 times the double p integral of dS over the region 0  y  2a, 0  z  4a2 2ay, or

The required area is S D4

ˇ ˇ ˇ rF .x; y; z/ ˇ ˇ dx dz dS D ˇˇ F2 .x; y; z/ ˇ ˇ ˇ ˇ rF .x; y; z/ ˇ ˇ dy dz dS D ˇˇ F1 .x; y; z/ ˇ

ˇ ˇ ˇ 2xi C .2y 2a/j ˇ ˇ ˇ dy dz dS D ˇ ˇ 2x s .y a/2 dy dz D 1C 2ay y 2 s 2ay y 2 C y 2 2ay C a2 a D dy dz D p 2ay y 2 2ay

Similarly,

dS D

(PAGE 905)

Let u D 4a2 r 2 du D 2r dr

0

0

4a2 cos2 

0

=2

2a cos  / d ˇ=2 ˇ D 8a2 . sin  /ˇˇ

7.

.2a 0

D 16a2 .

On the surface S with equation z D x 2 =2 we have @z=@x D x and @z=@y D 0. Thus

2/ sq. units.

0

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dS D

p 1 C x 2 dx dy: 595

dy dz:

lOMoARcPSD|6566483

SECTION 15.5 (PAGE 905)

ADAMS and ESSEX: CALCULUS 9

If R is the first quadrant part of the disk x 2 C y 2  1, then the required surface integral is ZZ

S

x dS D D

ZZ Z

R

p

x2

x 1

x4

1

x 1C

0

D

Z

D

1 2

p x 1 C x 2 dx dy p

1

1

p

p

1 x2

dS D

dy 0

Let u D x 2 du D 2x dx 1  u2 du D D : 24 8

0

Z

dx

Z

10. One-eighth of the required area lies in the first octant, above the triangle T with vertices .0; 0; 0/, .a; 0; 0/ and .a; a; 0/. (See the figure.) The surface x 2 C z 2 D a2 has normal n D xi C zk, so an area element on it can be written

1

0

a a dx dy jnj : dx dy D dx dy D p jn  kj z a2 x 2

The area of the part of that cylinder lying inside the cylinder y 2 C z 2 D a2 is ZZ Z x Z a dx a dx dy D 8a dy p p S D8 2 x2 a2 x 2 0 0 ZTa a x dx p D 8a a2 ˇx 2 0 p ˇa D 8a a2 x 2 ˇˇ D 8a2 sq. units.

dx

2 2 ı 8. The normal to the cone z 2 D px C y makes a 45 angle with the vertical, so dS D 2 dx dy is a surface area element for the cone. Both nappes (halves) of the cone pass through the interior of the cylinder x 2 C y 2 D 2ay, sopthe area of that part of the cone inside the cylinder is 2 2a2 square units, since the cylinder has a circular cross-section of radius a.

0

z y 2 Cz 2 Da2

x 2 Cz 2 Da2

9. One-quarter of the required area lies in the first octant. (See the figure.) In polar coordinates, the Cartesian equation x 2 C y 2 D 2ay becomes r D 2a sin  . The arc length element on this curve is

ds D

s

r2 C



dr d

2

p Thus dS D x 2 C y 2 ds D 2ar d D 4a2 sin  d on the cylinder. The area of that part of the cylinder lying between the nappes of the cone is

4

Z

=2 0

T

d D 2a d:

4a2 sin  d D 16a2 sq. units.:

z

y

x .a;a;0/

Fig. 15.5-10 11.

Let the sphere be x 2 C y 2 C z 2 D R2 , and the cylinder be x 2 C y 2 D R2 . Let S1 and S2 be the parts of the sphere and the cylinder, respectively, lying between the planes z D a and z D b, where R  a  b  R. Evidently, the area of S2 is S2 D 2R.b a/ square units. An area element on the sphere is given in terms of spherical coordinates by dS D R2 sin  d d: On S1 we have z D R cos , so S1 lies between  D cos 1 .b=R/ and  D cos 1 .a=R/. Thus the area of S1 is

z 2 Dx 2 Cy 2

dS

S1 D R2 y x

ds

x 2 Cy 2 D2y

Z

2

d 0

Z

cos

cos

1 .a=R/

sin  d 1 .b=R/

ˇcos ˇ D 2R2 . cos /ˇˇ cos

Fig. 15.5-9

596

1 .a=R/

1 .b=R/

D 2R.b

Observe that S1 and S2 have the same area.

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a/ sq. units.

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 15.5

(PAGE 905)

z

zDb zDa y x

zD R

Fig. 15.5-11 12. We want to find A1 , the area of that part of the cylinder x 2 C z 2 D a2 inside the cylinder y 2 C z 2 D b 2 , and A2 , the area of that part of y 2 C z 2 D b 2 inside x 2 C z 2 D a2 . We have A1 D 8  .area of S1 /; A2 D 8  .area of S2 /; where S1 and S2 are the parts of these surfaces lying in the first octant, as shown in the figure. A normal to S1 is n1 D xi C zk, and the area element on S1 is jn1 j a dy dz dS1 D dy dz D p : jn1  ij a2 z 2

13.

a

dz

Z

p b2 z 2

R1 a

Z

dy

z2

dx

.1 C y/2 D 2.x 2 C y 2 /

1 C 2y C y 2 D 2x 2 C 2y 2

b y 2 Cz 2 Db 2

2x 2 C y 2

S1 a

x2 C

R1

y

Thus Fig. 15.5-12 A normal to S2 is n2 D xj C zk, and the area element on S2 is b dx dz jn2 j dx dz D p dS2 D : jn2  jj b2 z2 Let R1 be the region of the first quadrant of the yz-plane bounded by y 2 C z 2 D b 2 , y D 0, z D 0, and z D a. Let R2 be the quarter-disk in the first quadrant of the xzplane bounded by x 2 C z 2 D a2 , x D 0, and z D 0. Then

2y C 1 D 2

1/2

.y

D 1: p Note that E has area A D .1/. 2/ and centroid .0; 1/. If S is the part of the plane lying inside the cone, then the area element on S is s  2 p @z dx dy D 2 dx dy: dS D 1 C @y

S2

R2

x

Z

The intersection of the plane z D 1 C y and the cone p z D 2.x 2 C y 2 / has projection onto the xy-plane the elliptic disk E bounded by

z

x 2 Cz 2 Da2

ZZ

p dS1 D 8a a2 z 2 0 0 p 2 2 b z D 8a dz Let z D a sin t p 2 0 a z2 dz D a cos t dt Z =2 p 2 D 8a b 2 a2 sin t dt 0 s Z =2 a2 1 sin2 t dt D 8ab b2 0 a D 8abE sq. units. b Z pa2 ZZ Z a dz p A2 D 8 dS2 D 8b b2 z2 0 R2 0 Z ap 2 2 a z D 8b dz Let z D b sin t p b2 z2 0 dz D b cos t dt Z sin 1 .a=b/ p D 8b a2 b 2 sin2 t dt 0 s Z sin 1 .a=b/ b2 1 sin2 t dt D 8ab a2 0   a b ; sin 1 sq. units. D 8abE a b

A1 D 8

zDR

14.

ZZ

S

y dS D

2

p ZZ p 2 y dx dy D 2Ay D 2: E

p Continuing the above solution, the cone z D 2.x 2 C y 2 / has area element s  2  2 @z @z C dx dy dS D 1 C @x @y s p 4.x 2 C y 2 / D 1C dx dy D 3 dx dy: z2

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SECTION 15.5 (PAGE 905)

ADAMS and ESSEX: CALCULUS 9

If S is the part of the cone lying below the plane z D 1 C y, then ZZ p p p ZZ y dx dy D 3Ay D 6: y dS D 3 S

15.

E

If S is the part of z D x 2 in the first octant and inside (that is, below) z D 1 3x 2 y 2 , then S has projection E onto the xy-plane bounded by x 2 D 1 3x 2 y 2 , or 4x 2 Cp y 2 D 1, an ellipse. Since z D x 2 has area element dS D 1 C 4x 2 dx dy, we have ZZ ZZ p xz dS D x 3 1 C 4x 2 dx dy S

D D

Z

Z

E

1=2

x 0 1=2

3

p

1C

p x3 1

4x 2

dx

1 D 64 16. The surface z D

p

1

1=2

u

0

0

y2 z2 x2 18. The upper half of the spheroid 2 C 2 C 2 D 1 has a a c a circular disk of radius a as projection onto the xy-plane. Since

p 1 4x 2

dy

0

16x 4 dx

0

Z

Z

1 : du D 96

Let u D 1 16x 4 du D 64x 3 dx

and, similarly,

0

The surface S is given by x z D u, for 0  u  1, 0  v ˇ u ˇ e sin v @.y; z/ D ˇˇ 1 @.u; v/ ˇ ˇ 1 @.z; x/ D ˇˇ u e cos v @.u; v/ ˇ u ˇ e cos v @.x; y/ D ˇˇ u e sin v @.u; v/

@z D @y

D e u cos v, y D e u sin v,  . Since ˇ e u cos v ˇˇ u ˇ D e cos v 0 ˇ ˇ 0 ˇ D e u sin v e u sin v ˇ ˇ e u sin v ˇˇ D e 2u e u cos v ˇ

the area element on S is p p dS D e 2u cos2 v C e 2u sin2 v C e 4u du dv D e u 1 C e 2u du dv:

)

@z D @x

c2x ; a2 z

c2y , the area element on the a2 z

spheroid is dS D

2xy has area element

If its density is kz, the mass of the specified part of the surface is Z 5 Z 2 p xCy dy mD dx k 2xy p 2xy 0 0 Z 5 Z 2 Dk dx .x C y/ dy 0 0 Z 5 Dk .2x C 2/ dx D 35k units:

598

2z @z 2x C 2 D0 a2 c @x

D

r x y C dx dy dS D 1 C 2x 2y s 2xy C y 2 C x 2 jx C yj D dx dy D p dx dy: 2xy 2xy

17.

p If the charge density on S is 1 C e 2u , then the total charge is Z  ZZ p Z 1 dv e u .1 C e 2u / du 1 C e 2u dS D 0 0 S ˇ 1  e 3u ˇˇ  D  eu C ˇ D .3e C e 3 4/: 3 ˇ 3

D

s

s

s

1C

c4 x2 C y2 dx dy a4 z2

1C

c2 x2 C y2 dx dy 2 2 a a x2 y2

a4 C .c 2 a2 .a2

a2 /r 2 r dr d r 2/

in polar coordinates. Thus the area of the spheroid is s Z a Z 2 2 a4 C .c 2 a2 /r 2 r dr SD d a 0 a2 r 2 0 Let u2 D a2 r 2 u Z du D r dr 4 a p 4 a C .c 2 a2 /.a2 u2 / du D a 0 Z 4 a p 2 2 D a c .c 2 a2 /u2 du a 0 s Z a c 2 a2 2 u du: D 4c 1 a2 c 2 0 For the case of a prolate spheroid 0 < a < c, let c 2 a2 k2 D . Then a2 c 2 Z ap S D 4c 1 k 2 u2 du Let ku D sin v 0 k du D cos v dv Z sin 1 .ka/ 4c cos2 v dv D k 0 ˇsin 1 .ka/ ˇ 2c ˇ .v C sin v cos v/ˇ D ˇ k p 0 2 2ac c 2 a2 D p C 2a2 sq. units. sin 1 2 2 c c a

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lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 15.5

19. We continue from the formula for the surface area of a spheroid developed part way through the solution above. For the case of an oblate spheroid 0 < c < a, let a2 c 2 k2 D . Then a2 c 2 Z ap S D 4c 1 C k 2 u2 du Let ku D tan v 0 k du D sec2 v dv Z tan 1 .ka/ 4c sec3 v dv D k 0 1 ˇ ˇtan .ka/ 2c  ˇ D sec v tan v C ln.sec v C tan v/ ˇ ˇ k 0 !# " p p 2 2 2 2ac a c a2 c 2 a a C ln C D p c2 c c a2 c 2 ! p 2 2 2 aC a c 2ac ln sq. units. D 2a2 C p 2 2 c a c

z 2b

a

Fig. 15.5-20

21.

Z 2 p dv a2 u2 C b 2 du 0 0 Z 1p D 2a a2 u2 C b 2 du Let au D b tan  0 a du D b sec2  d Z uD1 D 2b 2 sec3  d uD0  ˇˇuD1 D b 2 sec  tan  C ln j sec  C tan  j ˇˇ uD0 ˇ ˇ!ˇ p ˇ au C pa2 u2 C b 2 ˇ ˇ1 2 u2 C b 2 a au ˇ ˇ ˇ 2 C ln ˇ D b ˇ ˇ ˇ ˇ ˇ b2 b 0 ! p p 2 C b2 a C a 2 sq. units. D a a2 C b 2 C b ln b

The distance from the origin to the plane P with equation Ax C By C C z D D, (D ¤ 0) is ıD p

A2

jDj

C B2 C C 2

:

If P1 is the plane z D ı, then, since the integrand depends only on distance from the origin, we have ZZ

dS C y 2 C z 2 /3=2 ZZ P dS D 2 2 2 3=2 P1 .x C y C z / Z 2 Z 1 r dr Let u D r 2 C ı 2 D d 2 C ı 2 /3=2 .r 0 0 du D 2r dr Z 1 1 du D 2  2 ı 2 u3=2 ˇ1  2 ˇˇ p ˇ D u ˇ 2 pı 2 2 A2 C B 2 C C 2 D D : ı jDj

The area of the ramp is Z

y

x

20. x D au cos v; y D au sin v; z D bv, .0  u  1; 0  v  2/. This surface is a spiral (helical) ramp of radius a and height 2b, wound around the z-axis. (It’s like a circular staircase with a ramp instead of stairs.) We have ˇ ˇ ˇ a cos v @.x; y/ au sin v ˇˇ ˇ D a2 u Dˇ a sin v au cos v ˇ @.u; v/ ˇ ˇ ˇ a sin v au cos v ˇ @.y; z/ ˇ D ab sin v D ˇˇ ˇ 0 b @.u; v/ ˇ ˇ ˇ 0 ˇ @.z; x/ b ˇ D ab cos v D ˇˇ a cos v au sin v ˇ @.u; v/ p dS D a4 u2 C a2 b 2 sin2 v C a2 b 2 cos2 v du dv p D a a2 u2 C b 2 du dv:

ADa

(PAGE 905)

1

22.

.x 2

Use spherical coordinates. The area of the eighth-sphere S is 1 a2 A D .4a2 / D sq. units. 8 2 The moment about z D 0 is MzD0 D D D

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ZZ

Z

z dS S

=2

d 0

a3 2

Z

0

Z

0 =2

=2

a cos  a2 sin  d

sin 2 a3 d D : 2 4

599

lOMoARcPSD|6566483

SECTION 15.5 (PAGE 905)

ADAMS and ESSEX: CALCULUS 9

MzD0 a D . By symmetry, x D y D z, Thus z D A 2 so the centroid of that part of the surface of the  asphere a a x 2 C y 2 C z 2 D a2 lying in the first octant is ; ; . 2 2 2 ! p x2 C y2 has normal 23. The cone z D h 1 a @z i @x

nD

h a

D

@z jCk @y xi C yj p x2 C y2

Thus, the total force on m is

F D km

Z

Z

2

d 0

!

C k;

dS 

The moment about z D 0 is ZZ MzD0 D  h 1

!p p x2 C y2 a2 C h2 dx dy a a x 2 Cy 2 a2 p Z 2h a2 C h2 a  r D 1 r dr a a 0 p ha a2 C h2 : D 3

m

25.

kma.b z/ d dz km dS cos D D2 D3 kma.b z/ d dz D  3=2 : a2 C .b z/2

dF D

The total force exerted by the cylindrical surface on the mass m is

F D

Z

2

d

0

D 2kma a

y

D 2km

Fig. 15.5-23 24.

By symmetry, the force of attraction of the hemisphere shown in the figure on the mass m at the origin is vertical. The vertical component of the force exerted by area element dS D a2 sin  d d at the position with spherical coordinates .a; ;  / is dF D

600

km dS cos  D km sin  cos  d d: a2

y

The surface element dS D a d dz at the point with cylindrical coordinates .a; ; z/ attracts mass m at point .0; 0; b/ with a force whose vertical component (see the figure) is

z

hp zDh a x 2 Cy 2

a

Fig. 15.5-24

h Thus z D . By symmetry, x D y D 0. The centre of 3 mass is on the axis of the cone, one-third of the way from the base towards the vertex.

h

a

a

x

The mass of the conical shell is p ZZ p  a2 C h2 mD .a2 / D a a2 C h2 : dS D a x 2 Cy 2 a2

a

sin  cos  d D km units.

0

z

so its surface area element is s p h2 a2 C h2 C 1 dx dy D dx dy: dS D 2 a a

x

=2

Z

Z

Z

h 0

kma.b z/ dz  3=2 a2 C .b z/2

zDh

zD0 zDh

Let b z D a tan t dz D a sec2 t dt

a tan t a sec2 t dt a3 sec3 t

sin t dt ˇzDh ˇ D 2km. cos t /ˇˇ zD0

zD0

D 2km p

a

a2 C .b

D 2kma

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p

ˇh ˇ ˇ ˇ 2 z/ ˇ 0

1

a2 C .b

h/2

p

1 a2 C b 2

!

:

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 15.6

The mass of S, which has areal density , was also deterp mined in that exercise: m D a a2 C h2 . The moment of inertia of S about the z-axis is

z .0;0;b/

m

I D

D

h

dS

a

a

ZZ

S

.x 2 C y 2 / dS

p Z Z a  a2 C h2 2 D d r 2 r dr a 0 0 p p 2 a2 C h2 a4 a3 a2 C h2 D D : a 4 2

a

x

y

The radius of gyration is D D Fig. 15.5-25 29. 2

2

2

26. S is the cylindrical surface x C y D a , 0  z  h, with areal density . Its mass is m D 2ah. Since all surface elements are at distance a from the z-axis, the radius of gyration of the cylindrical surface about the zaxis is D D a. Therefore the moment of inertia about that axis is 2 I D mD D ma2 D 2a3 h:

27.

1 2 mv C 2 1 D mv 2 C 2 5 D mv 2 : 6

K:E: D

ZZ

r

zDh 1

x2 C y2 a

!

Differentiating with respect to time t , we get 0D

2 a. 3

5 dv dh 5 dv m 2v C mg D mv C mgv sin ˛: 6 dt dt 3 dt

Thus the sphere rolls with acceleration dv 3 D g sin ˛: dt 5

;

Section 15.6 Oriented Surfaces and Flux Integrals (page 912)

having base radius a and height h, was determined in the solution to Exercise 23 to be dS D

p

a2 C h2 dx dy: a

1 I 2 2 1 2 2 v2 ma 2 2 3 a

5 2 mv C mgh D constant: 6

28. The surface area element for a conical surface S, p

a I =m D p . 2

The potential energy is P:E: D mgh, so, by conservation of total energy,

.x 2 C y 2 / dS S Z 2 Z  D d a2 sin2  a2 sin  d 0 0 Z  sin .1 cos2 / d Let u D cos  D 2a4 0 du D sin  d Z 1 8a4 2 4 : .1 u / du D D 2a 3 1

p The radius of gyration is D D I =m D

p

By Exercise 27, the moment of inertia of a spherical shell 2 of radius a about its diameter is I D ma2 . Following 3 the argument given in Example 4(b) of Section 14.7, the kinetic energy of the sphere, rolling with speed v down a plane inclined at angle ˛ above the horizontal (and therefore rotating with angular speed  D v=a) is

S is the spherical shell, x 2 C y 2 C z 2 D a2 , with areal density . Its mass is 4a2 . Its moment of inertia about the z-axis is I D

(PAGE 912)

1.

F D xi C zj. The surface S of the tetrahedron has four faces:

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601

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SECTION 15.6 (PAGE 912)

ADAMS and ESSEX: CALCULUS 9

O D i, F  N O D 0. On S1 , x D 0, N O O D z, dS D dx dz. On S2 , y D 0, N D j, F  N O D k, F  N O D 0. On S3 , z D 0, N 2j C 3k O D i Cp On S4 , x C 2y C 3z D 6, N , 14 p dx dy 14 C 2z O D xp dx dz. , dS D D FN O  jj 2 14 jN We have ZZ

ZZ ZZ

S1

O dS D FN

S2

O dS D FN D

S4

O dS D FN D D D

ZZ

O D a on S. Thus the flux If F D xi C yj C zk, then F  N of F out of S is ZZ

S

3. S3

Z

Z

O dS D 0 FN

2

z dz 0

Z

6 3z

dx

F D xi C yj C zk. O D 0 on the three faces x D 0, The box has six faces. F  N O D i, so y D 0, and z D 0. On the face x D a, we have N O F  N D a. Thus the flux of F out of that face is

0

2

.6z

3z 2 / dz D

a  .area of the face/ D abc:

4

p0 Z 2 Z 6 3z 14 1 dz .x C 2z/ dx p 2 14 0 0  Z  1 2 .6 3z/2 C 2z.6 3z/ dz 2 0 2 Z 2 1 .6 3z/.6 C z/ dz 4 0 ˇ2 ˇ 1 2 3 ˇ .36z 6z z /ˇ D 10: ˇ 4

By symmetry, the flux of F out of the faces y D b and z D c are also each abc. Thus the total flux of F out of the box is 3abc. z c

0

S

O dS D 0 FN

S1

F D yi C zk. Let S1 be the conical surface and S2 be the base disk. The flux of F outward through the surface of the cone is ZZ ZZ ZZ O D FN C : S

S4 3 y 6

Fig. 15.6-3

4. 2

x

S3

S1

D

2. On the sphere S with equation x 2 C y 2 C z 2 D a2 we have O D xi C yj C zk : N a

S1

S2

!

p xi C yj p C k , dS D 2 dx dy. 2 2 x Cy

O D p1 On S1 : N 2 Thus ZZ

Fig. 15.6-1

602

y

x

4 C 0 C 10 D 6:

z

S2

b

a

The flux of F out of the tetrahedron is ZZ

O dS D a  4a2 D 4a3 : FN

O dS FN

ZZ

x 2 Cy 2 1

D 0 C   12 D

p xy p x2 C y2 C1 x2 C y2 Z 2 Z 1 d r 2 dr 0

!

dx dy

0

 2 D : 3 3

O D k and z D 0, so F  N O D 0. Thus, the total On S2 : N flux of F out of the cone is =3.

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lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 15.6

Note that D has area 4 and centroid . 1; 0/. For z D 4 x 2 y 2 , the downward vector surface element is O dS D 2xi 2yj k dx dy: N 1

z

1

O N S1

zD1

Thus the flux of F D y 3 i C z 2 j C xk downward through S is ZZ ZZ   O dS D FN 2xy 3 C 2y.4 x 2 y 2 /2 C x dx dy

p

x 2 Cy 2

S

D

S2 O N

1

x

D

y

Fig. 15.6-4 5. The part S of z D a x 2 y 2 lying above z D b < a lies inside the vertical cylinder x 2 C y 2 D a b. For z D a x 2 y 2 , the upward vector surface element is

8.

D

Z

Œ2.x 2 C y 2 / C a

x2

.r 2 C a/r dr 0 0   .a b/2 a.a b/  D 2 C D .a 4 2 2

D

9.

d

b/.3a

The upward vector surface element on the top half of x 2 C y 2 C z 2 D a2 is

ZZ

y 2  dx dy

x 2 Cy 2 a b Z pa b 2

D



xi C yj Ck z



dx dy:

The flux of F D z 2 k upward through the first octant part S of the sphere is

Thus the flux of F D xi C yj C zk upward through S is O dS FN S ZZ

(use the symmetry of D about the x-axis) ZZ x dA D .4/. 1/ D 4:

O dS D 2xi C 2yj C 2zk dx dy D N 2z

O dS D 2xi C 2yj C k dx dy: N 1

ZZ

(PAGE 912)

S

O dS D FN

Z

=2

d 0

Z

a

.a2

0

r 2 /r dr D

The upward vector surface element on z D 2

a4 : 8

x2

2y 2 is

O dS D 2xi C 4yj C k dx dy: N 1

b/:

x2 C y 2 D 1, then the 2 flux of F D xi C yj through the required surface S is

If E is the elliptic disk bounded by 6. For z D x 2

y 2 the upward surface element is

ZZ

2xi C 2yj C k dx dy: 1

O dS D N

The flux of F D xi C xj C k upward through S, the part of z D x 2 y 2 inside x 2 C y 2 D a2 is ZZ

S

O dS D FN D

ZZ

. 2x C 2xy C 1/ dx dy

x 2 Cy 2 a2 Z 2 2

cos  d

2

0

D a2

7.

2

2./

Z

a 0

r 3 dr C 0 C a2

 a4 D a2 .2 4 2

a2 /:

The part S of z D 4 x 2 y 2 lying above z D 2x C 1 has projection onto the xy-plane the disk D bounded by 2x C 1 D 4

x2

y2;

or .x C 1/2 C y 2 D 4:

D

O dS FN

S ZZ

E

.2x 2 C 4y 2 / dx dy

p ZZ D4 2

p Z D4 2

.u2 C v 2 / du dv

u2 Cv 2 1 Z 1 2

d

0

p Let x D 2u; y D v p dx dy D 2 du dv

0

(now use polars)

p r 3 dr D 2 2:

10. S: r D u2 vi C uv 2 j C v 3 k, .0  u  1; 0  v  1/, has upward surface element O dS D @r  @r du dv N @u @v D .2uvi C v 2 j/  .u2 i C 2uvj C 3v 2 k/ du dv D .3v 4 i

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6uv 3 j C 3u2 v 2 k/ du dv:

603

lOMoARcPSD|6566483

SECTION 15.6 (PAGE 912)

ADAMS and ESSEX: CALCULUS 9

y

The flux of F D 2xi C yj C zk upward through S is ZZ

11.

S

O dS FN Z 1 Z 1 .6u2 v 5 du D 0 0 Z 1 1 1 2 u du D : D 2 0 6

a

R 2 5

a

2 5

a

6u v C 3u v / dv

x

a

Fig. 15.6-13

S: r D u cos vi C u sin vj C uk, .0  u  2; 0  v  /, has upward surface element O dS D @r  @r du dv N @u @v D . u cos vi u sin vj C uk/ du dv:

6ma

S

12. S: r D e u cos vi C e u sin vj C uk, .0  u  1; 0  v  /, has upward surface element O dS D @r  @r du dv N @u @v D . e u cos vi e u sin vj C e 2u k/ du dv:

ZZ

xzj C .x 2 C y 2 /k upward through S

O dS FN Z  1 . ue 2u sin v cos v C ue 2u sin v cos v C e 4u / dv du D 0 0 Z  Z 1 .e 4 1/ : dv D  e 4u du D 4 0 0 S

Z

13. F D

mr m.xi C yj C zk/ . D 2 jrj3 .x C y 2 C z 2 /3=2

14.

By symmetry, the flux of F out of the cube a  x; y; z  a is 6 times the flux out of the top face, O D k and dS D dx dy. The total flux is z D a, where N

604

.x 2

ZZ

dx dy C y 2 C a2 /3=2

r dr d 2 C a2 /3=2 .r R (R as shown in the figure) Z =4 Z a sec  r dr D 48ma d 2 C a2 /3=2 .r 0 0 Let u D r 2 C a2 du D 2r dr Z =4 Z a2 .1Csec2 / du D 24ma d 3=2 2 u 0 a  Z =4  1 1 p d D 48ma a a 1 C sec2  0 ! Z =4  cos  d D 48m p 4 cos2  C 1 0 ! Z =4  cos  d p D 48m 4 0 2 sin2  p Let 2 sin v D sin  p 2 cos v dv D cos  d ! Z =6 p  2 cos v dv D 48m p 4 2 cos v 0   D 4 m: D 48m 4 6

O dS FN Z  Z 2 . u2 cos2 v u2 sin2 v C u3 / dv du D 0 0 Z 2 Z  4 D .u3 u2 / du dv D : 3 0 0

The flux of F D yzi is

axa aya

D 48ma

The flux of F D xi C yj C z 2 k upward through S is ZZ

Z

mr out of the cube 1  x; y; z  2 jrj3 is equal to three times the total flux out of the pair of opposite faces z D 1 and z D 2, which have outward normals k and k respectively. This latter flux is The flux of F D

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lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 15.6

mI1 , where Z 2 Z 2 dy dx Ik D 2 2 2 3=2 1 .x C y C k / 1 p 2 Let y D x C k 2 tan u p dy D x 2 C k 2 sec2 u du Z yD2 Z 2 dx cos u du D 2 2 yD1 1 x Ck ˇ Z 2 ˇyD2 dx  ˇ sin u ˇ D 2 C k2 ˇ x 1 yD1 0 ˇ2 1 Z 2 ˇ dx @ y ˇ A D p D Jk2 ˇ 2 2 2 2 2 x Cy Ck ˇ 1 x Ck

Using the identities

2mI2

Z

Thus,

4

p k 8 C k2

C tan

1

1

2 tan #

2 tan

D m tan

tan

1

1 p 3

1

1

1

4 C 2 tan 3

1

1 C tan 3

15.

2 p 6

2 6 # 1 1 tan p : 3

1

3  4 D C tan 1 4 2 3 1 12  tan 1 p : p D 2 6 2 6 1

The flux of the plane vector field F across the piecewise O to smooth curve C, in the direction of the unit normal N the curve, is Z C

F  n ds:

The flux of F D xi C yj outward across a) the circle x 2 C y 2 D a2 is I

C

F



xi C yj a



ds D

b) the boundary of the square 4

16.

FD

Z

a2  2a D 2a2 : a 1  x; y  1 is

1 1

.i C yj/  i dy D 4

Z

1 1

dy D 8:

xi C yj . x2 C y2

a) The flux of F inward across the circle of Exercise 7(a) is  xi C yj xi C yj ds  a2 a C I 1 a2 ds D  2a D 2: D 3 a a C

I 

p k 5 C k2

1 p

1

Thus the net flux out of the pair of opposite faces is 0. By symmetry this holds for each pair, and the total flux out of the cube is 0. (You were warned this would be a difficult calculation!)

2

1

tan

2 p D tan 6

1 p : k 2 C k2

2 tan

2a ; and a2 1 tan 1 ; a 1

Jk1 ;

The contribution to the total flux from the pair of surfaces z D 1 and z D 2 of the cube is 2mI2 mI1 "

 2

aD

1 D 3

1

2 tan

1

1

a D tan

we calculate

2

" 1 tan Ik D k

1

tan

dx p .x 2 C k 2 / x 2 C n2 C k 2 p Let x D n2 C k 2 tan v p dx D n2 C k 2 sec2 v dv Z xD2 sec2 v dv h i Dn xD1 .n2 C k 2 / tan2 v C k 2 sec v Z xD2 cos v dv Dn 2 2 2 2 2 xD1 .n C k / sin v C k cos v Z xD2 cos v dv Dn Let w D n sin v 2 2 2 xD1 k C n sin v dw D n cos v dv ˇxD2 Z xD2 ˇ 1 dw 1 wˇ D tan D ˇ 2 2 k kˇ xD1 k C w xD1 ˇxD2 ˇ n sin v ˇ 1 D tan 1 ˇ k k ˇ xD1 ˇ2 ˇ nx 1 ˇ 1 D tan p ˇ k k x 2 C n2 C k 2 ˇ1   2n 1 n tan 1 p D tan 1 p : k k 4 C n2 C k 2 k 1 C n2 C k 2

Jk n D n

1

2 tan

1

where

(PAGE 912)

b) The flux of F inward across the boundary of the square of Exercise 7(b) is four times the flux inward across the edge x D 1, 1  y  1. Thus it is 4

Z

1 1



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i C yj 1 C y2



Z

1

dy 1 C y2 ˇ1 ˇ D 4 tan 1 y ˇˇ D 2:

 i dy D 4

1

1

605

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SECTION 15.6 (PAGE 912)

ADAMS and ESSEX: CALCULUS 9

3. 17.

O across S is The flux of N ZZ ZZ O N O dS D N dS D area of S: S

The cone z D dS D

ZZ

ZZ

4. 0yb 0zc

.F1

F1 / dy dz D 0:

The flux out of the other two pairs of opposite faces is also 0. Thus the total flux of F out of the box is 0.

1C

S

x dS D

Thus the flux out of S is ZZ 1 .F1 x C F2 y C F3 z/ ds D 0; a S

5.

2y dx C x dy C 2 dz Z 2 D Œ4t .1/ C t .2/ C 2.1 C 8t / dt 0 Z 2 D .22t C 2/ dt D 48: 0

1 Z 1

1

Z

1 y2

x dx 0

0

p 2y 2 C y 4 8 2 dy D : 2 15

S

Z 1 x p Z 1 3 x dx y.1 x y/ dy 0 0 p Z 1 x.1 x/3 dx Let u D 1 x D 3 6 0 du p p D dx  p Z 1 3 3 1 1 3 3 D : u .1 u/ du D D 6 0 6 4 5 120

xyz dS D

For z D xy, the upward vector surface element is

ZZ

CW

1

dy

y2

yi

xj C k dx dy: 1

The flux of F D x 2 yi 10xy 2 j upward through S, the part of z D xy satisfying 0  x  1 and 0  y  1 is

Review Exercises 15 (page 913)

2. C can be parametrized x D t , y D 2t , z D t C 4t 2 , .0  t  2/. Thus

1

O dS D N

since the sphere S is symmetric about the origin.

x D t; y D 2e t ; z D e 2t ; . 1  t  1/ p v D 1 C 4e 2t C 4e 4t D 1 C 2e 2t Z 1 Z 1 C 2e 2t ds dt D 2e t 1 C y  ˇˇ1 e t 3.e 2 1/ t ˇ D Ce ˇ D : ˇ 2 2e

p Z 2

p D2 2

O D xi C yj C zk : N a

S

O dS D FN

Z

0

0

6.

1

Z

1

. x 2 y 2 C 10x 2 y 2 / dy Z 1 Z 1 D 3x 2 dx 3y 2 dy D 1: dx

0

0

The plane x C 2y C 3z D 6 has downward vector surface element O dS D i 2j 3k dx dy: N 3 If S is the part of the plane in the first octant, then the projection of S on the xy-plane is the triangle 0  y  3, 0  x  6 2y. Thus ZZ O dS .xi C yj C zk/  N S Z Z 6 2y 1 3 D dy .x C 2y C 6 x 2y/ dx 3 0 0 Z 3 D 2 .6 2y/ D 36 C 18 D 18: 0

606

p x2 C y2 dx dy D 2 dx dy: z2

p The plane x Cy Cz D 1 has area element dS D 3 dx dy. If S is the part of the plane in the first octant, then the projection of S on the xy-plane is the triangle 0  x  1, 0  y  1 x. Thus ZZ

b) If S is a sphere of radius a we can choose the origin so that S has equation x 2 C y 2 C z 2 D a2 , and so its outward normal is

C

s

If S is the part of the cone in the region 0  x  1 (which itself lies between y D 1 and y D 1), then

a) If R is a rectangular box, we can choose the origin and coordinate axes in such a way that the box is 0  x  a, 0  y  b, 0  z  c. On the faces O D i and N O D i x D 0 and x D a we have N respectively. Since F1 is constant, the total flux out of the box through these two faces is

Z

x 2 C y 2 has area element

S

18. Let F D F1 i C F2 j C F3 k be a constant vector field.

1.

p

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INSTRUCTOR’S SOLUTIONS MANUAL

7.

REVIEW EXERCISES 15

r D a sin t i C a cos t j C bt k, .0  t  6/ r.0/ D aj, r.6/ D aj C 6bk.

The field line passes through .1; 1; 0/ provided C1 D 0 and C2 D 0. In this case the field line also passes through .e; e; 1/, and the segment from .1; 1; 0/ to .e; e; 1/ can be parametrized r.t / D e t i C e t j C t k; .0  t  1/: Then

a) The force F D mgk D r.mgz/ is conservative, so the work done by F as the bead moves from r.6/ to r.0/ is

W D

Z

ˇzD0 ˇ ˇ mgz ˇ ˇ

tD0 tD6

F  dr D

D 6 mgb:

R

v D jvj

p

R a2

C

b2

10.

W D

8.

6 0

p

R a2 C b 2

Z

p

jvj2 dt D 6R a2 C b 2 :

C

G  dr D

D

11.

3

Z

y/.j C k/  d r

2.z C

ˇ.0;1;2/ ˇ z 2 /ˇˇ .1;0;0/

1

t /.1 C 2/ dt ˇ1 ˇ e C 3t 2 ˇˇ D e: .2t

0

0

Since the field lines of F are xy D C , and so satisfy y dx C x dy D 0;

or

dx D x

dy ; y

thus F D .x; y/.xi yj/. Since p jF.x; y/j D 1 if .x; y/ ¤ .0; 0/, .x; y/ D ˙1= x 2 C y 2 , and xi yj : F.x; y/ D ˙ p x2 C y2

Thus we need a D 2, b D 3, and c D 1. With these values, F D r.x 2 y C 3xyz C y 3 z/. Thus

Since F.1; 1/ D .i

p j/= 2, we need the plus sign. Thus

xi yj F.x; y/ D p ; x2 C y2

.0;1; 1/

ln y D z C C2 :

C

Z

F  dr C

C2

is conservative, that is, if

9. F D .x 2 =y/i C yj C k. dy y dx D D dz. Thus The field lines satisfy x2 y 2 2 dx=x D dy=y and the field lines are given by

Z

D .xe xCy C y 2

F D .axy C 3yz/i C .x 2 C 3xz C by 2 z/j C .bxy C cy 3 /k

ˇ.2;1;1;/ ˇ 2 3 ˇ F d r D .x y C3xyz Cy z/ˇ D 11 . 1/ D 12: ˇ C

2zk

2

b) G D .1 C x/e xCy i C .xe xCy C 2z/j 2yk D F C 2.z y/.j C k/: C W r D .1 t /e t i C t j C 2t k; .0  t  1/. r.0/ D .1; 0; 0/; r.1/ D .0; 1; 2/. Thus

v:

@F2 @F1 D D 2x C 3z ax C 3z D @y @x @F3 @F1 D D by 3y D @z @x @F2 @F3 3x C by 2 D D D bx C 3cy 2 : @z @y

2

D r.xe Cy z /: Thus F is conservative.

C F  d r can be determined using only the endpoints of C, provided

1 1 D C C1 ; x y

0

a) F D .1 C x/e xCy i C .xe xCy C 2y/j

R

Z

1

.e 2t C e 2t C 1/ dt ˇ1 ˇ D .e 2t C t /ˇˇ D e 2 :

F  dr D

xCy

Since d r D v dt , the work done against the resistive force is Z

Z

0

p b) v D a cos t i a sin t j C bk, jvj D a2 C b 2 . A force of constant magnitude R opposing the motion of the bead is in the direction of v, so it is FD

Z

C

zD6b

(PAGE 913)

which is continuous everywhere except at .0; 0/. 12. The first octant part of the cylinder y 2 C z 2 D 16 has outward vector surface element O dS D 2yj C 2zk dx dy D N 2z

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p

y 16

y2

!

jCk

dx dy:

607

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REVIEW EXERCISES 15 (PAGE 913)

The flux of 3z 2 xi surface S is O dS D FN D

Z

Z

yk outward through the specified

xj

5

dx 0

0

Z

D

Z

4

0 y2

p 16

y dy y2 ˇyD4 y 2 ˇˇ dx ˇ 2 ˇ yD0

5

0

Therefore the surface S is traced out twice as u goes from 0 to 2. (It is a Mobius band. See Figure 15.28 in the text.) If S1 is the part of the surface corresponding to 0  u  , and S2 is the part corresponding to   u  2, then S1 and S2 coincide as point sets, O2 D N O 1 at but their normals are oppositely oriented: N corresponding points on the two surfaces. Hence ZZ ZZ O 1 dS D O 2 dS; FN FN

!

xy

0

 p x 16

5

ADAMS and ESSEX: CALCULUS 9

.4x C 8/ dx D

S1

90:

S2

for any smooth vector field, and ZZ ZZ ZZ O dS D O 1 dS C FN FN S

Challenging Problems 15 (page 913)

S1

S2

O 2 dS D 0: FN

3. 1.

Given: x D .2 C cos v/ cos u, y D .2 C cos v/ sin u, z D sin v for 0  u  2, 0  v  . The cylindrical coordinate r satisfies

.0; 0; b/

r 2 D x 2 C y 2 D .2 C cos v/2 r D 2 C cos v

b

dS

Z

 0

2.2 C cos v/ dv D 4 2 :

The strip has moment z dS D 2.2 C cos v/ sin v dv about z D 0, so the moment of the whole surface about z D 0 is MzD0 D 2 D 2

Z

 0



.2 C cos v/ sin v dv 2 cos v

ˇˇ 1 ˇ cos.2v/ ˇ D 8: ˇ 4



8 2 D . The centroid is .0; 0; 2=/. 4 2 

r.u C ; v/ D r.u; v/:

a

Fig. C-15-3 The mass element p dS at position Œa; ;   on the sphere is at distance D D a2 C b 2 2ab cos  from the mass m located at .0; 0; b/, and thus it attracts m with a force of magnitude dF D kmdS=D 2 . By symmetry, the horizontal components of dF coresponding to mass elements on opposite sides of the sphere (i.e., at Œa; ;   and Œa; ;  C ) cancel, but the vertical components dF cos

0

2. This is a trick question. Observe that the given parametrization r.u; v/ satisfies

608

D

a cos 

This equation represents the surface of a torus, obtained by rotating about the z-axis the circle of radius 1 in the xz-plane centred at .2; 0; 0/. Since 0  v   implies that z  0, the given surface is only the top half of the toroidal surface. By symmetry, x D 0 and y D 0. A ring-shaped strip on the surface at angular position v with width dv has radius 2 C cos v, and so its surface area is dS D 2.2 C cos v/ dv. The area of the whole given surface is

Thus z D

a cos 

2/2 C z 2 D 1:

.r

SD

m

D

km dS b D2

a cos  D

reinforce. The total force on the mass m is the sum of all such vertical components. Since dS D a2 sin  d d , it is Z 2 Z  .b a cos / sin  d F D kma2 d 2 2 2ab cos /3=2 0 0 .a C b Z 1 .b at /dt D 2kma2 : 2 2abt C b 2 /3=2 1 .a

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INSTRUCTOR’S SOLUTIONS MANUAL

CHALLENGING PROBLEMS 15

We have made the change of variable t D cos  to get the last integral. This integral p can be evaluated by using another substitution. Let u D a2 2abt C b 2 . Thus tD

a2 C b 2 u2 ; 2ab

dt D

u du ; ab

b at D

u2 C b 2 2b

When t D 1 and t D 1 we have u D a C b and u D ja bj respectively. Therefore   Z ja bj 2 u C b 2 a2 u du F D 2kma2 2bu3 ab aCb ! Z aCb 2 2 b a kma du 1 C D b2 u2 ja bj !ˇaCb kma b 2 a2 ˇˇ D u : ˇ ˇ b2 u

(PAGE 913)

There are now two cases to consider. If the mass m is outside the sphere, so that b > a and ja bj D b a, then a2

:

F D

kma b2

  a2 .aCb/ .b a/ .b a/C.bCa/ D 4km 2 : b

However, if m is inside the sphere, so that b < a and ja bj D a b, then F D

kma b2

 .a C b/ C .a

b/

.a

b/

 .a C b/ D 0:

ja bj

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609

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SECTION 16.1 (PAGE 922)

ADAMS and ESSEX: CALCULUS 9

CHAPTER 16. VECTOR CALCULUS

7.

F D f .x/i C g.y/j C h.z/k @ @ @ f .x/ C g.y/ C h.z/ div F D @x @y @z D f 0 .x/ C g 0 .y/ C h0 .z/ ˇ ˇ j k ˇ ˇ i ˇ @ @ @ ˇˇ ˇ curl F D ˇ ˇD0 @y @z ˇ ˇ @x ˇ f .x/ g.y/ h.z/ ˇ

8.

F D f .z/i f .z/j  @ @  div F D f .z/ C f .z/ D 0 @x @y ˇ ˇ j k ˇ ˇ i ˇ ˇ @ @ @ ˇ ˇ curl F D ˇ ˇ D f 0 .z/.i C j/ @y @z ˇ ˇ @x ˇ f .z/ f .z/ 0 ˇ

Section 16.1 Gradient, Divergence, and Curl (page 922) 1.

2.

3.

4.

F D xi C yj @ @ @ div F D .x/ C .y/ C .0/ D 1 C 1 D 2 @x @y @z ˇ ˇ j k ˇ ˇ i ˇ @ @ @ ˇˇ ˇ curl F D ˇ ˇD0 ˇ @x @y @z ˇ ˇ x y 0 ˇ F D yi C xj @ @ @ div F D .y/ C .x/ C .0/ D 0 C 0 D 0 @x @y @z ˇ ˇ j k ˇ ˇ i ˇ @ @ @ ˇˇ ˇ curl F D ˇ ˇ D .1 1/k D 0 ˇ @x @y @z ˇ ˇ y x 0 ˇ

6.

Since x D r cos  , and y D r sin  , we have r 2 D x 2 C y 2 , and so

F D yi C zj C xk @ @ @ div F D .y/ C .z/ C .x/ D 0 @x @y @z ˇ ˇ ˇ i j k ˇ ˇ @ @ @ ˇˇ ˇ curl F D ˇ ˇD i j k ˇ @x @y @z ˇ ˇ y z x ˇ

x @r D D cos  @x r @r y D D sin  @y r @ y xy @ sin  D D 3 D @x @x r r @ @ y 1 y2 sin  D D @y @y r r r3 2 2 x cos  D 3 D r r @ @ x 1 x2 cos  D D @x @x r r r3 2 2 sin  y D 3 D r r @ @ x xy cos  D D 3 D @y @y r r

F D yzi C xzj C xyk @ @ @ div F D .yz/ C .xz/ C .xy/ D 0 @x @y @z ˇ ˇ ˇ i j k ˇ ˇ @ @ @ ˇˇ ˇ curl F D ˇ ˇ ˇ @x @y @z ˇ ˇ yz xz xy ˇ D .x

5.

9.

x/i C .y

y/j C .z

z/k D 0

F D xi C xk @ @ @ .x/ C .0/ C .x/ D 1 div F D @x @y @z ˇ ˇ j k ˇ ˇ i ˇ @ @ @ ˇˇ ˇ curl F D ˇ ˇD j ˇ @x @y @z ˇ ˇ x 0 x ˇ

610

2xzj

2xyk

cos  sin  : r

(The last two derivatives are not needed for this exercise, but will be useful for the next two exercises.) For F D ri C sin  j;

F D xy 2 i yz 2 j C zx 2 k    @ @ @ div F D xy 2 C yz 2 C zx 2 @x @y @z D y2 z2 C x2 ˇ ˇ ˇ i j k ˇˇ ˇ ˇ @ @ @ ˇ ˇ curl F D ˇˇ ˇ @x @y @z ˇ 2 ˇ 2 2ˇ ˇ xy yz zx D 2yzi

cos  sin  r

we have @ cos2  @r C sin  D cos  C @x @y r ˇ ˇ j k ˇ ˇ i ˇ @ @ @ ˇˇ ˇ curl F D ˇ ˇ @y @z ˇ ˇ @x ˇ r sin  0 ˇ   sin  cos  sin  k: D r div F D

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 16.1

F D rO D cos  i C sin  j

10.

where    represents terms of degree 4 and higher in a, b, and c. Similar formulas obtain for the two other pairs of faces, and the three formulas combine into ZZ O dS D 8abcdiv F.0; 0; 0/ C    :

FN

sin2  cos2  1 1 div F D C D D p 2 r r r x C y2 ˇ ˇ j k ˇ ˇ i ˇ @ @ @ ˇˇ ˇ curl F D ˇ ˇ @x @y @z ˇ ˇ ˇ cos  sin  0 ˇ   cos  sin  cos  sin  kD0 D r r

Ba;b;c

It follows that lim

a;b;c!0C

11.

F D O D sin  i C cos  j cos  sin  cos  sin  div F D D0 r r ˇ ˇ j k ˇ ˇ i ˇ @ @ @ ˇˇ ˇ curl F D ˇ ˇ @y @z ˇ ˇ @x ˇ sin  cos  0 ˇ ! cos2  1 1 sin2  C kD kD p k D 2 r r r x C y2

13.

ZZ 1 O dS D div F.0; 0; 0/:

FN 8abc Ba;b;c

This proof just mimics that of Theorem 1. F can be expanded in Maclaurin series F D F0 C F1 x C F2 y C    ; where F0 D F.0; 0/

ˇ  ˇ @F1 @ ˇ F1 D F.x; y/ˇ iC D ˇ @x @x .0;0/ ˇ  ˇ @F1 @ ˇ D F.x; y/ˇ iC F2 D ˇ @y @y

12. We use the Maclaurin expansion of F, as presented in the proof of Theorem 1:

.0;0/

F D F0 C F1 x C F2 y C F3 z C    ;

F0 D F.0; 0; 0/

ˇ ˇ  ˇ @ @F2 @F3 ˇˇ @F1 ˇ F1 D F.x; y; z/ˇ iC jC k ˇ D ˇ ˇ @x @x @x @x ˇ.0;0;0/ ˇ.0;0;0/   ˇ @ @F1 @F2 @F3 ˇˇ ˇ F2 D F.x; y; z/ˇ iC jC k ˇ D ˇ ˇ @y @y @y @y .0;0;0/ ˇ ˇ .0;0;0/   ˇ @F1 @F2 @F3 ˇˇ @ ˇ D F.x; y; z/ˇ iC jC k ˇ F3 D ˇ ˇ @z @z @z @z .0;0;0/

and where    represents terms of degree 2 and higher in x, y, and z. O D k. On the top of the box Ba;b;c , we have z D c and N O D k. On the bottom of the box, we have z D c and N On both surfaces dS D dx dy. Thus ZZ Z

top a

C

ZZ

bottom b

Z



O dS FN

 cF3  . k/ C    a b ˇ ˇ @ ˇ C ; D 8abcF3  k C    D 8abc F3 .x; y; z/ˇ ˇ @z D

dx

 dy cF3  k

.0;0;0/

ˇ @F2 ˇˇ j ˇ @x ˇ .0;0/ ˇˇ @F2 ˇ j ˇ @y ˇ .0;0/

and where    represents terms of degree 2 and higher in x and y. On the curve C of radius  centred at .0; 0/, we have O D 1 .xi C yj/. Therefore, N 

where

.0;0;0/

(PAGE 922)

 O D 1 F0  ix C F0  jy C F1  ix 2 FN   C F1  jxy C F2  ixy C F2  jy 2 C   

where    represents terms of degree 3 or higher in x and y. Since I I I x ds D y ds D xy ds D 0 I

C

C

C

x 2 ds D

I

C

C

y 2 ds D

Z

0

2

 2 cos2   d D  3 ;

we have 1  2

I

C

3 O ds D 1  .F1  i C F2  j/ C    FN  2 

D div F.0; 0/ C   

where    represents terms of degree 1 or higher in . Therefore, taking the limit as  ! 0 we obtain I 1 O ds D div F.0; 0/: lim FN !0  2 C

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SECTION 16.1 (PAGE 922)

14.

ADAMS and ESSEX: CALCULUS 9

We use the same Maclaurin expansion for F as in Exercises 12 and 13. On C we have

3.

@ .F2 G3 F3 G2 / C    @x @G3 @F3 @F2 D G3 C F2 G2 @x @x @x D .r  F/  G F  .r  G/:

r  .F  G/ D

r D  cos  i C  sin  j; .0    2/ d r D  sin  i C  cos  j  F  dr D  sin  F0  i C  cos  F0  j

 2 sin  cos  F1  i C  2 cos2  F1  j

  2 sin2  F2  i C  2 sin  cos  F2  j C    ds;

4.

Z

2

sin  d D

0 2 0

Z

cos2  d D

2

cos  d D

0

Z

2 0

Z

sin  cos  d D 0

sin2  d D ;

I

C

F  d r D F1  j

F2  i C    ;

!0C

1  2

I

C

F  d r D F1  j D

@F2 @x

F1

F2  i @F1 @y

@F1 @F1 @F1 C G2 C G3 : @x @y @z

When we add these four first components, eight of the fourteen terms cancel out and the six remaining terms are the six terms of the first component of r.F  G/, as calculated above. Similar calculations show that the second and third components of both sides of the identity agree. Thus

Theorem 3(a):

r.FG/ D F.r G/CG .r F/C.F r/GC.Gr/F:

@ @ @ . / C . / C . / @x @y @z     @ @ @ @ C i C  C  C k D  @x @x @z @z D r C r:

r. / D

5.

@ @ @ .F1 / C .F2 / C .F3 / @x @y @z @F1 @ @F3 @ F1 C  C  C F3 C  C  D @x @x @z @z D r  F C r  F:

Theorem 3(h). By equality of mixed partials, ˇ ˇ j k ˇ ˇ i ˇ @ @ @ ˇˇ ˇ ˇ ˇ r  r D ˇ @x @y @z ˇ ˇ @ @ @ ˇ ˇ ˇ ˇ ˇ @x @y @z   @ @ @ @ D i C    D 0: @y @z @z @y

2. Theorem 3(b):

612

:

@G1 @G1 @G1 C F2 C F3 : @x @y @z

G1

Section 16.2 Some Identities Involving Grad, Div, and Curl (page 929)

r  .F/ D



The first component of .G  r/F is

O D curl F  k D curl F  N:

1.

@F3 @x

The first component of .F  r/G is

where    represents terms of degree at least 1 in . Hence lim

Theorem 3(f). The first component of r.F  G/ is

The first component of G  .r  F/ is    @F2 @F1 @F1 G2 G3 @x @y @z

we have 1  2

@G2 C  @x

We calculate the first components of the four terms on the right side of the identity to be proved. The first component of F  .r  G/ is     @G1 @G3 @G2 @G1 F3 : F2 @x @y @z @x

2 0

F3

@F1 @G1 @F2 @G2 @F3 @G3 G1 C F1 C G2 C F2 C G3 C F3 : @x @x @x @x @x @x

where    represents terms of degree 3 or higher in . Since Z

Theorem 3(d):

6.

Theorem 3(i). We examine the first components of the terms on both sides of the identity r  .r  F/ D r.r  F/

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r 2 F:

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 16.2

  If f .r/r is solenoidal then r  f .r/r D 0, so that u D f .r/ satisfies

The first component of r  .r  F/ is 

@F2 @x @2 F2 D @y@x

@ @y

 @F1 @y @2 F1 @y 2

  @ @F1 @F3 @z @z @x @2 F1 @2 F3 C : @z 2 @z@x

du C 3u D 0 dr du 3 dr D u r ln juj D 3 ln jrj C ln jC j

r

The first component of r.r  F/ is

u D Cr

@2 F2 @2 F1 @2 F3 @ C r FD C : 2 @x @x @x@y @x@z The first component of r 2 F1 D

@2 F1 @y 2

@2 F1 : @z 2

If the field lines of F.x; y; z/ are parallel straight lines, in the direction of the constant nonzero vector a say, then

11.

.F  r/r D F1

r  .F  r/

r : r

r  .F  r/ 12. If r 2  D 0 and r 2 r  .r

r.c  r/ D c  .r  r/ C r  .r  c/ C .c  r/r C .r  r/c D 0 C 0 C c C 0 D c: 9.

r.F  r/ D 3F 2.F  r/r .r  F/r r  .r  F/ D F .r  F/r r  .r  F/:

In particular, if r  F D 0 and r  F D 0, then

If c is a constant vector, then its divergence and curl are both zero. By Theorem 3(d), (e), and (f) we have

.c  r/r

@r @r @r C F2 C F3 D F: @x @y @z

Combining all these results, we obtain

8. If r D xi C yj C zk and r D jrj, then

    r  f .r/r D rf .r/  r C f .r/.r  r/ rr C 3f .r/ D f 0 .r/ r 0 D rf .r/ C 3f .r/:

.F  r/r

If r D xi C yj C zk, then r  r D 3 and r  r D 0. Also,

Since r is an arbitrary gradient, div F can have any value, but curl F is perpendicular to a, and thereofore to F.

r  .c  r/ D .r  c/  r c  .r  r/ D 0 r  .c  r/ D .r  r/c C .r  r/c .r  c/r D 3c C 0 0 c D 2c

By Theorem 3(e) and 3(f), r  .F  r/ D .r  r/F C .r  r/F .r  F/r r.F  r/ D F  .r  r/ C r  .r  F/ C .F  r/r C .r  r/F:

div F D div .a/ D r  a curl F D curl .a/ D r  a:

rr D

, for some constant C .

so  is also harmonic.

for some scalar field , which we assume to be smooth. By Theorem 3(b) and (c) we have

r  r D 0;

:

r 2  D r  r D r  F D 0;

F.x; y; z/ D .x; y; z/a

r  r D 3;

3

10. Given that div F D 0 and curl F D 0, Theorem 3(i) implies that r 2 F D 0 too. Hence the components of F are harmonic functions. If F D r, then

Evidently the first components of both sides of the given identity agree. By symmetry, so do the other components. 7.

3

Thus f .r/ D C r

r 2 F is @2 F1 @x 2

(PAGE 929)

D r  r

so r 13.

r.F  r/ D F:

D 0, then r/

C r 2

r

 r

r 2  D 0;

r is solenoidal.

By Theorem 3(c) and (h), r  .r / D r  r C r  r D r  r r  . r/ D r  r r  r D r  r :

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SECTION 16.2 (PAGE 929)

14.

ADAMS and ESSEX: CALCULUS 9

  r  f .rg  rh/

D rf  .rg  rh/ C f r  .rg  rh/  D rf  .rg  rh/ C f .r  rg/  rh

D rf  .rg  rh/ C 0 15.

Look for a solution with G2 D 0. We have Z G3 D xe 2z dy D xye 2z C M.x; z/:

By Theorem 3(b), (d), and (h), we have

 rg  .r  rh/

Try M.x; z/ D 0. Then G3 D xye 2z , and @G3 @G1 D ye 2z C D 2ye 2z : @z @x

0 D rf  .rg  rh/:

If F D r and G D r , then r  F D 0 and r  G D 0 by Theorem 3(h). Therefore, by Theorem 3(d) we have

Thus

r  .F  G/ D .r  F/  G C F  .r  G/ D 0:

Since

G1 D

so r

D F  G;

is a vector potential for F  G. (So is

16. If r  G D F D

r.)

yi C xj, then @G3 @y @G1 @z @G2 @x

@G2 D y @z @G3 Dx @x @G1 D 0: @y

@G1 D 0 we may take N.x; y/ D 0. @y 1 2 G D xzi y k is a vector potential for F. (Of course, 2 this answer is not unique.) Since

If F D xe 2z i C ye 2z j

e 2z k, then

div F D e 2z C e 2z

2e 2z D 0;

so F is solenoidal. If F D r  G, then @G3 @y @G1 @z @G2 @x

614

@G2 D xe 2z @z @G3 D ye 2z @x @G1 D e 2z : @y

e 2z

@N ; @y

18. For .x; y; z/ in D let v D xi C yj C zk. The line segment r.t / D t v, .0  t  1/, lies in D, so div F D 0 on the path. We have

D

@G3 y2 . Thus D0 Again we try M.x; z/ D 0, so G3 D 2 @x and Z G1 D x dz D xz C N.x; y/:

@G1 D @y

we can take N.x; y/ D 0. Thus G D ye 2z i C xye 2z k is a vector potential for F.

G.x; y; z/ D

As in Example 1, we try to find a solution with G2 D 0. Then Z y2 C M.x; z/: G3 D y dy D 2

17.

2ye 2z dz D ye 2z C N.x; y/:

e 2z D

Thus F  G is solenoidal. By Exercise 13, r  .r / D r  r

Z

Z

Z

1 0 1 0

  t F r.t /  v dt

  t F .t /; .t /; .t /  v dt

where  D tx;  D ty;  D t z. The first component of curl G is .curl G/1 Z 1   D t curl .F  v/ dt 1 0  Z 1  @ @ .F  v/3 .F  v/2 dt D t @y @z 0  Z 1  @ @ t D .F1 y F2 x/ .F3 x F1 z/ dt @y @z 0 Z 1 @F2 @F3 @F 1 t 2x t 2x D tF1 C t 2 y @ @ @ 0 ! @F1 C tF1 C t 2 z dt @  Z 1 @F1 @F1 @F1 C t 2y C t 2z dt: D 2tF1 C t 2 x @ @ @ 0 To get the last line we used the fact that d ivF D 0 to @F2 @F3 @F1 replace t 2 x t 2x with t 2 x . Continuing the @ @ @ calculation, we have Z

 d 2 t F1 .; ; / dt 0 dt ˇ1 ˇ D t 2 F1 .tx; ty; t z/ˇˇ D F1 .x; y; z/:

.curl G/1 D

1

0

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 16.3

Similarly, .curl G/2 D F2 and .curl G/3 D F3 . Thus curl G D F, as required.

(f) LHS := Del(F . G): RHS1 := F &x (Del &x G): RHS2 := G &x (Del &x F): RHS3 := F[1]*diff(G,x) +F[2]*diff(G,y)+F[3]*diff(G,z): RHS4 := G[1]*diff(F,x) +G[2]*diff(F,y)+G[3]*diff(F,z): RHS := RHS1 + RHS2 + RHS3 + RHS4: simplify(LHS - RHS);

19. In the following we suppress output (which for some calculations can be quite lengthy) except for the final check on each inequality. You may wish to use semi-colons instead of colons to see what the output actually looks like. >

with(VectorCalculus):

>

SetCoordinates(’cartesian’[x,y,z]):

(PAGE 933)

0 ex > F := VectorField ():

All these zero outputs indicate that the inequalities (a)–(f) of the theorem are valid.

> G := VectorField ():

Section 16.3 Green’s Theorem in the Plane (page 933)

(a) LHS := Del(phi(x,y,z)*psi(x,y,z)): RHS := phi(x,y,z)*Del(psi(x,y,z)) + psi(x,y,z)*Del(phi(x,y,z)): simplify(LHS - RHS); 0 ex 1. (b) LHS := Del . (F*phi(x,y,z)): RHS := (Del(phi(x,y,z))).F phi(x,y,z)*(Del.F): simplify(LHS - RHS);

I

2

.sin x C 3y 2 / dx C .2x e y / dy  ZZ  @ @ 2 .2x e y / .sin x C 3y 2 / dA D @x @y ZZR D .2 6y/ dA Z R Z a D d .2 6r sin  /r dr 0 Z0  Z a D a2 6 sin  d r 2 dr C

+

0 (c) LHS := Del &x (phi(x,y,z)*F): RHS := RHS := (Del(phi(x,y,z))) &x F + phi(x,y,z)*(Del &x F): simplify(LHS - RHS);

0

D a2

0

4a3 :

y

0 ex

C

(d) LHS := Del . (F &x G): RHS := (Del &x F) . G - F . (Del &x G): simplify(LHS - RHS);

R a

0

x

Fig. 16.3-1

(e) LHS := Del &x (F &x G): RHS1 := (Del . G)*F: RHS2 := G[1]*diff(F,x) +G[2]*diff(F,y)+G[3]*diff(F,z): RHS3 := (Del . F)*G: RHS4 := F[1]*diff(G,x) +F[2]*diff(G,y)+F[3]*diff(G,z): RHS := RHS1 + RHS2 - RHS3 - RHS4: simplify(LHS - RHS); 0 ex

a

2.

I

.x 2 xy/ dx C .xy y 2 / dy  ZZ  @ @ 2 D .xy y 2 / .x xy/ dA @x @y ZZT D .y C x/ dA T   1 C1 1D D .y C x/  (area of T ) D 3 C

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SECTION 16.3 (PAGE 933)

ADAMS and ESSEX: CALCULUS 9

y

6. .1;1/

C T 2

x

O Applying the 2-dimensional DiverThen F  TO D G  N. gence Theorem to G, we obtain

Fig. 16.3-2 3.

I

.x sin y 2 C ZZ

D

ZZT

D

T

h

Let R, C, and F be as in the statement of Green’s Theorem. As noted in the proof of Theorem 7, the unit tangent O to C and the unit exterior normal N O satisfy N O DT O  k. T Let G D F2 .x; y/i F1 .x; y/j:

Z

y 2 / dx C .x 2 y cos y 2 C 3x/ dy 2

2

2xy cos y C 3

i 2y/ dA

.2xy cos y ZZ .3 C 2y/ dA D 3 dA C 0 D 3  3 D 9:

C

F1 dx C F2 dy D D

Z

C ZZ

F  TO ds D

Z

C

O ds GN

div G dA  ZZR  @F2 @F1 dA D @x @y R

T

y

2

as required 7.

.1;1/

T

r D sin t i C sin 2t j;

.0  t  2/ y

C

C x

R1

R2

.1; 1/

x

2

Fig. 16.3-3 Fig. 16.3-7

4. Let D be the region x 2 C y 2  9, y  0. Since C is the clockwise boundary of D, I

C

2

2

F D ye x i C x 3 e y j ˇ ˇ i j ˇ @ ˇ @ curl F D ˇˇ @x @y ˇ ˇ ye x 2 x 3 e y

2

x y dx xy dy  ZZ  @ @ 2 2 D . xy / .x y/ dx dy @y D @x ZZ Z  Z 3 81 D : .y 2 C x 2 / dA D d r 3 dr D 4 D 0 0

ZZ

I 1 Area D x dy y dx 2 C Z 2 h 1 a cos3 t 3b sin2 t cos t D 2 0

R1

2

e x /k:

O dS D curl F  N

ZZ

O dS: curl F  N



O dS D 0: curl F  N

R2

Thus

i b sin3 t . 3a cos2 t sin t / dt

I

C

8.

F  dr D

ZZ

R1

C

ZZ

R2

a) F D x 2 j I I ZZ F  dr D x 2 dy D 2x dA D 2Ax: C

616

ˇ ˇ ˇ ˇ ˇ D .3x 2 e y ˇ ˇ ˇ

Observe that C bounds two congruent regions, R1 and R2 , one counterclockwise and the other clockwise. O D k; for R2 , N O D k. Since R1 and R2 are For R1 , N mirror images of each other in the y-axis, and since curl F is an even function of x, we have

5. By Example 1,

Z 3ab 2 2 sin t cos2 t dt D 2 0 Z 3ab 2 sin2 .2t / 3ab D dt D : 2 0 4 8

k @ @z 0

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C

R

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INSTRUCTOR’S SOLUTIONS MANUAL

b) F D xyi I I F  dr D xy dx D C

ZZ

C

2

SECTION 16.4

3. R

x dA D

Ax:

c) F D y i C 3xyj I I F  dr D y 2 dx C 3xy dy C ZZ C D .3y 2y/ dA D Ay:

4.

.0  t  2/:

0

Z

0

5.

2

u.x0 C r cos t; y0 C r sin t / dt;

 Z 2  1 @u @u d ur D cos t C sin t dt dr 2 0 @x @y I 1 O ds ru  N D 2 r Cr

6.

B

div F d V

R ZZZ

R

.x C y C z/ d V D 2.x C y C z/V

If R is the ellipsoid x 2 C y 2 C 4.z 1/2  4, then x D 0, y D 0, z D 1, and V D .4=3/.2/.2/.1/ D 16=3. The flux of F out of R is 2.0 C 0 C 1/.16=3/ D 32=3.

7.

If F D x 2 i C y 2 j C z 2 k, then div F D 2.x C y C z/. Therefore the flux of F out of any solid region R is

B

S

ZZZ

where .x; y; z/ is the centroid of R and V is the volume of R.

In this exercise, the sphere S bounds the ball B of radius a centred at the origin. If F D xi 2yj C 4zk, then div F D 1 2 C 4 D 3. Thus

ZZ ZZZ O dS D

FN 0 d V D 0:

.x C y C z/ d V D 2.x C y C z/V

If F D x 2 i C y 2 j C z 2 k, then div F D 2.x C y C z/. Therefore the flux of F out of any solid region R is Flux D

Section 16.4 The Divergence Theorem in 3-Space (page 938)

2. If F D ye z i C x 2 e z j C xyk, then div F D 0, and

R

If R is the ball .x 2/2 C y 2 C .z 3/2  9, then x D 2, y D 0, z D 3, and V D .4=3/33 D 36. The flux of F out of R is 2.2 C 0 C 3/.36/ D 360.

D2

ZZ ZZZ O dS D

FN 3 d V D 4a3 :

div F d V

R ZZZ

where .x; y; z/ is the centroid of R and V is the volume of R.

Thus ur D limr!0 ur D u.x0 ; y0 /:

S

ZZZ

D2

since ds D r dt . By the (2-dimensional) divergence theorem, and since u is harmonic,

1.

0

If F D x 2 i C y 2 j C z 2 k, then div F D 2.x C y C z/. Therefore the flux of F out of any solid region R is Flux D

and so

ZZ d ur 1 D r  ru dx dy dr 2 r Dr  ZZ  2 @ u @2 u 1 C 2 dx dy D 0: D 2 r Dr @x 2 @y

0

12 5 a : D 5

O the unit normal Note that d r=dt D cos t i C sin t j D N, to Cr exterior to the disk Dr of which Cr is the boundary. The average value of u.x; y/ on Cr is 1 2

If F D x 3 i C 3yz 2 j C .3y 2 z C x 2 /k, then div F D 3x 2 C 3z 2 C 3y 2 , and

ZZ ZZZ O

F  N dS D 3 .x 2 C y 2 C z 2 / d V S B Z 2 Z  Z a D3 d sin  d R4 dR

9. The circle Cr of radius r and centre at r0 has parametrization

ur D

If F D .x 2 C y 2 /i C .y 2 z 2 /j C zk, then div F D 2x C 2y C 1, and

ZZ ZZZ ZZZ 4 O dS D

FN .2xC2yC1/ d V D 1 d V D a3 : 3 S B B

R

r D r0 C r cos t i C r sin t j;

(PAGE 938)

Flux D

ZZZ

D2

div F d V

R ZZZ

R

.x C y C z/ d V D 2.x C y C z/V

where .x; y; z/ is the centroid of R and V is the volume of R.

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SECTION 16.4 (PAGE 938)

ADAMS and ESSEX: CALCULUS 9

If R is the tetrahedron with vertices .3; 0; 0/, .0; 3; 0/, .0; 0; 3/, and .0; 0; 0/, then x D y D z D 3=4, and V D .1=6/.3/.3/.3/ D 9=2. The flux of F out of R is 2..3=4/ C .3=4/ C .3=4//.9=2/ D 81=4.

Thus

ZZZ

D

r  r d V D 2 

the volume of the tetrahedron D being abc=6 cubic units. z

8. If F D x 2 i C y 2 j C z 2 k, then div F D 2.x C y C z/. Therefore the flux of F out of any solid region R is Flux D

ZZZ

D2

R ZZZ

c

back

div F d V side R

x

If R is the cylinder x 2 C y 2  2y (or, equivalently, x 2 C .y 1/2  1), 0  z  4, then x D 0, y D 1, z D 2, and V D .12 /.4/ D 4. The flux of F out of R is 2.0 C 1 C 2/.4/ D 24.

O D k and z D 0, so r  N O D 0, and On the bottom, N the flux out of the bottom face is 0. O D j, so r  N O D x. The On the side, y D 0 and N flux out of the side face is ZZ ZZ ac a a2 c O dS D r  N x dx dz D  D : 2 3 6 side side

div F d V D 3V:

S1

D0C

O dS C FN

ZZ

D

ZZ

D

ZZ

D

10. The required surface integral, ZZ

S

O D i, so the flux out of On the back face, x D 0 and N that face is ZZ ZZ bc b b2 c O dS D r  N y dy dz D  D : 2 3 6 back back Therefore, by the Divergence Theorem

so 11.

ZZ

S

O dS D I D r  N

618

c.a2 C b 2 / abc C . 3 6

F D .x C y 2 /i C .3x 2 y C y 3

x 3 /j C .z C 1/k

div F D 1 C 3.x 2 C y 2 / C 1 D 2 C 3.x 2 C y 2 /: z b

O dS; r  N

can be calculated directly by the methods of Section 6.6. We will do it here by using the Divergence Theorem instead. S is one face of a tetrahedral domain D whose other faces are in the coordinate planes, as shown in the figure. Since  D xy C z 2 , we have r D yi C xj C 2zk;

b2 c abc C0D ; 6 3

a2 c 6

I

dS D AR

where A is the area of D. By the Divergence Theorem, 3V D AR, so V D AR=3.

I D

(We used the fact that MxD0 D area  x and x D a=3 for that face.)

O dS FN

FF R2 dS D R R

bottom

The flux of r out of D is the sum of its fluxes out of the four faces of the tetrahedron.

The region C described in the statement of the problem is the part of a solid cone with vertex at the origin that lies inside a ball of radius R with centre at the origin. The surface S of C consists of two parts, the conical wall S1 , and the region D on the spherical boundary of the ball. At any point P on S1 , the outward normal O is perpendicular to the line OP , that is, to F, so field N O D 0. At any point P on D, N O is parallel to F, in FN O fact N D F=jFj D F=R. Thus ZZ ZZ O dS D

FN

a

Fig. 16.4-10

9. If F D xi C yj C zk, then div F D 3. If C is any solid region having volume V , then

C

y

b

where .x; y; z/ is the centroid of R and V is the volume of R.

S

S D

.x C y C z/ d V D 2.x C y C z/V

ZZZ

abc abc D ; 6 3

r  r D r 2  D 2:

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O N S

D B x

a

a

k Fig. 16.4-11

y

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 16.4

O D On the back, x D 0, N

Let D be the conical domain, S its conical surface, and B its base disk, as shown in the figure. We have ZZZ

D

div F d V D

Z

2

d Z a

0

Z

a

r dr

0

Z

b.1 .r=a//

0

ZZ

.2 C 3r 2 / dz

r dr r.2 C 3r 2 / 1 D 2b a 0  Z a 2r 2 3r 4 2r C 3r 3 D 2b dr a a 0 3a4 b 2a2 b C : D 3 10

O D On B we have z D 0, N ZZ

B

O dS D FN



O D k, F  N

ZZ

S

O dS C FN

ZZ

O dS D FN

B

O dS D 2 FN

bottom

S

D

d 0

Z

a

r cos  r dr 0

ˇ=2 ˇ a3 ˇ D sin  ˇ  ˇ 3

Z

O D 2x, so k, F  N

=2

d

0

Z

a

0

r cos  r dr D

ZZ

a2 :

D

2a3 : 3

S

a3 2a3 a3 C D : 3 3 6

O dS C 0 FN

Hence the flux of F upward through S is

ZZZ

ZZ

div F d V;

D

3a4 b 2a2 b C C a2 : 3 10

13.

3 O dS D a FN 6 S

a3 : 3

e x sin y/k

F D .x C yz/i C .y xz/j C .z div F D 1 C 1 C 1 D 3: z

12. F D .y C xz/i C .y C yz/j .2x C z 2 /k div F D z C .1 C z/ 2z D 1. Thus ZZZ

a3 : 3

By the Divergence Theorem

so the flux of F upward through the conical surface S is ZZ

=2

y, so

0

O D On the bottom, z D 0, N

By the Divergence Theorem, ZZ

Z

O dS D FN D

1, so

area of B D

back

O D i, F  N

(PAGE 938)

O N a3 ; 6

div F d V D volume of D D

S2

2a

D

a

y x

where D is the region in the first octant bounded by the sphere and the coordinate planes. The boundary of D consists of the spherical part S and the four planar parts, called the bottom, side, and back in the figure.

O N

S1

z a

Fig. 16.4-13

back side

a) The flux of F out of D through S D S1 [ S2 is

S

ZZ ZZZ O dS D

FN div F d V

D

S

a x

y

a

bottom

ZZ

side

D

2

d 0

D 12

Fig. 16.4-12 O D On the side, y D 0, N

D3

Z

O D 0, so j, F  N

O dS D 0: FN

Z

Z

2a

r dr

a

2a

p r 4a2

Z

p

4a2 r 2

2 dz 0

r 2 dr

a

Let u D 4a2 r 2 du D 2r dr Z 3a2 p D 6 u1=2 du D 12 3a3 : 0

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SECTION 16.4 (PAGE 938)

ADAMS and ESSEX: CALCULUS 9

xi C yj , dS D a d dz. The flux of F a out of D through S1 is

O D On the back, x D 0, N

O D b) On S1 , N ZZ

S1

O dS D FN D

ZZ

x2

a

S1

a

Z

2

y 2 C xyz

xyz p

Z

2

d

0

3a

dz D

p 3a

ZZ

back

a d dz

ZZ

D3

Z

D 1

Z

dx 0

D3

d

0

Z

1

front

D 1 1

y

bottom

Fig. 16.4-14

side

O D On the bottom, z D 0, N ZZ

620

bottom

O dS D FN

O D x, so j, F  N 1

x dx 0

Z

1

0

dz D

1 : 2

O D y, so k, F  N Z

1

y dy 0

Z

0

1 2

1

dx D

1 : 2

3 : 16

1 2

0

3 D 16

1:

Now

ZZZ

2z C 6/ d V:

R

R

x d V D MxD0 D V x, where R has volume V

and centroid .x; y z/. Similar formulas obtain for the other variables, so the required flux is

16.

2V z C 6V:

F D xi C yj C zk implies that div F D 3. The total flux of F out of D is ZZ ZZZ O dS D 3

FN d V D 12; bdry of D

S

Z

r 2 cos2  r dr D

S

1

O dS D FN

0

ZZ O dS D 2V x C 4V y

FN

back

ZZ

S

0

z

O D On the side, y D 0, N

1

ZZ ZZZ O dS D

FN .2x C 4y

r 2 cos2  r dr

The boundary of D consists of the cylindrical surface S and four planar surfaces, the side, bottom, back, and front.

x

0

Z

The flux of F out of R through its surface S is

3 1   D : 4 4 16

side

d

F D .x 2 x 2y/i C .2y 2 C 3y z/j .z 2 4z C xy/k div F D 2x 1 C 4y C 3 2z C 4 D 2x C 4y 2z C 6:

yk;

=2

=2

O dS D 3 .3xz 2 i xj yk/  N 16 S

then div F D 3z 2 , so the total flux of F out of D is ZZ ZZZ O dS D

FN 3z 2 d V bdry of D

Z

ZZ 15.

xj

front

O dS D 3 FN

Hence,

Let D be the domain bounded by S, the coordinate planes, and the plane x D 1. If F D 3xz 2 i

O dS D 0: FN

O D i, F  N O D 3z 2 , so On the front, x D 1, N

p 4 3a3 :

c) The flux of F out of D through the spherical part S2 is ZZ ZZ ZZ O dS D F  N O dS O dS FN FN S2 S S1 p p p D 12 3a3 C 4 3a3 D 16 3a3 : 14.

O D 0, so i, F  N

D

since the volume of D is half that of a cube of side 2, that is, 4 square units. D has three triangular faces, three pentagonal faces, and a hexagonal face. By symmetry, the flux of F out of each triangular face is equal to that out of the triangular face T O D k  k D 1 on that face, in the plane z D 1. Since F  N these fluxes are ZZ 1 dx dy D area of T D : 2 T Similarly, the flux of F out of each pentagonal face is equal to the flux out of the pentagonal face P in the plane O D k  . k/ D 1; that flux is z D 1, where F  N ZZ

P

dx dy D area of P D 4

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7 1 D : 2 2

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 16.4

In addition,

Thus the flux of F out of the remaining hexagonal face H is   7 1 C D 0: 12 3  2 2

ˇ ˇ ˇ 1 ˇˇ curl G D ˇ 3ˇ ˇ

(This can also be seen directly, since F radiates from the origin, so is everywhere tangent to the plane of the hexagonal face, the plane x C y C z D 0.) . 1;0;1/

T

.0; 1;1/

ZZ

D

H D

y

i @ @x y3

j @ @y x3

19.

F  k dA D 3

S

x

20.

21.

then d ivF D 2x C 2y. By the Divergence Theorem, S

ZZ

D

F  . k/ dx dy D

ZZZ

R

div F d V D 0

because R is symmetric about x D 0 and y D 0. Thus the flux of F outward across S is ZZ ZZ O dS D FN .3 C x/ dx dy D 3.3a2 / D 9a2 : S

D

ZZ

S

O dS C FN

ZZ

D

F  . k/ dA D

ZZZ

ZZZ

R

div F d V D

ZZZ

22.

R

ZZ

r 3 dr D

3 : 2

x d V D MxD0 D V x.

Taking F D r in the first identity in Theorem 7(a), we have ZZ ZZZ O dS D

r  N curl r d V D 0; S

D

since r  r D 0 by Theorem 3(h). 23.

div .F/ D div F C r  F by Theorem 3(b). Thus ZZZ

D

div F d V C

ZZZ

D

r  F d V D

ZZZ

div .F/ d V ZZ D O dS D F  N

div F d V:

.2 C   0/ d V D 2.5/ D 10:

0

We use Theorem 7(b), the proof of which is given in Exercise 29. Taking .x; y; z/ D x 2 C y 2 C z 2 , we have

S

R

Now div curl G D 0 by Theorem 3(g). Also div r D div .2xi 2yj C 2zk/ D 2 2 C 2 D 2. Therefore

1

If r D xi C yj C zk, then div r D 3 and

since

18.  D x 2 y 2 C z 2 , G D 13 . y 3 i C x 3 j C z 3 k/. F D r C curl G. Let R be the region of 3-space occupied by the sandpile. Then R is bounded by the upper surface S of the sandpile and by the disk D: x 2 C y 2  1 in the plane z D 0. The outward (from R) normal on D is k. The flux of F out of R is given by

0

Z

ZZ ZZ 1 O dS D 1  N O dS

.x 2 C y 2 C z 2 /N 2V S 2V S ZZZ 1 D grad  d V 2V ZZZ D 1 .xi C yj C zk/ d V D V D r;

2

O dS C FN

d

ZZ ZZZ 1 O dS D 1

rN 3 d V D V: 3 S 3 D

F D .x 2 C y C 2 C z 2 /i C .e x C y 2 /j C .3 C x/k;

ZZ

2

D

Fig. 16.4-16 The part of the sphere S: x 2 C y 2 C .z a/2 D 4a2 above z D 0 and the disk D: x 2 C y 2 D 3a2 in the xy-plane form the boundary of a region R in 3-space. The outward normal from R on D is k. If

Z

ˇ ˇ ˇ ˇ ˇ D 3.x 2 C y 2 /k; ˇ ˇ ˇ

The flux of F out of S is 10 C .3/=2. ZZ ZZZ O dS D

curl F  N div curl F D 0, by Theorem

3(g).

P

17.

k @ @z z3

and r  k D 2z D 0 on D, so

z

. 1; 1;1/

(PAGE 938)

by the Divergence Theorem. 24.

If F D r in the previous exercise, then div F D r 2  and ZZZ

D

r 2  d V C

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ZZZ

D

ZZ O dS: jrj2 d V D r  N S

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SECTION 16.4 (PAGE 938)

ADAMS and ESSEX: CALCULUS 9

If r 2  D 0 in D and  D 0 on S, then ZZZ

D

Hence, by the Divergence Theorem, ZZZ ZZZ .r 2 r 2 / d V D div .r r/ d V D ZZ D O dS D .r r/  N  ZZS  @ @ dS: D  @n @n S

jrj2 d V D 0:

Since  is assumed to be smooth, r D 0 throughout D, and therefore  is constant on each connected component of D. Since  D 0 on S, these constants must all be 0, and  D 0 on D.

29.

25. If u and v are two solutions of the given Dirichlet problem, and  D u v, then r 2  D r 2 u r 2 v D f f D 0 on D  D u v D g g D 0 on S:

S

By the previous exercise,  D 0 on D, so u D v on D. That is, solutions of the Dirichlet problem are unique.

Thus c

26. Re-examine the solution to Exercise 24 above. If O D 0 on S, then we r 2  D 0 in D and @=@n D r  N can again conclude that ZZZ

D

30.

D

D

D

 div F

 div F.P0 / d V:

 max jdiv F

r  r d V

P in D

div F.P0 /j

! 0 as  ! 0 C assuming div F is continuous: ZZ 1 O dS D div F.P0 /:

FN lim !0C vol.D / S

Section 16.5 Stokes’s Theorem

r/

D r  r

622

ZZZ

ˇ ˇ ZZ ˇ ˇ 1 ˇ ˇ O ˇ vol.D / F  N dS div F.P0 /ˇ  S ZZZ 1  jdiv F div F.P0 /j d V vol.D / D

ZZ ZZ O dS D @ dS: D r  N S S @n

D r

S

1 vol.D /

Thus

28. By Theorem 3(b), div .r

S

ZZ ZZZ 1 1 O dS D

FN div F d V vol.D / S vol.D / D "ZZZ 1 D div F.P0 / d V vol.D / D # ZZZ   C div F div F.P0 / d V D div F.P0 / C

Apply the Divergence Theorem to F D r: ZZZ

r d V

D

so  is constant on any connected component of S, and u and v can only differ by a constant on S.

r2 d V D

D

S

 ZZ O dS D 0:

N

D

r 2  D r 2 u r 2 v D f f D 0 on D @u @v @ D D g g D 0 on S; @n @n @n

ZZZ

ZZZ

Since c is arbitrary, the vector in the large parentheses must be the zero vector. Hence ZZZ ZZ O dS: r d V D  N

jrj d V D 0

and r D 0 throughout D. Thus  is constant on the connected components of D. (We can’t conclude the constant is 0 because we don’t know the value of  on S.) If u and v are solutions of the given Neumann problem, then  D u v satisfies

27.

If F D c, where c is an arbitrary, constant vector, then div F D r  c, and by the Divergence Theorem, ZZZ ZZZ c r d V D div F d V D ZZ D O dS D FN S ZZ ZZ O dS D c   N O dS: D c  N

2

1. C r 2 2

r :

r

 r

(page 943)

The triangle T lies in the plane x C y C z D 1. We use the downward normal

r2

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O D N

iCjCk p 3

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 16.5

on T , because of the given orientation of its boundary. If F D xyi C yzj C zxk, then ˇ ˇ ˇ i j k ˇ ˇ @ ˇ @ @ ˇ ˇ curl F D ˇ ˇ D yi zj xk: ˇ @x @y @z ˇ ˇ xy yz zx ˇ

Therefore I I xy dx C yz dz C zx dz D F  dr C C ZZ ZZ y CzCx O dS D dS D curl F  N p 3 T T ZZ 1 1 D p dS D p  (area of T ) 3 T 3 p ! 3 1 1 1 p  2 p D p  D : 2 2 3 2

(PAGE 943)

dx dy on S, we have O kN I ZZ O dS x dy C z 2 dz D F  dr D curl F  N C S ZZ O dx dy D 8: D 2k  N O kN D

Since dS D I

3.

y dx C

Let C be the circle x 2 C y 2 D a2 ; z D 0, oriented counterclockwise as seen from the positive z-axis. Let D be the disk bounded by C, with normal k. We have F D 3yi 2xzj C .x 2 y 2 /k ˇ ˇ ˇ i ˇ j k ˇ ˇ @ @ ˇ @ ˇ ˇ ˇ curl F D ˇ ˇ @x @y @z ˇ ˇ 2 2ˇ ˇ 3y 2xz x y D 2.x

z

y/i

2xj

.2z C 3/k:

Applying Stokes’s Theorem (twice) we calculate ZZ I ZZ D F  dr D curl F  k dA S CZZ D D 3 dA D 3a2 :

1

C T

D

1 y x

z

1

O N

Fig. 16.5-1 2. Let S be the part of the surface z D y 2 lying inside the O cylinder x 2 C y 2 D 4, and having upward normal N. Then C is the oriented boundary of S. Let D be the disk x 2 C y 2  4, z D 0, that is, the projection of S onto the xy-plane.

S k D

C

Fig. 16.5-3

O N

4.

The surface S with equation

S

x 2 C y 2 C 2.z

D y x

Fig. 16.5-2 If F D yi

2

xj C z k, then ˇ ˇ i j ˇ ˇ @ @ curl F D ˇˇ ˇ @x @y ˇ y x

y

C

x

z

k @ @z z2

ˇ ˇ ˇ ˇ ˇD ˇ ˇ ˇ

2k:

1/2 D 6;

z  0;

O is that part of an ellipsoid of revwith outward normal N, olution about the z-axis, centred at .0; 0; 1/, and lying above the xy-plane. The boundary of S is the circle C: x 2 C y 2 D 4, z D 0, oriented counterclockwise as seen from the positive z-axis. C is also the oriented boundary O D k. of the disk x 2 C y 2  4, z D 0, with normal N 3 3 z x 2 Cy 2 Cz 2 If F D .xz y cos z/i C x e j C xyze k, then, on z D 0, we have ˇˇ  @ @ 3 z ˇ 3 x e .xz y cos z/ ˇ curl F  k D ˇ @x @y zD0  ˇˇ 2 z 2 2 ˇ D 3x e C 3y cos z ˇ D 3.x C y 2 /: zD0

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623

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SECTION 16.5 (PAGE 943)

Thus ZZ

S

ADAMS and ESSEX: CALCULUS 9

If D is the disk x 2 C y 2  1 in the xy-plane, then

I

ZZ F  dr D curl F  k dA C D Z 2 Z 2 D d 3r 2 r dr D 24:

O dS D curl F  N

0

C

ZZ O dS D curl F  N 3.x 2 C y 2 / dx dy S D Z 2 Z 1 3 D3 d : r 2 r dr D 2 0 0

F  dr D

0

5. The circle C of intersection of x 2 C y 2 C z 2 D a2 and x C y C z D 0 is the boundary of a circular disk of radius a in the plane x C y C z D 0. If F D yi C zj C xk, then ˇ ˇ i ˇ @ ˇ curl F D ˇ ˇ @x ˇ y

I

j @ @y z

k @ @z x

ˇ ˇ ˇ ˇ ˇD ˇ ˇ

7.

The part of the paraboloid z D 9 x 2 y 2 lying above the O has boundary the circle xy-plane having upward normal N 2 2 C: x C y D 9, oriented counterclockwise as seen from above. C is also the oriented boundary of the plane disk O D k. x 2 C y 2  9, z D 0, oriented with normal field N yi C x 2 j C zk, then

If F D

.i C j C k/:

ˇ ˇ ˇ ˇ curl F D ˇˇ ˇ ˇ

If C is oriented so that D has normal O D N O D then curl F  N I

C

p

iCjCk ; p 3

I

ZZ O dS F  dr D curl F  N C ZZ D p p dS D 3a2 ; D 3

since D has area a2 .

r D cos t i C sin t j C sin 2t k;

0  t  2;

lies on the surface z D 2xy, since sin 2t D 2 cos t sin t . It also lies on the cylinder x 2 Cy 2 D 1, so it is the boundary of that part of z D 2xy lying inside that cylinder. Since C is oriented counterclockwise as seen from high on the z-axis, S should be oriented with upward normal, O D p 2yi 2xj C k ; N 1 C 4.x 2 C y 2 /

and has area element

F  dr D D

8.

ZZ

ZZD

k @ @z z

ˇ ˇ ˇ ˇ ˇ D .2x C 1/k: ˇ ˇ ˇ

D

.curl F  k/ dA .2x C 1/ dA D 0 C .32 / D 9:

The closed curve

y 3 /i C .e y C x 3 /j C e z k; then j @ @y ey C x3

k @ @z ez

ˇ ˇ ˇ ˇ ˇ D 3.x 2 C y 2 /k: ˇ ˇ ˇ

cos t

sin t /k;

.0  t  2/, lies in the plane x C y C z D 3 and is oriented counterclockwise as seen from above. Therefore it is the boundary of a p region S in that plane with normal O D .i C j C k/= 3. The projection of S onto the field N xy-plane is the circular disk D of radius 1 with centre at .1; 1/. If F D ye x i C .x 2 C e x /j C z 2 e z k, then ˇ ˇ i ˇ ˇ @ curl F D ˇˇ ˇ @xx ˇ ye

By Stokes’s Theorem,

p dS D 1 C 4.x 2 C y 2 / dx dy:

ˇ ˇ i ˇ ˇ @ curl F D ˇˇ ˇ x @x 3 ˇe y

j @ @y x2

r D .1 C cos t /i C .1 C sin t /j C .1

6. The curve C:

624

I

C

D

If F D .e x

i @ @x y

By Stokes’s Theorem, the circulation of F around C is

3 on D, so

y dx C z dy C x dz D

ZZ

I

C

j @ @y x2 C ex

ˇ ˇ k ˇ @ ˇ ˇ D 2xk: @z ˇˇ z2 C ez ˇ

ZZ

O dS curl F  N ZZ 2x p 2x D p dS D p . 3/ dx dy 3 3 D S D 2xA D 2;

F  dr D

ZZS

where x D 1 is the x-coordinate of the centre of D, and A D 12 D  is the area of D.

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 16.5

9. If S1 and S2 are two surfaces joining C1 to C2 , each having upward normal, then the closed surface S3 consisting of S1 and S2 (that is, S2 with downward normal) bound a region R in 3-space. Then ZZ

S1

ZZ

O dS FN D

ZZS2

O dS FN O dS C FN

11.

As was shown in Exercise 13 of Section 7.2, r  .r / D

ZZ

I

O dS FN

S3

D

z/i C .xy C y 3 C z/j C ˇy 2 .z C 1/k;

O dS D FN

3

D

3

ZZ

Z

H 

0

y 2 dx dy Z sin2  d

1 0

r 3 dr D

r  r

ˇ ˇ i ˇ @ ˇ ˇ curl F D ˇ @x ˇ 2 ˇ z C y 2 C sin x 2 1/i C zj:

j @ @y 2xy C z

ˇ ˇ k ˇ @ ˇ ˇ ˇ @z ˇ xz C 2yz ˇ

By Stokes’s Theorem, I

C

ZZ

ZZ

ZZS

ZZS ZZS

S

O dS r  .r /  N O dS .r  r /  N O dS r  . r/  N O dS: .r  r /  N r.

12. We are given that C bounds a region R in a plane P with O D aiCbjCck. Therefore, a2 Cb 2 Cc 2 D 1. unit normal N If F D .bz cy/i C .cx az/j C .ay bx/k, then ˇ i ˇ ˇ @ ˇ curl F D ˇ ˇ @x ˇ bz cy

3 : 8

j @ @y cx

k @ @z az

D 2ai C 2bj C 2ck:

ay

ˇ ˇ ˇ ˇ ˇ ˇ bx ˇ

O D 2.a2 C b 2 C c 2 / D 2. We have Hence curl F  N 1 2

I

.bz C

13.

cy/ dx C .cx az/ dy C .ay bx/ dz I ZZ 1 1 O dS D F  dr D curl F  N 2 C 2 R ZZ 1 D 2 dS D area of R: 2 R

The circle C of radius  centred at P is the oriented boundary of the disk S of area  2 having constant norO By Stokes’s Theorem, mal field N. I

C

F  dr D

O dS curl F  N S ZZ 1 D p .2.2z 1/ C z/ dS 6 S 5z 2 p D p .8 6/ D 24: 6

F  dr D

 / D r  r :

is solenoidal, with potential r , or

F D .z 2 C y 2 C sin x 2 /i C .2xy C z/j C .xz C 2yz/k;

D .2z

r D

C

10. The curve C: .x 1/2 C 4y 2 D 16, 2x C y C z D 3, oriented counterclockwise as seen from above, bounds an elliptic disk S on the p plane 2x C y C z D 3. S has normal O D .2i C j C k/= 6. Since its projection onto the xyN plane is an elliptic disk with centre at p .1; 0; 0/ and area .4/.2/ D 8, therefore S has area 8 6 and centroid .1; 0; 1/. If

then

D

I

R

we have div F D 2˛x C x C 3y 2 C ˇy 2 D RR0 if ˛ D 1=2 O dS for and ˇ D 3. In this case we can evaluate S F  N any such surface S by evaluating the special case where S is the half-disk H : x 2 C y 2  1, z D 0, y  0, with O D k. We have upward normal N S

D

r

C

provided that div F D 0 identically. Since

ZZ

r .

Thus, by Stokes’s Theorem,

S2 ZZ S1 ZZZ O D F  N dS D ˙ div F d V D 0;

F D .˛x 2

(PAGE 943)

D

ZZ

S

ZZ

O dS curl F  N

O dS curl F.P /  N ZZ   O dS C curl F curl F.P /  N S

S

O D  2 curl F.P /  N ZZ   O dS: C curl F curl F.P /  N S

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625

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SECTION 16.5 (PAGE 943)

ADAMS and ESSEX: CALCULUS 9

Since F is assumed smooth, its curl is continuous at P . Therefore F  dr C ZZ ˇ 1 ˇ  ˇ curl F  2 S

max jcurl F.Q/ S ! 0 as  ! 0C. Thus lim

Q on

I

y x

ˇ ˇ Oˇ curl F.P /  N ˇ

ˇ I ˇ 1 ˇ ˇ  2 

z

!0C C

z

ˇ  O ˇˇ dS curl F.P /  N

dS

O N S

R

curl F.P /j

O F  d r D curl F.P /  N. Fig. 16.6-1

Section 16.6 Some Physical Applications of Vector Calculus (page 950)

1.

a) If we measure depth in the liquid by z, so that the zaxis is vertical and z D 0 at the surface, then the pressure at depth z is p D gz, where  is the density of the liquid. Thus rp D

ZZ

gk D g;

S2

where g D gk is the constant downward vector acceleration of gravity. The force of the liquid on surface element dS of the solid O is with outward (from the solid) normal N dB D

b) The above argument extends to the case where the solid is only partly submerged. Let R be the part of the region occupied by the solid that is below the surface of the liquid. Let S D S1 [ S2 be the boundary of R , with S1  S and S2 in the plane of the surface of the liquid. Since p D gz D 0 on S2 , we have

Therefore the buoyant force on the solid is

O dS D . gz/N O dS D gz N O dS: pN BD

Thus, the total force of the liquid on the solid (the buoyant force) is ZZ O dS B D gz N S ZZZ D r.gz/ d V R ZZZ D g d V D

O dS D 0: gz N

D

ZZ

ZZS1

O dS gz N O dS C gz N

ZZ

ZZ S1 O dS D gz N S ZZZ D g d V D

(see Theorem 7)

R

S2

O dS gz N

M  g;

M g;

R

where M D

ZZZ

 d V is the mass of the liquid which R

would occupy the same space as the solid. Thus B D F, where F D M g is the weight of the liquid displaced by the solid.

626

where M  D

ZZZ

 d V is the mass of the liquid R

which would occupy R . Again we conclude that the buoyant force is the negative of the weight of the liquid displaced.

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 16.6

5.

This derivation is similar to that of the continuity equation for fluid motion given in the text. If S is an (imaginary) surface bounding an arbitrary region D, then the rate of change of total charge in D is @ @t

S2

R

O is .F1 G/  N. O Applying 2. The first component of F.G  N/ the Divergence Theorem and Theorem 3(b), we obtain ZZ ZZZ O dS D

.F1 G/  N div .F1 G/ d V S ZZZD   D rF1  G C F1 r  G dS: But rF1  G is the first component of .G  r/F, and F1 r  G is the first component of Fdiv G. Similar results obtain for the other components, so

6.

bj2 D .x b1 /2 C .y b2 /2 C .z @ jr bj D 2.x b1 / 2jr bj @x @ x b1 jr bj D : @x jr bj

ZZ ZZZ ZZZ O dS D

EN div E d V D k  d V D kQ; R

 d V is the total charge in R.

4. If f is continuous and vanishes outside a bounded region (say the ball of radius a centred at r), then jf .; ; /j  K, and, if .R; ;  / denote spherical coordinates centred at r, then Z a 2 Z  Z 2 R jf .s/j sin  d d d V  K dR s 0 R 0 0 R3 jr sj D 2Ka2 a constant.

ZZZ

b3 /2

Similar formulas hold for the other first partials of jr so   1 r jr bj   @ 1 @ D jr bji C    C jr bjk jr bj2 @x @z 1 .x b1 /i C .y b2 /j C .z b3 /k D jr bj2 jr bj r b D : jr bj3

3. Suppose the closed surface S bounds a region R in which charge is distributed with density . Since the electric field E due to the charge satisfies div E D k, the total flux of E out of R through S is, by the Divergence Theorem,

R

D

Since r D xi C yj C zk and b D b1 i C b2 j C b3 k, we have jr

D

RRR

D

@ d V; @t

@ C div J D 0: @t

ZZ ZZZ   O dS D

F.G  N/ Fdiv G C .G  r/F d V:

where Q D

ZZZ

Since D is arbitrary and we are assuming the integrand is continuous, it must be 0 at every point:

D

R

D

 dV D

O is the outward (from (The negative sign occurs because N D) normal on S.) Thus we have  ZZZ  @ C div J d V D 0: @t D

Fig. 16.6-1

S

ZZZ

where  is the charge density. By conservation of charge, this rate must be equal to the rate at which charge is crossing S into D, that is, to I ZZZ O dS D . J/  N div J d V:

S1

S

S

(PAGE 950)

7.

bj,

Using the result of Exercise 4 and Theorem 3(d) and (h), we calculate, for constant a,   r b div a  jr bj3   1 D div a  r jr bj 1 1 D .r  a/  r Car r D 0 C 0 D 0: jr bj jr bj

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SECTION 16.6 (PAGE 950)

ADAMS and ESSEX: CALCULUS 9

8. For any element d s on the filament F, we have   r s div d s  D0 jr sj3

12. By analogy with the filament case, the current in volume element d V at position s is J.s/ d V , which gives rise at position r to a magnetic field d B.r/ D

by Exercise 5, since the divergence is taken with respect to r, and so s and d s can be regarded as constant. Hence div

I

  I d s  .r s/ r s D div d s  D 0: jr sj3 F jr sj3 F

If R is a region of 3-space outside which J is identically zero, then at any point r in 3-space, the total magnetic field is ZZZ 1 J.s/  .r s/ B.r/ D d V: 4 jr sj3 R

9. By the result of Exercise 4 and Theorem 3(e), we calculate curl

  r b a jr bj3   1 D curl a  r jr bj     1 1 D r r r a a r jr bj jr bj 1 1 C .r  a/r C .a  r/r : jr bj jr bj

Observe that r  r

1 jr

bj

Now A.r/ was defined to be A.r/ D

13.

11.

14.

Using the results of Exercises 7 and 8, we have curl

I

  I d s  .r s/ r s D curl d s  D0 jr sj3 F jr sj3 F

for r not on F. (Again, this is because the curl is taken with respect to r, so s and d s can be regarded as constant for the calculation of the curl.)

628

I 4 I div A.r/ D 4 I D 4 A.r/ D

I

jr IF

ds sj 

 1 div r ds jr sj  IF  1  ds r jr sj F (by Theorem 3(b)) D 0 for r not on F, since r.1=jr sj/ is conservative.

Similarly, the other components have zero line integrals, so .d s  r/F.s/ D 0:

R

J.s/ d V: jr sj

  ZZZ 1 1 J.s/ d V rr  4 jr sj ZZZR 1 1 D  J.s/ d V rr 4 jr sj R (by Theorem 3(c)) ZZZ .r s/  J.s/ 1 dV D 4 jr sj3 R (by Exercise 4) D B.r/:

10. The first component of .d s  r/F.s/ is rF1 .s/  d s. Since F is closed and rF1 is conservative, I I i  .d s  r/F.s/ D rF1 .s/  d s D 0: F F

F

ZZZ

curl A.r/ D

calculation or by noting that r

I

1 4

We have

D 0 for r ¤ b, either by direct

1 is the field of a jr bj point source at r D b and applying the result of Example 3 of Section 7.1.   1  r a D 0 and r  a D 0, since a is Also r jr bj constant. Therefore we have   r b 1 curl a  D .a  r/r jr bj3 jr bj r b D .a  r/ : jr bj3

1 J.s/  .r s/ d V: 4 jr sj3

ZZZ J.s/ d V 1 , where R is a region of 3-space 4 sj R jr such that J.s/ D 0 outside R. We assume that J.s/ is continuous, so J.s/ D 0 on the surface S of R. In the following calculations we use subscripts s and r to denote the variables with respect to which derivatives are taken. By Theorem 3(b),

A.r/ D

div s

  1 1 J.s/ D rs r s  J.s/  J.s/ C jr sj jr sj jr sj   1 D rr  J.s/ C 0 jr sj

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 16.7

because r r jr sj D r s jr sj, and because r  J D r  .r  B/ D 0 by Theorem 3(g). Hence

(PAGE 961)

This internal energy increases at (time) rate dH D c dt

 ZZZ  1 1 div A.r/ D rr  J.s/ d V 4 jr sj R ZZZ 1 J.s/ D dV rs  4 jr sj ZZ R J.s/ 1 O dS D 0

N D 4 S jr sj

ZZZ

R

@T d V: @t

If heat is not “created” or “destroyed” (by chemical or other means) within R, then the increase in internal energy must be due to heat flowing into R across S. The rate of flow of heat into R across surface element dS O is with outward normal N

since J.s/ D 0 on S.

O dS: krT  N

By Theorem 3(i), r2A D

J D r  B D r  .r  A/ D r.r  A/

Therefore, the rate at which heat enters R through S is

r 2 A:

ZZ O dS: k rT  N S

15.

By Maxwell’s equations, since  D 0 and J D 0, div E D 0 curl E D

div B D 0

@B @t

0

curl B D 0

By conservation of energy and the Divergence Theorem we have

@E @t

c

Therefore, r2E D

curl curl E D grad div E r2E D

curl curl E D 0

@2 E @ curl B D 0 0 2 : @t @t Thus,

1 : 0  0

@B ¤ 0: Thus in the @t non-static case we cannot have E D r.

On the other hand, we can still say that curl A D B since div curl A D div B D 0 because there are no magnetic monopoles.

1.

d V D 0.



@2 T @2 T @2 T C C 2 2 2 @x @y @z



:

f .r; ; z/ D r z 9,

(cylindrical coordinates). By Example @f 1 @f O @f C k rO C @r r @ @z D  z rO C z O C r k:

rf D @curl A D0 @t

@B D @t

@B : @t 2.

18. The internal energy of an arbitrary region R (with surface S) at time t is H.t / D c



Section 16.7 Orthogonal Curvilinear Coordinates (page 961)

@A , then @t

curl E D curl r

k 2 r T c

k 2 k @T D r T D @t c c

16. curl . r/ D 0, but curl E D

r

@T @t

Since R is arbitrary, and the temperature T is assumed to be smooth, the integrand must vanish everywhere. Thus

Thus U D E and U D B both satisfy the wave equation

If E D

ZZZ  R

@2 B r B D 0  0 2 : @t

where c 2 D

ZZ @T O dS d V D k rT  N @t S ZZZ Dk r  rT d V ZZZR Dk r 2 T d V: R

2

17.

R

r2E

Similarly,

@2 U D c 2 r 2 U; @t 2

ZZZ

ZZZ

T .x; y; z; t / d V: R

f .R; ;  / D R (spherical coordinates). By Example 10, 1 @f O @f O 1 @f O RC rf D C  @R R @ R sin  @ O C  O C  O : D  R sin 

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SECTION 16.7 (PAGE 961)

3.

4.

5.

6.

7.

F.r; ; z/ D r rO   1 @ 2 .r / D 2 div F D r @r ˇ ˇ rO r O k ˇ 1 ˇˇ @ @ @ curl F D ˇ r ˇ @r @ @z ˇ r 0 0

F.r; ; z/ D r O   1 @ div F D .r/ D 0 r @ ˇ ˇ rO r O k ˇ @ @ 1 ˇˇ @ curl F D ˇ r ˇ @r @ @z ˇ 0 r2 0

9.

ˇ ˇ ˇ ˇ ˇ D 0: ˇ ˇ ˇ

uO D

1 hu 1 D hu

rf .u; v/ D

vO D

1 @r : hv @v



O F.R; ;  / D R R    1 @ div F D 2 R4 sin  D 4R R sin  @R ˇ ˇ ˇ R O R O R sin  O ˇˇ ˇ ˇ ˇ @ 1 @ @ ˇ ˇ curl F D 2 ˇ D 0: ˇ ˇ R sin  ˇ @R @ @ ˇ ˇ ˇ ˇ R2 0 0

1 @f uO C @u hv 1 @f uO C @u hv

1 @f @f vO C k @v 1 @z @f vO : @v

For F.u; v/ D Fu .u; v/ uO C Fv .u; v/ vO (independent of z and having no k component), we have  @ @ .hu Fu / C .hv Fv / @u @v ˇ ˇ ˇ hu uO k ˇ hv vO ˇ ˇ @ @ ˇˇ 1 ˇˇ @ curl F.u; v/ D @v @z ˇˇ hu hv ˇˇ @u ˇ hu Fu hv Fv 0 ˇ   @ @ 1 .hv Fv / .hu Fu / k: D hu hv @u @v div F.u; v/ D

11.

1 hu hv



We can use the expressions calculated in the text for cylindrical coordinates, applied to functions independent of z and having no k components: 1 @f @f rO C @r r @ @Fr Fr div F.r;  / D C C r @r @F F curl F.r;  / D C @r r rf .r;  / D

O 1 @F r @  1 @Fr k: r @

12. x D a cosh u cos v, y D a sinh u sin v. a) u-curves: If A D a cosh u and B D a sinh u, then x2 y2 C D cos2 v C sin2 v D 1: A2 B2

2

630

and

10. Since .u; v; z/ constitute orthogonal curvilinear coordinates in R3 , with scale factors hu , hv and hz D 1, we have, for a function f .u; v/ independent of z,

ˇ ˇ ˇ ˇ ˇ D 2k: ˇ ˇ ˇ

  @ R2 D 0 @ ˇ ˇ ˇ R O R O R sin  O ˇˇ ˇ ˇ @ ˇ 1 @ @ ˇ ˇ curl F D 2 ˇ ˇ ˇ R sin  ˇ @R @ @ ˇ ˇ ˇ 0 2 0 R sin  ˇ O 2 O : D cot  R 1 R2 sin 

1 @r hu @u

The area element is dA D hu hv du dv.

F.R; ;  / D R O    1 @ R2 sin  D cot  div F D 2 R sin  @ ˇ ˇ ˇ R O R O R sin  O ˇˇ ˇ ˇ ˇ @ 1 @ @ ˇ ˇ curl F D 2 ˇ D 2 O : ˇ ˇ R sin  ˇ @R @ @ ˇ ˇ ˇ ˇ 0 2 R 0 F.R; ;  / D R O

Let r D x.u; v/ i C y.u; v/ j. The scale factors are ˇ ˇ ˇ ˇ ˇ @r ˇ ˇ @r ˇ ˇ ˇ hu D ˇ ˇ and hv D ˇˇ ˇˇ : @u @v The local basis consists of the vectors

O F.R; ;  / D sin  R    @ 1 2 sin  R2 sin2  D div F D 2 R sin  @R R ˇ ˇ ˇ R O R sin  O ˇ O R  ˇ ˇ ˇ ˇ 1 @ @ ˇ @ ˇ curl F D 2 ˇ ˇ ˇ R sin  ˇ @R @ @ ˇ ˇ ˇ sin  ˇ 0 0 cos  O : D R

div F D

8.

ADAMS and ESSEX: CALCULUS 9

Since A2 B 2 D a2 .cosh2 u sinh2 u/ D a2 , the u-curves are ellipses with foci at .˙a; 0/. b) v-curves: If A D a cos v and B D a sin v, then x2 A2

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y2 D cosh2 u B2

sinh2 u D 1:

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 16.7

Since A2 C B 2 D a2 .cos2 v C sin2 v/ D a2 , the v-curves are hyperbolas with foci at .˙a; 0/.

The coordinate curves are u-curves: the horizontal hyperbolas in which the v D v0 cylinders intersect the z D z0 planes. v-curves: the horizontal ellipses in which the u D u0 cylinders intersect the z D z0 planes. z-curves: sets of four vertical straight lines where the elliptic cylinders u D u0 and hyperbolic cylinders v D v0 intersect.

c) The u-curve u D u0 has parametric equations x D a cosh u0 cos v;

y D a sinh u0 sin v;

and therefore has slope at .u0 ; v0 / given by dy dy mu D D dx dv

,

ˇ dx ˇˇ ˇ dv ˇ

.u0 ;v0 /

D

a sinh u0 cos v0 : a cosh u0 sin v0 14.

The v-curve v D v0 has parametric equations x D a cosh u cos v0 ;

y D a sinh u sin v0 ;

and therefore has slope at .u0 ; v0 / given by dy dy mv D D dx du

,

ˇ dx ˇˇ ˇ du ˇ

.u0 ;v0 /

D

@f 1 @f O @f rO C C k @r  r @  @z r 2 f .r; ; z/ D div rf .r; ; z/        @f @ 1 @f @ @f 1 @ r C C r D r @r @r @ r @ @z @z 1 @f @2 f 1 @2 f @2 f C C : C 2 D @r 2 r @r r @ 2 @z 2 rf .r; ; z/ D

a cosh u0 sin v0 : a sinh u0 cos v0

Since the product of these slopes is mu mv D 1, the curves u D u0 and v D v0 intersect at right angles. d)

(PAGE 961)

15.

r D a cosh u cos v i C a sinh u sin v j @r D a sinh u cos v i C a cosh u sin v j @u @r D a cosh u sin v i C a sinh u cos v j: @v

The scale factors are

@f O 1 @f O 1 @f O RC C  @R R @ R sin  @   r 2 f .R; ;  / D div f .R; ;  / "     @ @f @ 1 @f 1 R2 sin  C R sin  D 2 R sin  @R @R @ R @  # R @f @ C @ R sin  @ rf .R; ;  / D

D

ˇ ˇ p ˇ @r ˇ hu D ˇˇ ˇˇ D a sinh2 u cos2 v C cosh2 u sin2 v @u ˇ ˇ p ˇ @r ˇ hv D ˇˇ ˇˇ D a sinh2 u cos2 v C cosh2 u sin2 v D hu : @v

@2 f 2 @f 1 @2 f C C @R2 R @R R2 @ 2 @2 f 1 cot  @f C : C 2 2 2 R @ R sin  @ 2

The area element is

16.

dA D hu hv du dv

 D a2 sinh2 u cos2 v C cosh2 u sin2 v du dv:

13.

x D a cosh u cos v y D a sinh u sin v z D z: Using the result of Exercise 12, we see that the coordinate surfaces are u D u0 : vertical elliptic cylinders with focal axes x D ˙a, y D 0. v D v0 : vertical hyperbolic cylinders with focal axes x D ˙a, y D 0. z D z0 : horizontal planes.

1 @f 1 @f 1 @f O uO C vO C w hu @u hv @v hw @w   r 2 f .u; v; w/ D div rf .u; v; w/ "     1 @ hu hw @f @ hv hw @f D C hu hv hw @u hu @u @v hv @v  # @ hu hv @f C @w hw @w     1 @hv 1 @hw 1 @hu @f 1 @2 f C C D 2 hu @u2 hv @u hw @u hu @u @u     1 @hu 1 @hw 1 @hv @f 1 @2 f C C C 2 hv @v 2 hu @v hw @v hv @v @v     1 @2 f 1 @hu 1 @hv 1 @hw @f C 2 C C : hw @w 2 hu @w hv @w hw @w @w rf .u; v; w/ D

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ADAMS and ESSEX: CALCULUS 9

1.

O specified in The semi-ellipsoid S with upward normal N the problem and the disk D given by x 2 C y 2  16, z D 0, with downwardpnormal k together bound the solid region R: 0  z  21 16 x 2 y 2 . By the Divergence Theorem: ZZ ZZ ZZZ O dS C FN F  . k/ dA D div F d V: S D R

S

R

div F d V D

.2xz C 2yz C 3/ d V ZZZ D0C0C3 d V D 3  (volume of R)

D2

3.

R

D 64 C

R

div F d V D D

Z

Z

0

4

0

dx dy

ZZD2 D2 2

Z

b

0

Œb C .e

ZZ

S

O dS C FN D

Therefore,

632

ZZ

S

ZZ

D1 ZZZ

R

6

P

2

y dA D

b

4.

1/ dx dy

ZZ

D2 2

F  . k/ dA b

C x

If F D

zi C xj C yk, then ˇ ˇ i j ˇ @ @ ˇ curl F D ˇ ˇ @x @y ˇ z x

k @ @z y

ˇ ˇ ˇ ˇ ˇDi ˇ ˇ

j C k:

O to a region in the plane 2xCyC2z D 7 The unit normal N is O D ˙ 2i C j C 2k : N 3 If C is the boundary of a disk D of radius a in that plane, then I ZZ O dS F  dr D curl F  N C D ZZ 2 1C2 dS D ˙a2 : D˙ 3 D

1/:

2

.3; 1/

Fig. R-16-3

.1 C e z / dz

div F d V D a b C a .e

O dS D a2 b. FN

6yA D 6;

.2; 0/

D1

F  k dA C

2

.6y C 4xye y / dA

P

ZZ F  . k/ dA D e 0 dA D a2 D2 D2 ZZ ZZ F  k dA D e b dA D a2 e b : D1

Œ4xye y

PZZ

r 3 dr D 128:

ZZ

By the Divergence Theorem

2

.1; 1/

cos2  d

ZZ

y

since P has area A D 2 and its centroid has y-coordinate y D 1=2. y

D a b C a2 .e b Also

2

x 2 dA

D 2

k

.3y 2 C 2xe y / dx C .2x 2 ye y / dy C ZZ

D

2. Let R be the region inside the cylinder S and between the planes z D 0 and z D b. The oriented boundary of R O 1 D k and consists of S and the disks D1 with normal N O 2 D k as shown in the figure. For D2 with normal N F D xi C cos.z 2 /j C e z k we have div F D 1 C e z and ZZZ

I

D

3 4 2 4 2 D 64: D 2 3

D 64 C

O2 D N

2a

Fig. R-16-2

R

The flux of F across S is ZZ ZZ O dS D 64 C FN F  k dA S ZZD

R

O N

x

ZZZ

b

D1

For F D x 2 zi C .y 2 z C 3y/j C x 2 k we have ZZZ

z

O1 D k N

Review Exercises 16 (page 961)

5. 1/:

If Sa is the sphere of radius a centred at the origin, then ZZ 1 O dS

FN div F.0; 0; 0/ D lim 4 a!0C a3 Sa 3 3 3 D lim .a3 C 2a4 / D : a!0C 4a3 4

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INSTRUCTOR’S SOLUTIONS MANUAL

REVIEW EXERCISES 16

O and boundary 6. If S is any surface with upward normal N 2 2 the curve C: x C y D 1, z D 2, then C is oriented counterclockwise as seen from above, and it has parametrization r D cos t i C sin t j C 2k .0  2  2/:

10. Let C be a simple, closed curve in the xy-plane bounding a region R. If F D .2y 3

Thus d r D . sin t i C cos t j/ dt , and if F D yi C x cos.1 x 2 y 2 /j C yzk, then the flux of curl F upward through S is ZZ I O dS D curl F  N F  dr S C Z 2 .sin2 t C cos2 t C 0/ dt D 2: D

I

F  dr C ZZ 

D

D D

F.r/ D r  r where r D xi C yj C zk and r D jrj. Since r 2 D x 2 C y 2 C z 2 , therefore @r=@x D x=r and @  .r x/ D r  @x

1x

2

r



Cr Dr

 2

2

.x C r /:

F is solenoidal on any set in R3 that excludes the origin if an only if  D 3. In this case F is not defined at r D 0. There is no value of  for which F is solenoidal on all of R3 . 8. If curl F D F on R3 , where  ¤ 0 is a constant, then div F D

1 div curl F D 0 

by Theorem 3(g) of Section 7.2. By part (i) of the same theorem, r 2 F D r.div F/ curl curl F D0

curl F D

2 F:

Thus r 2 F C 2 F D 0. 9. Apply the variant of the Divergence Theorem given in Theorem 7(b) of Section 7.3, namely ZZZ ZZ O dS; grad  d V D  N P S

ZZR

ZZR

11.

x 3 C x 2 y/

.1

3x 2 C 2xy

.4

3x 2

 3y C xy 2 / dA

@ .2y 3 @y

6y 2 C 3

2xy/ dA

6y 2 / dx dy:

R

F D .4x C 2x 3 z/i

y.x 2 C z 2 /j

.3x 2 z 2 C 4y 2 z/k;

then by the Divergence Theorem, the flux of F through S is ZZ ZZZ ZZZ O dS D

FN div F d V D .4 x 2 4y 2 z 2 / d V: S R R The last integral has a maximum value when the region R is bounded by the ellipsoid x 2 C 4y 2 C z 2 D 4 with outward normal; this is the largest region in R3 where the integrand is nonnegative. 12. Let C be a simple, closed curve on the plane x C y C z D 1, oriented counterclockwise as seen from above, and bounding a plane region Spon x C y C z D 1. O D .i C j C k/= 3. If Then S has normal N 2 F D xy i C .3z xy 2 /j C .4y x 2 y/k, then ˇ ˇ i ˇ ˇ @ curl F D ˇˇ ˇ @x2 ˇ xy D .1

iD1

ZZ n n n ZZ X X X Ni Ni O dS D dS D Ai D Ni : 0D N Ai Fi Ai S iD1 iD1 iD1

@ .x @x

Let S be a closed, oriented surface in R3 bounding a reO If gion R, and having outward normal field N.

to the scalar field  D 1 over the polyhedron P . Here n [ S D Fi is the surface of P , oriented with outward

O i on the face Fi . If Ni D Ai N O i , where Ai normal field N is the area of Fi , then, since grad  D 0, we have

x 3 C x 2 y/j;

The last integral has a maximum value when the region R is bounded by the ellipse 3x 2 C 6y 2 D 4, oriented counterclockwise; this is the largest region in the xy-plane where the integrand is nonnegative.

2

Similar expressions hold for .@=@y/.r  y/ and .@=@z/.r  z/, so div F.r/ D r  2 .r 2 C 3r 2 / D . C 3/r  :

3y C xy 2 /i C .x

then by Green’s Theorem, the circulation of F around C is

0

7.

(PAGE 961)

j @ @y 3z xy 2

x 2 /i C 2xyj

ˇ ˇ k ˇ @ ˇ ˇ ˇ @z ˇ 2 ˇ 4y x y

.y 2 C 2xy/k:

By Stokes’s Theorem we have I

C

F  dr D

ZZ

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S

O dS D curl F  N

ZZ

S

1

x2 p

y2 3

dS:

633

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REVIEW EXERCISES 16 (PAGE 961)

ADAMS and ESSEX: CALCULUS 9

The last integral will be maximum if the projection of S onto the xy-plane is the disk x 2 C y 2  1. This maximum value is ZZ D

x2 p

1

x 2 Cy 2 1 Z 2 Z 1

d

0

y2 p 3

3 dx dy

2

r /r dr D 2

.1

0

b) If S is the intersection of a smooth surface with the general half-cone K, and is oriented with normal field O pointing away from the vertex P of K, and if Sa N is the intersection with K of a sphere of radius a centred at P , with a chosen so that S and Sa do not intersect in K, then S, Sa , and the walls of K bound a solid region R that does not contain the origin. If F D r=jrj3 , then div F D 0 in R (see Example 3 in O D 0 on the walls of K. It Section 7.1), and F  N follows from the Divergence Theorem applied to F over R that ZZ ZZ r O dS D dS FN F jrj S Sa ZZ a2 1 D 4 dS D 2 .area of Sa / a a Sa



1 2

1 4



D

 : 2

Challenging Problems 16 (page 962) 1.

By Theorem 1 of Section 7.1, we have ZZ 3 O

v.r/  N.r/ dS: !0C 4 3 S

div v.r1 / D lim

D area of S1 :

Here S is the sphere of radius  centred at the point (with position vector) r1 and having outward normal field O N.r/. If r is (the position vector of) any point on S , then O r D r1 C  N.r/, and ZZ O

v.r/  N.r/ dS SZZ h  i O dS D v.r1 / C v.r/ v.r1 /  N.r/ S ZZ O D v.r1 /  N.r/ dS ZZ  S  r r 1 C v.r/ v.r1 /  dS:  S

ZZ O But N.r/ dS D 0 by Theorem 7(b) of Section 7.3 S with  D 1. Also, since v satisfies v.r1 / D C jr2

v.r2 / we have

r1 j2 ;

ZZ   r r 1 dS

v.r/ v.r1 /   S ZZ C 2 D dS D 4 C  3 : S 

Thus div v.r1 / D lim

!0C

3 .0 C 4 C  3 / D 3C: 4 3

The divergence of the large-scale velocity field of matter in the universe is three times Hubble’s constant C . 2.

a) The steradian measure of a half-cone of semi-vertical angle ˛ is Z

0

634

2

d

Z

˛ 0

sin  d D 2.1

cos ˛/:

The area of S1 (the part of the sphere of radius 1 in K) is the measure (in steradians) of the solid angle subtended by K at its vertex P . Hence this measure is given by ZZ r O dS: N jrj S 3 3.

a) Verification of the identity     @ @r @ @r G G @t @s @s @t   @F @r @r @r D  C .r  F/   : @t @s @t @s can be carried out using the following MapleV commands: > > > > > > > > > > > > > > > > > > > >

with(linalg): F:=(x,y,z,t)-> [F1(x,y,z,t), F2(x,y,z,t),F3(x,y,z,t)]; r:=(s,t)->[x(s,t),y(s,t),z(s,t)]; G:=(s,t)->F(x(s,t),y(s,t),z(s,t),t); g:=(s,t)-> dotprod(G(s,t), map(diff,r(s,t),s)); h:=(s,t)-> dotprod(G(s,t), map(diff,r(s,t),t)); LH1:=diff(g(s,t),t); LH2:=diff(h(s,t),s); LHS:=simplify(LH1-LH2); RH1:=dotprod(subs(x=x(s,t),y=y(s,t), z=z(s,t),diff(F(x,y,z,t),t)), diff(r(s,t),s)); RH2:=dotprod(crossprod(subs(x=x(s,t), y=y(s,t),z=z(s,t), curl(F(x,y,z,t),[x,y,z])), diff(r(s,t),t)),diff(r(s,t),s)); RHS:=RH1+RH2; LHS-RHS; simplify(%);

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INSTRUCTOR’S SOLUTIONS MANUAL

CHALLENGING PROBLEMS 16

We omit the output here; some of the commands produce screenfulls of output. The output of the final command is 0, indicating that the identity is valid. b) As suggested by the hint, d dt

Z

Ct b

F  dr D

Z

b a

@ @t 

  @r G ds @s

 @r @ D G @s @t a      @r @ @r @ C G G ds @t @s @s @t ˇsDb @r ˇˇ DG ˇ @t ˇ sDa   Z b @r @r @F C .r  F/   ds C @t @t @s a     D F r.b; t /; t  vC .b; t / F r.a; t /; t  vC .a; t / Z Z   @F C  dr C .r  F/  vC  d r: C t @t Ct

4.

Z



> > > > > > > > > >

LH3:=diff(dotprod(G(u,v,t), ruxt(u,v,t)),v); LHS:=simplify(LH1-LH2-LH3); RH1:=dotprod(subs(x=x(u,v,t), y=y(u,v,t),z=z(u,v,t), diff(F(x,y,z,t),t)),ruxv(u,v,t)); RH2:=(divf(u,v,t))* (dotprod(rt(u,v,t),ruxv(u,v,t))); RHS:=simplify(RH1+RH2); simplify(LHS-RHS);

Again the final output is 0, indicating that the identity is valid. b) If C t is the oriented boundary of S t and L t is the corresponding counterclockwise boundary of the parameter region R in the uv-plane, then



 @r F  dr C t  @t    I @r @r @r D G  du C dv @t @u @v L     I t @r @r @r @r  CG  dt D G @u @t @t @v Lt "    ZZ @ @r @r D  G @t @v R @u   # @r @r @  du dv; C G @v @u @t



    @r @r @r @r @   G G @u @v @u @t @v    @ @r @r  G @v @u @t     @r @r @r @r @r @F    C .r  F/  : D @t @u @v @t @u @v

can be carried out using the following MapleV commands: > > > > > > > > > > > > > > > > > > > >

with(linalg): F:=(x,y,z,t)->[F1(x,y,z,t), F2(x,y,z,t),F3(x,y,z,t)]; r:=(u,v,t)->[x(u,v,t),y(u,v,t), z(u,v,t)]; ru:=(u,v,t)->diff(r(u,v,t),u); rv:=(u,v,t)->diff(r(u,v,t),v); rt:=(u,v,t)->diff(r(u,v,t),t); G:=(u,v,t)->F(x(u,v,t), y(u,v,t),z(u,v,t),t); ruxv:=(u,v,t)->crossprod(ru(u,v,t), rv(u,v,t)); rtxv:=(u,v,t)->crossprod(rt(u,v,t), rv(u,v,t)); ruxt:=(u,v,t)->crossprod(ru(u,v,t), rt(u,v,t)); LH1:=diff(dotprod(G(u,v,t), ruxv(u,v,t)),t); LH2:=diff(dotprod(G(u,v,t), rtxv(u,v,t)),u);



I

a) Verification of the identity @ @t

(PAGE 962)

by Green’s Theorem. c) Using the results of (a) and (b), we calculate    ZZ @ @r @r O dS D FN  G du dv @u @v S R @t   ZZ t @r @r @F   du dv D @u @v R @t   ZZ @r @r @r C  du dv .div F/  @t @u @v R "    ZZ @ @r @r C  G @t @v R @u   # @r @r @  du dv G C @v @u @t ZZ ZZ @F O O dS  N dS C .div F/vS  N D St StZZ@t

d dt

ZZ

C C t .F  vC /  d r:

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(PAGE 962)

5. We have "ZZZ # ZZZ 1 f .r; t C t / d V f .r; t / d V t D t Ct Dt ZZZ f .r; t C t / f .r; t / dV D t Dt ZZZ 1 f .r; t C t / d V C t D D ZZZt Ct t 1 f .r; t C t / d V t D t D t Ct D I1 C I2 I3 : ZZZ @f Evidently I1 ! d V as t ! 0. D t @t I2 and I3 are integrals over the parts of D t where the surface ÷ t is moving outwards and inwards, respectively, O is, respectively, positive and negative. that is, where vS  N O dS T , we have Since d V D jvS  Nj

636

ADAMS and ESSEX: CALCULUS 9

I2

I3 D D

ZZ

ZZS t

St

C

O dS f .r; t C t /vS  N O dS f .r; t /vS  N

ZZ  f .r; t C t / St

 O dS: f .r; t / vS  N

The latter integral approaches 0 as t ! 0 because ˇZZ  ˇ  ˇ ˇ ˇ O dS ˇ f .r; t C t / f .r; t / v  N S ˇ ˇ St ˇ ˇ ˇ @f ˇ  max jvS j ˇˇ ˇˇ (area of S t )t: @t

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 17.2

CHAPTER 17. DIFFERENTIAL FORMS AND EXTERIOR CALCULUS Section 17.1 k-Forms 1.

(page 971)

There are six terms in the expanded wedge product of  and ; each is a 4-form. Five of them have at least one of the basic forms dxi repeated twice, and so are zero. The only remaining nonzero form is ^

6.

7.

D a2 b1 dx3 ^ dx4 ^ dx1 ^ dx2 D a2 b1 dx1 ^ dx2 ^ dx3 ^ dx4

because f3; 4; 1; 2g is an even permutation of f1; 2; 3; 4g. 2. Only the first term of contributes to the product; the other two give zero when wedged with . Thus ^

D dx2 ^ dx3 ^ dx4 ^ dx1 D dx1 ^ dx2 ^ dx3 ^ dx4

because f2; 3; 4; 1g is an odd permutation of f1; 2; 3; 4g.

8.

3. When we calculate  ^ the five terms of  combine with the two terms of to give 10 terms. Eight of them have repeated differential factors and so are zero. The remaining two are

Since f5; 1; 2; 3; 4g is an even permutation of f1; 2; 3; 4; 5g, these two terms combine to give ^

D 7 dx1 ^ dx2 ^ dx3 ^ dx4 ^ dx5 :

4. Half of the 16 terms resulting from the wedge product of these two 4-term forms are zero because of repeated differentials. The remaining ones are D a1 b1 dx1 ^ dx2 ^ dx3 C a1 b2 dx1 ^ dx3 ^ dx4 C a2 b2 dx2 ^ dx3 ^ dx4 C a2 b3 dx2 ^ dx4 ^ dx1 C a3 b3 dx3 ^ dx4 ^ dx1 C a3 b4 dx3 ^ dx1 ^ dx2 C a4 b1 dx4 ^ dx2 ^ dx3 C a4 b4 dx4 ^ dx1 ^ dx2 D .a1 b1 C a3 b4 /dx1 ^ dx2 ^ dx3 C .a1 b2 C a3 b3 /dx1 ^ dx3 ^ dx4 C .a4 b1 C a2 b2 /dx2 ^ dx3 ^ dx4 C .a2 b3 C a4 b4 /dx1 ^ dx2 ^ dx4 :

256:

Section 17.2 Differential Forms and the Exterior Derivative (page 977) 1.

2.

ˆ D x 2 dx C y 2 dz dˆ D 2x dx ^ dx C 2y dy ^ dz D 2y dy ^ dz f D x e 2y si n.3z/

df D e 2y sin.3z/ dx C 2x e 2y si n.3z/ dy C 3x e 2y cos.3z/ dz 3.

‰ D x1 dx2 ^ dx3 C x2 dx1 ^ dx4 C .x3 C x4 / dx1 ^ dx2 d ‰ D dx1 ^ dx2 ^ dx3 C dx2 ^ dx1 ^ dx4 C dx3 ^ dx1 ^ dx2 C dx4 ^ dx1 ^ dx2 D 2 dx1 ^ dx2 ^ dx3 :

4.

‚ D x1 x2 x3 dx1 ^ dx3 ^ dx5 C x3 x4 x5 dx2 ^ dx4 ^ dx5 d‚ D dx2 ^ dx1 ^ dx3 ^ dx5 C x4 x5 dx3 ^ dx2 ^ dx4 ^ dx5 D x1 x3 dx1 ^ dx2 ^ dx3 ^ dx5 x4 x5 dx2 ^ dx3 ^ dx4 ^ dx5 :

5.

ˆ D e 2y sin.3z/ dx C 2x e 2y si n.3z/ dy C 3x e 2y cos.3z/ dz

^

5.  D .12/.13/.14/    .1k/, which involves k 1 reversals. Thus  is odd if k is even and even if k is odd.

 is a sum of wedge products of k differentials, and is a sum of wedge products of ` differentials. To transform  ^ to ^ , in each term of the product each of the ` differentials from must pass leftward through all k differentials from . This requires k reversals for each of the ` differentials from , and so a total of k` reversals in total (for each term of the product). Thus  ^ D . 1/kl ^  ˇ ˇ ˇ1 1ˇ ˇD 1 dx1 ^ dx2 .u; v/ D ˇˇ 1 0ˇ ˇ ˇ ˇ1 1 1ˇ ˇ ˇ ˇ ˇ ˇ1 1ˇ ˇD1 dx1 ^ dx2 ^ dx3 .u; v; w/ D ˇˇ 1 0 0 ˇˇ D ˇˇ 1 0ˇ ˇ0 1 0ˇ ˇ ˇ ˇ ˇ0 1 0ˇ ˇ ˇ ˇ0 1ˇ ˇ ˇD1 dx3 ^ dx4 ^ dx1 .u; v; w/ D ˇˇ 0 0 1 ˇˇ D ˇˇ 1 1ˇ ˇ1 1 1ˇ ˇ ˇ ˇ0 1 0ˇ ˇ ˇ dx3 ^ dx2 ^ dx4 .u; v; w/ D ˇˇ 1 0 0 ˇˇ D 1 ˇ0 0 1ˇ ˇ ˇ ˇ1 2 3 4 ˇˇ ˇ ˇ2 3 4 0 ˇˇ .v1 : : : ; v4 / D ˇˇ 3 4 0 0 ˇˇ ˇ ˇ4 0 0 0 ˇ ˇ ˇ ˇ ˇ ˇ 2 3 4 ˇˇ ˇ 3 ˇ 4 ˇˇ 4 0 ˇˇ D 16 ˇˇ D . 4/ ˇˇ 3 4 0 ˇ ˇ 4 0 0ˇ D .16/. 16/ D

5 dx5 ^ dx1 ^ dx2 ^ dx3 ^ dx4 and 2 dx1 ^ dx2 ^ dx3 ^ dx4 ^ dx5 :

(PAGE 977)

dˆ D 2e 2y sin.3z/ dy ^ dx C 3e 2y cos.3z/ dz ^ dx

C 2e 2y sin.3z/ dx ^ dy C 6xe 2y cos.3z/ dz ^ dy

C 3e 2y cos.3z/ dx ^ dz C 6xe 2y cos.3z/ dy ^ dz D 0 the zero differential 2-form:

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SECTION 17.2 (PAGE 977)

ADAMS and ESSEX: CALCULUS 9

Not surprising, since ˆ D df , where f is the differential 0-form in Exercise 2, and so dˆ D d 2 f D 0. 6.

14.

ˆ D x1 x3 dx1 ^ dx2 ^ dx3 ^ dx5 C x4 x5 dx2 ^ dx3 ^ dx4 ^ dx5 dˆ D 0 each term has a repeated differential. Not surprising, since ˆ D d‚, where ‚ is the differential 3-form in Exercise 4, and so dˆ D d 2 ‚ D 0, the zero differential 4-form.

7.

f .x/ D

d.aˆ C b‰/ D adˆ C bd ‰ 8. Each term in ˆ ^ ‚ is of the form

Now  n    X @bj1 j` @ai1 ik bj1 j` C ai1 ik dxm d ai1 ik bj1 j` D @xm @xm mD1

If we adjoin dxi1 ^    ^ dxik ^ dxj1 ^    ^ dj` , the result will the corresponding term of .dˆ/ ^ ‚ C . 1/k ˆ ^ .d‚/. The . 1/k accounts for the fact that in the second term of ./ the dxm must be shifted to the right of all the dxi s (k of them) to a position just before the first dxj to give d‚. 9.

j D1

11.

1

ˆ1 ^    ^ ˆj

1

Thus df D

15.

^ .dˆj / ^ ˆj C1 ^    ˆm :

curl grad f D 0

12. div curl .F1 i C F2 j C F3 k/ D 0 13. If ˆ D

k X

16.

(a) (c)

ai .x/ dxi , then

dˆ D

(e)

iD1

D ˆ.

@S @V @T @ D (b) D @T @N @S @ @S @V @S @P D (d) D @P @T @V @T @T @V D @P @S

(a) We have

k X k X @ai .x/ dxj ^ dxi D @xj iD1 j D1 X  @ai .x/ @aj .x/  D dxj ^ dxi : @xj @xi

 @Ey @Ez @Ex C C dx ^ dy ^ dz @x @y @z   1 @Ex @Bz @By C C dt ^ dy ^ dz c 2 @t @y @z   @Bx @Bz 1 @Ey C dt ^ dz ^ dx C c 2 @t @z @x   1 @Ez @By @Bx C C dt ^ dx ^ dy c 2 @t @x @y

1 dG D 2 c

1j 0 and X > 0, then   e kx  0 .x/ ke kx .x/ d .x/  0: D kx dx e e 2kx

Thus .x/=e kx is increasing on Œ0; X. Since its value at x D 0 is .0/ D A  0, therefore .x/=e kx  A on Œ0; X, and .x/  Ae kx there.

12. We start with x0 D 0, y0 D 0, and calculate xnC1 D xn C h

a) Suppose u0 D u2 , y 0 D x C y 2 , and v 0 D 1 C v 2 on Œ0; X, where u.0/ D y.0/ D v.0/ D 1, and X > 0 is such that v.x/ is defined on Œ0; X. (In part (b) below, we will show that X < 1, and we assume this fact now.) Since all three functions are increasing on Œ0; X, we have u.x/  1, y.x/  1, and v.x/  1 on Œ0; X. If .x/ D y.x/

a) For h D 0:2 we get x5 D 1, y5 D 0:904524. b) For h D 0:1 we get x10 D 1, y10 D 0:904524. c) For h D 0:05 we get x20 D 1, y20 D 0:904524.

a

u.x/, then .0/ D 0 and

 0 .x/ D x C y 2 u2  y 2 u2  .y C u/.y u/  2

on Œ0; X. By Exercise 16, .x/  0 on Œ0; X, and so u.x/  y.x/ there.

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SECTION 18.3 (PAGE 1016)

ADAMS and ESSEX: CALCULUS 9

Similarly, since X < 1, if .x/ D v.x/ .0/ D 0 and  0 .x/ D 1 C v 2 x y 2  v 2  .v C y/.v y/  2

Section 18.4 Differential Equations of Second Order (page 1020)

y.x/, then y2

1.

on Œ0; X, so y.x/  v.x/ there.

y 0 D e x .v 0 C v/; y 00 D e x .v 00 C 2v 0 C v/ 00 0 x 00 y 3y C 2y D e .v C 2v 0 C v 3v 0 3v C 2v/ D e x .v 00 v 0 /:

b) The IVP u0 D u2 , u.0/ D 1 has solution 1 u.x/ D , obtained by separation of variables. 1 x This solution is valid for x < 1. The IVP v 0 D 1 C v2 , v.0/ D 1 has solution v.x/ D tan x C 4 , also obtained by separation of variables. It is valid only for 3=4 < x < =4. Observe that =4 < 1, proving the assertion made about v in part (a). By the result of part (a), the solution of the IVP y 0 D x C y 2 , y.0/ D 1, increases on an interval Œ0; X and ! 1 as x ! X from the left, where X is some number in the interval Œ=4; 1.

y satisfies y 00 3y 0 C 2y D 0 provided w D v 0 satisfies w 0 w D 0. This equation has solution v 0 D w D C1 e x , so v D C1 e x C C2 . Thus the given DE has solution y D e x v D C1 e 2x C C2 e x . 2.

yn D 12:37139 yn D 31:777317 yn D 4071:117315:

3.

n D 94

xn xn xn xn xn

D 0:86 D 0:88 D 0:90 D 0:92 D 0:94

yn yn yn yn yn

y

2x

xn xn xn xn xn xn xn xn

D 0:86 D 0:87 D 0:88 D 0:89 D 0:90 D 0:91 D 0:92 D 0:93

xn D 0:94

yn yn yn yn yn yn yn yn

D 14:150706 D 16:493286 D 19:761277 D 24:638758 D 32:703853 D 48:591332 D 94:087476 D 636:786465

yn D 2:8399  1011 :

2x

.v 00

00

4v 0 C 4v/

0

6y D e .v 4v C 4v x 00 D e .v 5v 0 /:

2y1 D 0 C 2x

v 0 C 2v

6v/

2x D 0;

so y1 is a solution of the DE x 2 y 00 C 2xy 0 y D xv.x/. Then

D 14:149657 D 19:756061 D 32:651029 D 90:770048 D 34266:466629:

The values are still in reasonable agreement at x D 0:9, but they start to diverge quickly thereafter. This suggests that X is slightly greater than 0.9.

650

y 00 D e

2v/; 0

x 2 y100 C 2xy10

y 0 D xv 0 C v;

2 00

x y C 2xy

0

2y D 0. Let

y 00 D xv 00 C 2v 0

3 00

2y D x v C 2x 2 v 0 C 2x 2 v 0 C 2xv 2

00

2xv

0

D x .xv C 4v /:

y satisfies x 2 y 00 C 2xy 0 2y D 0 provided w D v 0 satisfies xw 0 C 4w D 0. This equation has solution v 0 D w D 3C1 x 4 (obtained by separation of variables), so v D C1 x 3 C C2 . Thus the given DE has solution y D xv D C1 x 2 C C2 x.

For h D 0:01 n D 86 n D 87 n D 88 n D 89 n D 90 n D 91 n D 92 n D 93

y

.v 0

00

.4 C 2 6/ D 0, 6y D 0. Let

If y1 D x on .0; 1/, then

For h D 0:02 n D 43 n D 44 n D 45 n D 46 n D 47

2x

2x

y satisfies y 00 y 0 6y D 0 provided w D v 0 satisfies w 0 5w D 0. This equation has solution v 0 D w D .C1 =5/e 5x , so v D C1 e 5x C C2 . Thus the given DE has solution y D e 2x v D C1 e 3x C C2 e 2x .

For h D 0:05 xn D 0:85 xn D 0:90 xn D 0:95

If y1 D e 2x , then y100 y10 6y1 D e so y1 is a solution of the DE y 00 y 0 y D e 2x v. Then y0 D e

c) Here are some approximations to y.x/ for values of x near 0.9 obtained by the Runge-Kutta method with x0 D 0 and y0 D 1: n D 17 n D 18 n D 19

If y1 D e x , then y100 3y10 C2y1 D e x .1 3C2/ D 0, so y1 is a solution of the DE y 00 3y 0 C 2y D 0. Let y D e x v. Then

4.

If y1 D x 2 on .0; 1/, then x 2 y100

3xy10 C 4y1 D 2x 2

6x 2 C 4x 2 D 0;

so y1 is a solution of the DE x 2 y 00 y D x 2 v.x/. Then y 0 D x 2 v 0 C 2xv; 2 00

x y

y 00 D x 2 v 00 C 4xv 0 C 2v

3xy C 4y D x v C 4x 3 v 0 C 2x 2 v

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0

3xy 0 C 4y D 0. Let

4 00

3x 3 v 0

3

00

0

6x 2 v C 4x 2 v

D x .xv C v /:

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 18.4 (PAGE 1020)

y satisfies x 2 y 00 3xy 0 C 4y D 0 provided w D v 0 satisfies xw 0 C w D 0. This equation has solution v 0 D w D C1 =x (obtained by separation of variables), so v D C1 ln x C C2 . Thus the given DE has solution y D x 2 v D C1 x 2 ln x C C2 x 2 .

If we substitute these expressions into the equation ./, many terms cancel out and we are left with the equation .cos x/v 00

Substituting u D v 0 , we rewrite this equation in the form

5. If y D x, then y 0 D 1 and y 00 D 0. Thus x 2 y 00

du D 2.sin x/u .cos x/ dx Z Z du D 2 tan x dx ) ln juj D 2 ln j sec xj C C0 : u

x.x C 2/y 0 C .x C 2/y D 0:

Now let y D xv.x/. Then y 0 D v C xv 0 ;

2.sin x/v 0 D 0:

y 00 D 2v 0 C xv 00 :

Thus v 0 D u D C1 sec2 x, from which we obtain v D C1 tan x C C2 :

Substituting these expressions into the differential equation we get

Thus the general solution of the Bessel equation ./ is 2x 2 v 0 C x 3 v 00

x2v

2xv

x3 v 0

yDx

2x 2 v 0 C x 2 v C 2xv D 0

x 3 v 00

x 3 v 0 D 0;

or v 00

7.

3 x 4

y 00 D

3=2

d dx

cos x

1=2

x

sin x 8.

5=2

cos x C x

3=2

sin x

1=2

x

cos x:



1=2

cos x:

y1 y2



D



0 a0

a1 y2 C f . Thus

1 a1



y1 y2



C



0 f



:

If y satisfies y .n/ C an

Thus

1 .x/y

.n 1/

C    C a1 .x/y 0 C a0 .x/y D f .x/;

then let

 x 2 y 00 C xy 0 C x 2

 1 y 4

3 1=2 x cos x C x 1=2 sin x x 3=2 cos x 4 1 1=2 x cos x x 1=2 sin x C x 3=2 cos x 2 D 0:

Therefore y D x equation

1=2

1 x 2

3 y 00 D x 4 x

3=2

1=2

1 x 4

1=2

cos x

x

5=2

.cos x/v C x

1=2

.cos x/v

2x

1=2 3=2



1 y D 0: 4

.sin x/v C x

.sin x/v

1=2

x

:::

yn D y .n

1/

:

y10 D y2 ; y20 D y3 ; : : : yn0 2 D yn 1 ; and yn0 D a0 y1 a1 y2 a2 y3    an 1 yn C f; and we have

./

.cos x/v.x/. Then

.cos x/v

y3 D y 00 ;

Therefore

cos x is a solution of the Bessel

 x 2 y 00 C xy 0 C x 2

Now let y D x

y2 D y 0 ;

y1 D y;

D

y0 D

sin x C C2 x

If y1 D y and y2 D y 0 where y satisfies

then y10 D y2 and y20 D a0 y1

cos x, then 1 x 2

y0 D

1=2

y 00 C a1 .x/y 0 C a0 .x/y D f .x/;

y D C1 x C C2 xe x : 1=2

.cos x/v D C1 x

v 0 D 0;

which has solution v D C1 C C2 e x . Hence the general solution of the given differential equation is

6. If y D x

1=2

1=2

3=2

.sin x/v 0 C x

.cos x/v 0

.cos x/v 0

1=2

.cos x/v 00 :

1 0 y1 y C B d B B 2C B B :: C D B dx @ : A B @ yn 0

00 B0 B : : CB B : @0 f

1

0 0 :: :

1 0 :: :

0 1 :: :

::: :::

0 a0

0 a1

0 a2

::: :::

10

1 y1 CBy C CB 2 C CB : C C@ : A : 1 A yn an 0 0 :: :

C C C: C A

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SECTION 18.4 (PAGE 1020)

ADAMS and ESSEX: CALCULUS 9

9. If y D C1 e x v, then

3.

y0 D C1 e x v D C1 e x Av D Ay

.r 2 C 1/2 D 0 ) r D i; i; i; i General solution: y D C1 cos t C C2 sin t C C3 t cos t C C4 t sin t .

provided  and v satisfy Av D v. ˇ ˇ ˇ2  1 ˇˇ D 6 5 C 2 2 10. ˇˇ 2 3 ˇ D 2 D .

4.

5 C 4 1/. 4/ D 0

AD



2 2

1 3

5.



v1 v2





D

Thus we may take v D v1 D If  D 4 and Av D 4v, then AD



2 1 2 3



v1 v2



D4

v1 v2





 1 . 1



v1 v2



, v1 C v2 D 0:

6.

, 2v1

Ce

7.

D C1 e x

y1 D

y2 D



1 1



C C2 e 4x

C1 e x C C2 e 4x

2. y .4/ 2y 00 C y D 0 Auxiliary: r 4 2r 2 C 1 D 0

.r 2 1/2 D 0 ) r D 1; 1; 1; 1 General solution: y D C1 e t C C2 t e t C C3 e t C C4 t e t .

652

.C7 C C8 t /:

2r C 1 D 0

x 2 y 00

xy 0

Thus; y D Ax

9.

C1 e x C 2C2 e 4x :

y 000 4y 00 C 3y 0 D 0 Auxiliary: r 3 4r 2 C 3r D 0 r.r 1/.r 3/ D 0 ) r D 0; 1; 3 General solution: y D C1 C C2 e t C C3 e 3t .

2t

3y D 0

r.r 1/ r 3 D 0 ) r 2 2r 3 D 0 ).r 3/.r C 1/ D 0 ) r1 D 1 and r2 D 3

or

Section 18.5 Linear Differential Equations with Constant Coefficients (page 1025) 1.

4/2 D 0

.r 1/2 D 0; r D 1; 1: Thus y D Ax C Bx ln x: 8.

  1 ; 2

2

x 2 y 00 xy 0 C y D 0 aux: r.r 1/ r C 1 D 0 r2

that is 

2/2 .r 2

r

y D e 2t .C1 C C2 t C C3 t 2 C C4 t 3 / C e t .C5 C C6 t /

v2 D 0:

y D C1 e x v1 C C2 e 4x v2 ;

y1 y2

Aux. eqn: .r 2

.r C 1/ .r 2/ .r 2/2 .r C 2/2 D 0 r D 2; 2; 2; 2; 1; 1; 2; 2: The general solution is

By the result of Exercise 9, y D e x v1 and y D e 4x v2 are solutions of the homogeneous linear system y0 D Ay. Therefore the general solution of the system is



If y D e 2t , then y 000 2y 0 4y D e 2t .8 4 4/ D 0. The auxiliary equation for the DE is r 3 2r 4 D 0, for which we already know that r D 2 is a root. Dividing the left side by r 2, we obtain the quotient r 2 C 2r C 2. Hence the other two auxiliary roots are 1 ˙ i . General solution: y D C1 e 2t C C2 e t cos t C C3 e t sin t . 2

  1 . 2

Thus we may take v D v2 D

y .4/ C 4y .3/ C 6y 00 C 4y 0 C y D 0 Auxiliary: r 4 C 4r 3 C 6r 2 C 4r C 1 D 0

.r C 1/4 D 0 ) r D 1; 1; 1; 1 General solution: y D e t .C1 C C2 t C C3 t 2 C C4 t 3 /.

if  D 1 or  D 4.   2 1 Let A D . 2 3 If  D 1 and Av D v, then

y .4/ C 2y 00 C y D 0 Auxiliary: r 4 C 2r 2 C 1 D 0

1

C Bx 3 :

x 2 y 00 C xy 0 y D 0 aux: r.r 1/ C r 1 D 0 B y D Ax C : x

) r D ˙1

10. Consider x 2 y 00 xy 0 C 5y D 0. Since a D 1, b D 1, and c D 5, therefore .b a/2 < 4ac. Then k D .a b/=2a D 1 and ! 2 D 4. Thus, the general solution is y D Ax cos.2 ln x/ C Bx sin.2 ln x/. 11.

x 2 y 00 C xy 0 D 0 aux: r.r 1/ C r D 0 Thus y D A C B ln x:

) r D 0; 0:

12. Given that x 2 y 00 C xy 0 C y D 0. Since a D 1, b D 1, c D 1 therefore .b a/2 < 4ac. Then k D .a b/=2a D 0 and ! 2 D 1. Thus, the general solution is y D A cos.ln x/ C B sin.ln x/.

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lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 18.6 (PAGE 1031)

13. x 3 y 000 C xy 0 y D 0. Trying y D x r leads to the auxiliary equation r.r r3 .r

2/ C r

1/.r

3r 2 C 3r

Since t D ln x, the given Euler equation has solution y D C1 x cos.ln x/ C C2 x sin.ln x/:

1D0

1D0

Section 18.6 Nonhomogeneous Linear Equations (page 1031)

1/3 D 0 ) r D 1; 1; 1:

Thus y D x is a solution. To find the general solution, try y D xv.x/. Then y 0 D xv 0 C v; Now x 3 y 000 C xy 0

y 00 D xv 00 C 2v 0 ;

1.

y 000 D xv 000 C 3v 00 :

y D x 4 v 000 C 3x 3 v 00 C x 2 v 0 C xv

yh D C1 e

xv

D x 2 .x 2 v 000 C 3xv 00 C v 0 /; and y is a solution of the given equation if v 0 D w is a solution of x 2 w 00 C 3xw 0 C w D 0. This equation has auxiliary equation r.r 1/ C 3r C 1 D 0, that is .r C 1/2 D 0, so its solutions are

2.

The general solution of the given equation is, therefore, y D C1 x C C2 x ln x C C3 x.ln x/2 :

2x

C C2 e x :

2.Ax C B/ D A

2x C 1 C C1 e 4

yD 3.

2B

2Ax:

dz d 2z C cz C .b a/ dt 2 dt d 2y dy dy Dax 2 C ax C .b a/x C cy D 0: dx 2 dx dx

e

z D C1 e t cos t C C2 e t sin t:

2r C 2 D 0,

De

yD 4.

The auxiliary equation for this equation is r 2 which has roots r D 1 ˙ i . Thus

x

We require A D equation is

By the previous exercise, z.t / D y.e t / D y.x/ must satisfy the constant coefficient equation dz C 2z D 0: dt

2x

C C2 e x :

y 00 C y 0 2y D e x . The complementary function is yh D C1 e 2x C C2 e x , as shown in Exercise 1. For a particular solution try y D Ae x . Then y 0 D Ae x and y 00 D Ae x , so y satisfies the given equation if

a

2

1 C C1 e 2

We require A 2B D 0 and 2A D 1, so A D 1=2 and B D 1=4. The general solution of the given equation is

Accordingly, z D z.t / satisfies

d 2z dt 2

C C2 e x :

y 00 C y 0 2y D x. The complementary function is yh D C1 e 2x C C2 e x , as shown in Exercise 1. For a particular solution try y D Ax C B. Then y 0 D A and y 00 D 0, so y satisfies the given equation if xDA

dx D e t D x, we have Since dt dy dx dy dz D Dx ; dt dx dt dx 2 2 d z dx dy d y dx D Cx 2 dt 2 dt dx dx dt 2 dy d y Dx : C x2 dx dx 2

15.

2x

For a particular solution yp of the given equation try y D A. This satisfies the given equation if A D 1=2. Thus the general solution of the given equation is yD

C2 2C3 ln x v0 D w D C x x v D C1 C C2 ln x C C3 .ln x/2 :

14.

y 00 C y 0 2y D 1. The auxiliary equation for y 00 C y 0 2y D 0 is r 2 C r 2 D 0, which has roots r D 2 and r D 1. Thus the complementary function is

x

.A

A

2A/ D

2Ae

x

:

1=2. The general solution of the given 1 e 2

x

C C1 e

2x

C C2 e x :

y 00 C y 0 2y D e x . The complementary function is yh D C1 e 2x C C2 e x , as shown in Exercise 1. For a particular solution try y D Axe x . Then y 0 D Ae x .1 C x/;

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y 00 D Ae x .2 C x/;

653

lOMoARcPSD|6566483

SECTION 18.6 (PAGE 1031)

ADAMS and ESSEX: CALCULUS 9

Thus we require A D eral solution

so y satisfies the given equation if e x D Ae x .2 C x C 1 C x

2x/ D 3Ae x :

yD

1 x xe C C1 e 3

2x

C C3 e x :

8.

5. y 00 C 2y 0 C 5y D x 2 . The homogeneous equation has auxiliary equation r 2 C 2r C 5 D 0 with roots r D 1 ˙ 2i . Thus the complementary function is x

yh D C1 e

cos.2x/ C C2 e

x

4x 25

2 Ce 125

2x

.C1 cos.2x/ C C2 sin.2x//:

7.

De

654

2x

:

8Ax C 4Ax 2 C 8Ax

8Ax 2 C 4Ax 2 /

x

cos x C C2 e

x

sin x:

This satisfies the nonhomogeneous DE if

2x

2x

e x sin x D y 00 C 2y 0 C 2y D e x cos x.2B C 2.A C B/ C 2A/ C e x sin x. 2A C 2.B A/ C 2B/ D e x cos x.4A C 4B/ C e x sin x.4B 4A/:

C C2 e 3x :

Thus we require A C B D 0 and 4.B A/ D 1, that is, B D A D 1=8. The given equation has general solution

For a particular solution, try y D Axe 2x . Then y 0 D e 2x .A 2Ax/ and y 00 D e 2x . 4A C 4Ax/. We have D y 00

:

y 0 D .A C B/e x cos x C .B A/e x sin x y 00 D 2Be x cos x 2Ae x sin x:

1 C C1 cos.2x/ C C2 sin.2x/: 8

yh D C1 e

2x

2x

For a particular solution, try y D Ae x cos x C Be x sin x. Then

y y 6y D e . The homogeneous equation has auxiliary equation r 2 r 6 D 0 with roots r D 2 and r D 3. Thus the complementary function is

e

.2A

yh D C1 e

Thus 2A C 4C D 0, 4A D 1, 4B D 0, and we have 1 1 A D , B D 0, and C D . The given equation has 4 8 general solution

0

C C2 xe

y 00 C 2y 0 C 2y D e x sin x. The homogeneous equation has auxiliary equation r 2 C 2r C 2 D 0 with roots r D 1 ˙ i . Thus the complementary function is

x 2 D y 00 C 4y D 2A C 4Ax 2 C 4Bx C 4C

00

2x

Thus we require A D 1=2. The given equation has general solution   2 x y D e 2x C C1 C C2 x : 2

6. y 00 C 4y D x 2 . The complementary function is y D C1 cos.2x/ C C2 sin.2x/. For the given equation, try y D Ax 2 C Bx C C . Then

1 2 x 4

2x

D 2Ae

9.

yD

C C2 e 3x :

D y 00 C 4y 0 C 4y

De

2

x

2x

y 00 C 4y 0 C 4y D e 2x . The homogeneous equation has auxiliary equation r 2 C 4r C 4 D 0 with roots r D 2, 2. Thus the complementary function is

e

Thus we require 5A D 1, 4A C 5B D 0, and 2A C 2B C 5C D 0. This gives A D 1=5, B D 4=25, and C D 2=125. The given equation has general solution x2 5

C C1 e

For a particular solution, try y D Ax 2 e 2x . Then y 0 D e 2x .2Ax 2Ax 2 / and y 00 D e 2x .2A 8AxC4Ax 2 /. We have

sin.2x/:

D 2A C 4Ax C 2B C 5Ax C 5Bx C 5C:

yD

2x

yh D C1 e

For a particular solution, try y D Ax 2 C Bx C C . Then y 0 D 2Ax C B and y 00 D 2A. We have x 2 D y 00 C 2y 0 C 5y

1 xe 5

yD

We require A D 1=3. The general solution of the given equation is

1=5. The given equation has gen-

y0 2x

yD

6y

. 4A C 4Ax

A C 2Ax

6Ax/ D

5Ae

2x

ex .sin x 8

:

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cos x/ C e

x

.C1 cos x C C2 sin x/:

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 18.6 (PAGE 1031)

10. y 00 C 2y 0 C 2y D e x sin x. The complementary function is the same as in Exercise 9, but for a particular solution we try

Thus we require A D 0 and B D 1=6. The given equation has general solution

Bx

x

sin x D y 00 C 2y 0 C 2y D 2Be x cos x 2Ae

Thus we require B D 0 and A D tion has general solution yD

11.

00

1 xe 2

x

cos x C e

0

x

x

x

C C1 e

x

C C2 xe

x

:

Ax/ 13.

This satisfies the nonhomogeneous DE if e

1 3 x e 6

yD

y D Axe x cos x C Bxe x sin x y 0 D e x cos x.A Ax C Bx/ C e x sin x.B y 00 D e x cos x.2B 2Bx 2A/ C e x sin x.2Ax 2A 2B/:

y 00 C y 0 2y D e x . The complementary function is yh D C1 e a particular solution use 2x

yp D e

sin x:

2x

C C2 e x . For

u1 .x/ C e x u2 .x/;

where the coefficients u1 and u2 satisfy

1=2. The given equa2x 0 u1 2x 0 u1

2e e

.C1 cos x C C2 sin x/:

Thus

y C y D 4 C 2x C e . The homogeneous equation has auxiliary equation r 2 C r D 0 with roots r D 0 and r D 1. Thus the complementary function is yh D C1 C C2 e x . For a particular solution, try y D Ax C Bx 2 C C xe x . Then

C

u1 D

e x u20

1 x 1 x e e D 3 6 solution of the given equation is yD

1 e 2

x

D 0:

u20 D

Thus yp D

y 0 D A C 2Bx C e x .C C x/ y 00 D 2B C e x . 2C C C x/:

x

1 2x e 3 1 2x e : u2 D 6

1 x e 3 1 x e 3

u10 D

x

C e x u20 D e

C C1 e

1 e 2

2x

x

. The general

C C2 e x :

This satisfies the nonhomogeneous DE if 4 C 2x C e

x

14.

D y 00 C y 0 D A C 2B C 2Bx

x

Ce

:

Thus we require A C 2B D 4, 2B D 2, and C D 1, that is, A D 2, B D 1, C D 1. The given equation has general solution y D 2x C x

2

xe

x

C C1 C C2 e

x

y 00 C y 0 2y D e x . The complementary function is yh D C1 e a particular solution use yp D e

2e e

y0 D e

y 00 D e

x x

.2Ax C .3B

.2A C .6B

A/x 2

Bx 3 /

4A/x

.6B

A/x 2 C Bx 3 /:

Thus u10 D u1 D

xe

00

0

D y C 2y C y D e x .2A C 6Bx/:

u1 .x/ C e x u2 .x/;

2x 0 u1 2x 0 u1

C e x u20 D e x

C e x u20 D 0:

1 3 1 u2 D x: 3

1 3x e 3 1 3x e 9

u20 D

1 x 1 e C xe x . The general solution of the 9 3 given equation is Thus yp D

This satisfies the nonhomogeneous DE if x

C C2 e x . For

where the coefficients u1 and u2 satisfy

:

12. y 00 C 2y 0 C y D xe x . The homogeneous equation has auxiliary equation r 2 C 2r C 1 D 0 with roots r D 1 and r D 1. Thus the complementary function is yh D C1 e x C C2 xe x . For a particular solution, try y D e x .Ax 2 C Bx 3 /. Then

2x

2x

yD D

1 x 1 e C xe x C C1 e 9 3 1 x xe C C1 e 3

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2x

2x

C C2 e x

C C3 e x :

655

lOMoARcPSD|6566483

SECTION 18.6 (PAGE 1031)

15.

ADAMS and ESSEX: CALCULUS 9

x 2 y 00 C xy 0 y D x 2 . If y D Ax 2 , then y 0 D 2Ax and y 00 D 2A. Thus x 2 D x 2 y 00 C xy 0 2

The term x=4 can be absorbed into the term C1 x in the complementary function, so the general solution is

y

D 2Ax C 2Ax

2

2

yD

2

Ax D 3Ax ;

so A D 1=3. A particular solution of the given equation is y D x 2 =3. The auxiliary equation for the homogeneous equation x 2 y 00 C xy 0 y D 0 is 4r.r 1/ C r 1 D 0, or r 2 1 D 0, which has solutions r D ˙1. Thus the general solution of the given equation is yD

19.

C2 1 2 x C C1 x C : 3 x

Accordingly, we look for a particular solution of the given equation having the form

Thus A D 1=.r 2 is

 1 D Ax r .r 2

1/ C r

The homogeneous DE y 00 2y 0 C y D 0 has auxiliary equation r 2 2r C 1 D 0 with roots r D 1; 1. Therefore, its general solution is y D C1 e x C C2 xe x :

16. x 2 y 00 C xy 0 y D x r has a solution of the form y D Ax r provided r ¤ ˙1. If this is the case, then  x r D Ax r r.r

yp D u1 .x/e x C u2 .x/ xe x : According to the procedure developed in the text, u10 and u20 can be determined by solving the pair of equations

1/:

u10 .x/e x C u20 .x/xe x D 0

1/ and a particular solution of the DE yD

1 r2

u10 .x/e x C u20 .x/.1 C x/e x D

r

1

1 C2 x ln x C C1 x C : 2 x

x :

ex x

or, equivalently, 17.

x 2 y 00 C xy 0 y D x. Try y D Ax ln x. Then y 0 D A.ln x C 1/ and y 00 D A=x. We have x D x2

A C xA.ln x C 1/ x

u10 .x/ C xu20 .x/ D 0 u10 .x/ C .1 C x/u20 .x/ D

Ax ln x D 2Ax:

The solution is

Thus A D 1=2. The complementary function was obtained in Exercise 15. The given equation has general solution yD

u10 .x/ D

1 C2 x ln x C C1 x C : 2 x

y D x. 1 Try y D xu1 .x/ C u2 .x/, where u1 and u2 satisfy x u20 D 0; x

u10

u20 D Thus u1 D

x ; 2

1 ln x and u2 D 2 yD

656

u10 D

1 : 2x

20.

2

1 x ln x 2

1 : x

The homogeneous DE y 00 C 4y 0 C 4y D 0 has auxiliary equation r 2 C4r C4 D 0 with roots r D 2; 2. Therefore, its general solution is y D C1 e

x . A particular solution is 4

u20 .x/ D

y D C1 e x C C2 xe x C xe x ln x:

u20 1 D : 2 x x

Solving these equations for u10 and u20 , we get

1;

Thus u1 .x/ D x and u2 .x/ D ln x. A particular solution of the DE is yp D xe x C xe x ln x, or, since the first term is a solution of the homogeneous equation, the simpler form yp D xe x ln x will do. The given equation has general solution

18. x 2 y 00 C xy 0

xu10 C

1 : x

2x

C C2 xe

2x

:

Accordingly, we look for a particular solution of the given equation having the form

x : 4

yp D u1 .x/e

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2x

C u2 .x/ xe

2x

:

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 18.7 (PAGE 1040)

According to the procedure developed in the text, u10 and u20 can be determined by solving the pair of equations u10 .x/e 2x

C

u20 .x/xe 2x

2x

2u10 .x/e

C .1

D0

2x/u20 .x/e

2x

D

where u1 and u2 satisfy x 

2x

e

x2

or, equivalently, u10 .x/ C xu20 .x/ D 0 2u10 .x/ C .1

2x/u20 .x/ D

.sin x/u20 D 0  1 3=2 x cos x x 1=2 sin x u10 2   1 3=2 1=2 x sin x x cos x u20 D x 2

1=2

.cos x/u10 C x

1 ; x

u20 .x/ D

1 : x2

1 : x2

which have solutions u10 D sin x, u20 D cos x, so that u1 D cos x and u2 D sin x. Thus a particular solution of the given equation is

ln x and u2 .x/ D

y D C1 e

21.

2x

C C2 xe

2x

xe

2x

yDx

1.

u10 C .1 C x/e x u20 D x:

 22. x y C xy C x 2

 1 y D x 3=2 . 4 A particular solution can be obtained in the form 1=2

.cos x/u1 .x/ C x

1=2

sin2 x D x

1=2

:

  1 C C2 cos x C C2 sin x :

By the Shifting Principal, Lfe at cos bt g is the Laplace transform of cos.bt / with s replaced by s a. Thus, by Example 1, s a : .s a/2 C b 2

This is valid for s > max a; 0. Inversely, L

2.

1



 s a D e at cos.bt /: .s a/2 C b 2

By the Shifting Principal, Lfe at sin bt g is the Laplace transform of sin.bt / with s replaced by s a. Thus, by Example 1,

x 2 C C1 x C C2 xe x :

0

yDx

1=2

Lfe at cos bt g D

Solving these equations for u10 and u20 , we get u10 D 1 and u20 D e x . Thus u1 D x and u2 D e x . The particular solution is y D x 2 x. Since x is a solution of the homogeneous equation, we can absorb that term into the complementary function and write the general solution of the given DE as

1=2

Section 18.7 The Laplace Transform (page 1040)

where u1 and u2 are chosen to satisfy

2 00

cos2 x C x

The general solution is

y D xu1 .x/ C xe x u2 .x/;

yD

1=2

yDx

ln x:

x 2 y 00 .2x C x 2 /y 0 C .2 C x/y D x 3 . Since x and xe x are independent solutions of the corresponding homogeneous equation, we can write a solution of the given equation in the form

xu10 C xe x u20 D 0;

:

.cos x/u10 C .sin x/u20 D 0 .sin x/u10 C .cos x/u20 D 1;

1 . A particular x 2x solution of the DE is yp D e ln x e 2x , or, since the last term is a solution of the homogeneous equation, the simpler form yp D e 2x ln x will do. The given equation has general solution Thus u1 .x/ D

1=2

We can simplify these equations by dividing the first by x 1=2 , and adding the first to 2x times the second, then dividing the result by 2x 1=2 . The resulting equations are

The solution is u10 .x/ D

1=2

Lfe at sin bt g D

.s

b : a/2 C b 2

This is valid for s > max a; 0. Inversely,

.sin x/u2 .x/;

L

1



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.s

 b D e at sin.bt /: a/2 C b 2

657

lOMoARcPSD|6566483

SECTION 18.7 (PAGE 1040)

3.

Lfcosh.at /g D L



e at C e 2

at



ADAMS and ESSEX: CALCULUS 9

D

1 2



1

s s

D

a

: s 2 a2 This nis valid for o s > jaj. Inversely, s L 1 2 D cosh.at /. s a2    at 1 1 e e at D 4. Lfsinh.at /g D L 2 2 s a a D 2 : s a2 This nis valid for s > jaj. Inversely, a o D sinh.at /. L 1 2 s a2

C

1 sCa

1 sCa



11.

As already seen in the first few lines of the proof, the formula LfF .n/ .t /g D s n f .s/ h s n 1 F .0/ C s n 2 F 0 .0/ C : : : C F .n



Now consider LfF .k/ .t /g D Lf.F .k .k 1/

Inversely, L

1



.s

nŠ a/nC1

.s

for s > maxfa; 0g:

 nŠ D t n e at . a/nC1

D s k jfF .t /g C sF .k

Lft e

gD

.s

nŠ.s C i b/nC1 nŠ D i b/nC1 .s 2 C b 2 /nC1 nC1

Inversely, L 7.

1 nŠ.s C i b/ .s 2 C b 2 /nC1

for s > 0:

.s C i b/2 .s 2 C b 2 /2 2 ibt

9. By Exercise 5 and since t e we have



s2 b2 : D 2 .s C b 2 /2

D

2bs : .s 2 C b 2 /2

kLft k



.s C i b/3 .s 2 C b 2 /3



.0/:

F 0 .0/ C   

1/

3bs 2 b 3 : .s 2 C b 2 /3

1

gDL



1 0Š D .0C1/ : s s

gD

.k

1/Š sk

 d k t D sLft k g dt

for some k  1.

0k D sLft k g

kŠ k .k 1/Š D kC1 : k s s s This completes the induction. Lft k g D

13.

In the formula €.p C 1/ D

Z

1

pe



d

0

make the change of variable  D st , d  D s dt to obtain

s 3 3b 2 s D 2 : .s C b 2 /3

D

2

and so

2

10. By Exercise 6 and since t 2 e ibt D t 2 cos.bt / C i t 2 sin.bt /, we have 

1/

Now suppose that Lft .k

D t cos.bt / C i t sin.bt /,

.s C i b/3 Lft 2 cos.bt /g D < .s 2 C b 2 /3

Lft 2 sin.bt /g D =

.0/ C F .k

Lft 0 g D L.1/ D

2



F .0/ C s k

12. As observed in the example,

8. By Exercise 6 and since t e ibt D t cos.bt / C i t sin.bt /, we have 

2/

1

Then, by Theorem 5,



.s C i b/2 Lft cos.bt /g D < .s 2 C b 2 /2

/ .t /g

That is, the formula holds for n D k if it holds for n D k 1.

By Exercise 5 and since t e ibt D t cos.bt / C i t sin.bt /, we have

Lft sin.bt /g D =

Œs k

D t n e ibt .



1/ 0

.k 1/

D sLfF .t /g F .0/ by the known case n D 1  k 1 k 2 Ds s LfF .t /g Œs F .0/ C s k 3 F 0 .0/ C     C F .k 2/ g.0/ F .k 1/ .0/ by the assumption

6. By the Shifting Principal and Example 3 n ibt

i .0/ :

holds if n D 1. To complete the induction assume the formula holds for n D k 1  1, that is, h LfF .k 1/ .t / D s .k 1/ LfF .t /g s k 2 F .0/Cs k 3 F 0 .0/C  CF .k

5. By the Shifting Principal and Example 3, Lft n e at g D

1/

€.p C 1/ D s pC1

Z

1

tp e

0

st

dt D s pC1 Lft p g:

Therefore, we have Lft p g D €.p C 1/=s pC1 : 14.

Since I10 .t / D F .t / and I1 .0/ D 0 we have f .s/ D LfF .t /g D sLfI1 .t /g

658 Copyright © 2018 Pearson Canada Inc. Downloaded by ted cage ([email protected])

and so LfI1 .t /g D

f .s/ s

2/

i .0/ :

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

15.

SECTION 18.7 (PAGE 1040)

f .s/ 1 Similarly, LfI2 .t /g D LfI1 .t /g D 2 , and, in general, s s 1 LfIn .t /g D f .s/. sn Z 1 t e st F .t / dt D LftF .t /g f 0 .s/ D 0 Z 1 f 00 .s/ D . 1/2 t 2 e st F .t / dt

Adding these fractions and equating coefficients of powers of s with the numerator s, we obtain A D 1=6, B D 1=6, and C D 1=3. Thus Lfyg D

yD 19.

2as a d D 2 ds s 2 C a2 .s C a2 /2 d s 2 a2 s D : ds s 2 C a2 .s 2 C a2 /2

Lft sin at g D Lft cos at g D

Thus Lfx.t /g D

Lfzg D

s2 !2 .s 2 C ! 2 /2 s2 C !2 2! 2 D 2 .s C ! 2 /2 .s 2 C ! 2 /2 1 D 2 2! Lfx.t /g s C !2 1 D Lfsin.!t / 2!Lfx.t /g: !

17.

s 2 Lfyg 3s C 4 C 2.sLfyg .s 2 C 2s/Lfyg D 3s C 2.

18. s 3 Lfyg

Lfyg D

2t

0/ C 6Lfzg D 0

2t

0

e

3t

, and y D e

2.t a/

1 : sC3 e

3.t a/

.

2 0 C Lfyg D Lft 2 g D 3 . Thus s

C Ds C E A B 2 D C 2C 3 C 2 : s 3 .s 2 C 1/ s s s s C1

and the initial-value problem has solution yD

21.

s 2 Lfyg

s

2 C t 2 C 2 cos.t /:

2 C 2.sLfyg

1/ C Lfyg D

.s C 1/2 Lfyg D s C 4 C

3/ D 0. Thus

1 Thus sC1

1 sC1

and

.

Lfyg D

sC4 1 1 1 3 C D C : C .s C 1/2 .s C 1/3 s C 1 .s C 1/2 .s C 1/3

Accordingly, y D e

s C 8Lfyg D 0, so s3

1 .s 1/ C 3 C sC2 .s 1/2 C 3

Adding the fractions on the right and equating coefficients of like powers of s in the numerator with the expression 2 in the left numerator we obtain five equations that are easily solved for A D 2, C D 2, D D 2, B D E D 0. Thus 2s 2 2 C 3C 2 Lfyg D s s s C1

3s C 2 1 2 Lfyg D D C : s.s C 2/ s sC2 We have y D 1 C 2e



p p  p C e t cos. 3t / C 3 e t sin. 3t / :

1 C 5.sLfzg

We have s 2 Lfyg

Solving for Lfx.t /g we obtain

 !t cos.!t / .

1 6

1 1 1 D D s 2 C 5s C 6 .s C 2/.s C 3/ sC2

Lfyg D

Lft cos.!t g D

1  Hence x.t / D sin.!t / 2! 2

2t

Accordingly, z D e 20.

 !Lft cos.!t /g :

D

Let z.t / D y.t C a/ so that z 0 D y 0 , z 00 D y 00 , z.0/ D y.a/ D 0, and z 0 .0/ D y 0 .a/ D 1. Then we have

Now consider the result

1  Lfx.t /g D Lfsin.!t /g 2! 2



which we solve to obtain

! : s2 C !2

! : .s 2 C ! 2 /2

1 e 6

s 2 Lfzg

16. We have s 2 Lfx.t /g C ! 2 Lfx.t /g D Lfsin.!x.t /g D

1 sC2 C 2 sC2 s 2s C 4

so we have

0

In general, every further differentiation contributes another factor . t / to the integrand. a s Since Lfsin at g D 2 and Lfcos at g D 2 , s C a2 a C s2 we have



1 6

22. s s A Bs C C D D C 2 : 2 C8 .s C 2/.s 2s C 4/ sC2 s 2s C 4

s 2 Lf g

s 0/

Copyright © 2018 Pearson Canada Inc. Downloaded by ted cage ([email protected])

t

  1 2 1 C 3t C t : 2  0 .0/ C

g Lf g D ˛Lfı.t l

1/g

659



lOMoARcPSD|6566483

SECTION 18.7 (PAGE 1040)

Lf g.s 2 C

Lf g D ˛

s

ADAMS and ESSEX: CALCULUS 9

g / D ˛e l r

l e g

s

s

after employing the periodic property of F . Converting back to dummy variable t , then substituting into the series of integrals leads us to,

g l

h LfF .t /g D 1 C e

g l

s2 C

From Example 6

 D˛

s

l sin g

r

 1/ H.t

g .t l

1/:

LfF .t /g D

Z

Lfug.s 2

2/ C 3Lfvg D 0 1 Lfvg.s 2 C 2/ C 4Lfug D s

3 3 3 1 2 2 C 64 s 2 4 64 s 2 C 4 16 s

s.s 2

1 2 .s 2 2/ D 4/.s 2 C 4/ 32 s 2 4

2

sin.t /e

3 sinh.2t / 64 1 sinh.2t / 32

26.

3 2 11 C : 32 s 2 C 4 8 s

3 sin.2t / C 64 3 sin.2t / C 32

3sT

C :::

iZ

T

F .t /e 0

F .t /e

st

dt:

0

1 s2

e s2 : C1

1 s2 C 1

Transforming in t leads to, LfU.x; t /g D u.x; s/, LfU t t .x; t /g D s 2 u.x; s/, LfUxx .x; t /g D uxx .x; s/, LfU.0; t /g D u.0; s/ D g.s/, and limx!1 u.x; s/ D 0, or s 2 u.x; s/ D uxx .x; s/ which has the general solution, according to Section 18.5, of sx

C Be sx :

But limx!1 u.x; s/ D 0 means B D 0 and u.0; s/ D g.s/ means A D g.s/. Thus u D g.s/e sx . but by Table 6 L 1 fg.s/e sx g D H.t x/G.t x/ D U.x; t /: The meaning is that the disturbance at x D 0, G.t /, propagates at a speed given by t x D constant, that is, points on the graph of G.t / move rightward at speed dx=dt D 1. The Heaviside function however excludes points where x > t from this. The disturbance has not yet arrived a those points in the previously still medium.

3 16 1 : 8

From Table 6 f .s/ D Lfe at g D 1=.s a/. f 0 .s/ D 1=.s a/2 and f 0 .s/ D Lf t e at g by direct differentiation under the integral. Thus Lft e at g D 1=.s a/2 :

25.

T

dt D

is confirmed.

u D Ae

v.t / D 24.

st

0

Using Table 6, u.t / D

Z

sT

Lfsin t g D

and Lfvg D

1

1 e

Thus

Solving the linear equations in the transforms and using partial fractions, 3 D 4/.s 2 C 4/

Ce

In the case of sin t , T D 2, so

23.

s.s 2

.2sT

Ce

The prefactor sum is a geometric series with common ratio r D e sT < 1 for positive s and t , and so converges to   1 1 e sT :Thus

After a short while this will damp out, although this was not accounted for in the equation. The owner would be better off to get up and wind the clock.

Lfug D

sT

27. LfF .t /g D D

Z

Z

Z

1

F .t /e

st

F .t /e

st

T 0 3T

F .t /e 2T

(a) Let Lfi.t /g D I.s/: Using Table 6,

dt

0

dt C

st

Z

nT

.n 1/T

660

F .t /e

st

dt D e

F .t /e

st

T

dt C

Lf.t /g  E.s/ D RI.s/ C LsI.s/ C

dt C : : : :

After making the substitution  D t integral we find that Z

2T

.n 1/sT

.n Z

I.s/ D 1/T on the nth

T

F ./e

s

1 I.s/ C s

sE.s/ Ls 2 C Rs C

1 C

(b) Differentiating the circuit equation with R D 0, then dividing by L,

d ;

0

Copyright © 2018 Pearson Canada Inc. Downloaded by ted cage ([email protected])

i 00 .t / C

1 i.t / D  0 .t /=L; LC

st

dt:

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 18.8 (PAGE 1045)

which is the second order differential equation for the harmonic oscillator with forcing function  0 .t /=L and frequency squared ! 2 D 1=LC: (c)

Thus a2 D a3 D 0, and anC2 D Given a0 and a1 we have

a0 34 a0 a4 D a8 D 78 3478 :: : a0 a4n D 3  4  7  8      .4n 1/.4n/ a0 D n 4 nŠ  3  7      .4n 1/ a1 a5 D 45 a5 a1 a9 D D 89 4589 :: : a1 a4nC1 D 4  5  8  9      .4n/.4n C 1/ a1 D n 4 nŠ  5  9      .4n C 1/ a4nC3 D a4nC2 D    D a3 D a2 D 0: a4 D

s I.s/ D E.s/ L.s 2 C ! 2 / From Table (6) It follows that Z 1 t i.t / D Lı.t  1/ cos !d  D H.t 1/ cos !.t 1/: L 0

28. (a) We have

Z 1 2 Z 1 D 2

f .t / D

 f ./e i! d  e i!t d! 1 1 Z 1 1 f ./ d  e i!.t / d!: 1

Z

1

1

1

But we know that for any continuous function, Z 1 ı.t / f ./ d  D f .t /: 1

Therefore we must have Z 1 ı.t / D 2

1

The solution is

e i!t dt:

1

(b) Let ! D

 in the last integral above: Z 1 Z 1 1 e it . d / D ı.t / D 2 1 2

1

y D a0 1 C it

e

1

d  D ı. t /:

1 X

nD1

C a1 x

1.

y D .x yD y 00 D

2.

2

1/ y. Try

1 X

an .x

nD0 1 X

n.n

1/n : y0 D 1/an .x

1/n

2

nD2 1 X

y 00 D

.n C 2/.n C 1/anC2 .x

1/n

0 D y 00 .x 1/2 y 1 X D .n C 2/.n C 1/anC2 .x

1/n

D

D

nD0

nD0 1 X

.n C 2/.n C 1/anC2 .x

1 X

nD0 1 X

1 X

1 X

nD1

1/

!

! .x 1/ : 4n nŠ  5  9      .4n C 1/ 4nC1

an x n . Then

nD0

nan x n

1

D

1 X

nD2

1

nD1

1/an x n

n.n

nan x n

2

D

1 X

.n C 2/.n C 1/anC2 x n :

nD0

Thus we have 1 X

nD0 1 X

1/n

nD0

D 2a2 C 6a3 .x 1/ 1 h X C .n C 2/.n C 1/anC2 nD2

y 00 D xy. Try

.x 1/4n n 4 nŠ  3  7      .4n

1C

Section 18.8 Series Solutions of Differential Equations (page 1045) 00

an 2 for n  2. .n C 1/.n C 2/

an .x an

1/nC2

2 .x

nD2

an

2

i

.x

1/n

0 D y 00 xy 1 X D .n C 2/.n C 1/anC2 x n D

1/n :

nD0 1 X

nD0

.n C 2/.n C 1/anC2 x n

D 2a2 C

1 h X

nD1

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1 X

nD0 1 X

an x nC1 an

1x

n

nD1

.n C 2/.n C 1/anC2

an

1

i

xn :

661

lOMoARcPSD|6566483

SECTION 18.8 (PAGE 1045)

Thus a2 D 0 and anC2 D Given a0 and a1 , we have

ADAMS and ESSEX: CALCULUS 9

an 1 for n  1. .n C 2/.n C 1/

Since a0 D y.0/ D 1, and a1 D y 0 .0/ D 2, we have a0 D 1 a2 D 1 1 a4 D 3

a0 23 a0 1  4  a0 a3 D D a6 D 56 2356 6Š a6 1  4  7  a0 a9 D D 89 9Š :: : 1  4      .3n 2/a0 a3n D .3n/Š 2  a1 a1 D a4 D 34 4Š a4 2  5  a1 a7 D D 67 7Š :: : 2  5      .3n 1/a1 a3nC1 D .3n C 1/Š 0 D a2 D a5 D a8 D    D a3nC2 : a3 D

y D a0

2/

nD1

1 X 2  5      .3n C a1 .3n C 1/Š

1/

x

3n

!

x 3nC1 :

nD1

3.

8 < :

Let

y 00 C xy 0 C 2y D 0 y.0/ D 1 y 0 .0/ D 2

yD y 00 D

1 X

nD0 1 X

an x

n

1 35 1 a8 D 357

1/an x n

n.n

The patterns here are obvious: . 1/n 3  5      .2n . 1/n 2n nŠ D .2n/Š

a2n D

Thus y D

1 X

nan x

n 1

2

D

nD0

an x n D 0;

nD0 1 X

2a2 C 2 C

y 00 D

1/n



an x n , then y 0 D

1 X

n.n

nD0

1/an x n

nD2

1 X

.n C 2/.n C 1/anC2 x n :

1 X

662

nD1

D

1 X

nan x n

1

and

.n C 2/.n C 1/anC2 x n :

nD0

D 2a2 C a0 C

nD1

nD1

so

Œ.n C 2/.n C 1/anC2 C .n C 2/an x n D 0:

anC2 D

an ; nC1

1

C

1 X

n D 1; 2; 3; : : : :

an x n

nD0

i .n C 2/.n C 1/anC2 C .n C 1/an x n :

Since coefficients of all powers of x must vanish, therefore 2a2 C a0 D 0 and, for n  1, .n C 2/.n C 1/anC2 C .n C 1/an D 0; an : that is, anC2 D nC2

nan x n

nD1

1;

2

P1

nD1

1 h X

1 1 If y.0/ D 1, then a0 D 1, a2 D , a4 D 2 , 2 2  2Š 1 1 , a8 D 4 ,: : :. If y 0 .0/ D 0, then a6 D 3 2  3Š 2  4Š a1 D a3 D a5 D : : : D 0. Hence,

It follows that a2 D

1/

. 1/n 2 2n nŠ

 x 2nC1 2n nŠx 2n C n 1 . .2n/Š 2 nŠ

1 X

nD0

.n C 2/.n C 1/anC2 x n C C2

If y D

nD0 .

nD0

nD1

nD2

1 X

4.

P1

a2nC1 D

0 D y 00 C xy 0 C y 1 1 X X D .n C 2/.n C 1/anC2 x n C x nan x n

Substituting these expressions into the differential equation, we get 1 X

2 246 2 a9 D : 2468

a7 D

Thus,

0

y D

2 2 2 a5 D 24 a3 D

a6 D

Thus the general solution of the given equation is 1 X 1  4      .3n 1C .3n/Š

a1 D 2

yD1

1 2 1 4 x C x 2 8

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1 X . 1/n 2n 1 6 x C  D x : 48 2n  nŠ nD0

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 18.8 (PAGE 1045)

5. y 00 C .sin x/y D 0, y.0/ D 1, y 0 .0/ D 0. Try

Therefore we have a2 D a4 D a6 D    D 0 4 ; a5 D 0 D a7 D a9 D    : a3 D 3

y D a0 C a1 x C a2 x 2 C a3 x 3 C a4 x 4 C a5 x 5 C    : Then a0 D 1 and a1 D 0. We have 00

The initial-value problem has solution

2

3

y D 2a2 C 6a3 x C 12a4 x C 20a5 x C      x3 x5 .sin x/y D x C  6 120  .1 C a2 x 2 C a3 x 3 C a4 x 4 C a5 x 5 C   /   1 D x C a2 x 3 C a3 x 4 6   1 1 a2 C x5 C    : C a4 6 120

7.

3xy 00 C 2y 0 C y D 0. Since x D 0 is a regular singular point of this equation, try 1 X yD an x nC .a0 D 1/ y0 D

Hence we must have 2a2 D 0, 6a3 C 1 D 0, 12a4 D 0, 1 20a5 C a2 D 0, : : : . That is, a2 D 0, a4 D 0, 6 1 1 , a5 D . The solution is a3 D 6 120

6. .1

x 2 /y 00

xy 0 C 9y D 0, y.0/ D 0, y 0 .0/ D 1. Try yD

1 X

an x n :

y 00 D

1 X

nD1 1 X

nan x n n.n

nD0

2

1 X

nD0

nD1

n

nan x C 9

an x

1/an x nC

1

nD0

D .32 /x  1 1 h X C 3.n C /2

2

:

C

1 X

an

1x

nC 1

nD1

 .n C / an C an

1

i

x nC

1

:

 D 0 and an D

1 ; 12

n.n

:: :

1/an x n

an D

n

nD0

a2 D

1 1225

1 122538

a3 D

nD2

D 2a2 C 9a0 C .6a3 C 8a1 /x 1 h X C .n C 2/.n C 1/anC2

. 1/n nŠ  2  5      .3n

1/

:

One series solution is .n

nD2

Thus 2a2 C 9a0 D 0, 6a3 C 8a1 D 0, and anC2 D

.n C /.n C 

nD0

a1 D

nD2

1 X

1

an 1 for 3.n C /2 .n C / n  1. There are two cases:  D 0 and  D 1=3. an 1 . Since a0 D 1 CASE I.  D 0. Then an D n.3n 1/ we have

0 D .1 x 2 /y 00 xy 0 C 9y 1 X D .n C 2/.n C 1/anC2 x n 1 X

.n C /an x nC

nD0 1 X

0 D 3xy 00 C 2y 0 C y 1 h i X D 3.n C /2 .n C / an x nC

Thus 32

1

1/an x n

nD0 1 X

nD1

Then a0 D 0 and a1 D 1. We have y0 D

y 00 D Then we have

1 5 1 3 x C x C : 6 120

yD1

4 3 x : 3

yDx

.n2 9/an : .n C 1/.n C 2/

2

i 9/an x n :

y D1C

1 X

nD1

. 1/n x n nŠ  2  5      .3n

1 . Then 3 an an D  1 2 3 nC 3

1/

:

CASE II.  D

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1

nC

1 3

 D

an 1 : n.3n C 1/

663

lOMoARcPSD|6566483

SECTION 18.8 (PAGE 1045)

ADAMS and ESSEX: CALCULUS 9

Since a0 D 1 we have 1 ; 14

a1 D

1 1427

a2 D

Section 18.9 Dynamical Systems, Phase Space, and the Phase Plane (page 1058)

1 1  4  2  7  3  10

a3 D :: :

1.

. 1/n an D : nŠ  1  4  7      .3n C 1/ A second series solution is yDx

1=3

1C

1 X

nD1

! . 1/n x n : nŠ  1  4  7      .3n C 1/

2.

8. xy 00 C y 0 C xy D 0. Since x D 0 is a regular singular point of this equation, try 1 X yD an x nC .a0 D 1/ y0 D y 00 D

nD0 1 X

nD0 1 X

nD0

.n C /an x nC

1

.n C /.n C 

1/an x nC

3. 2

:

Then we have 0 D xy 00 C y 0 C xy 1 h X D .n C /.n C  nD0

C D

1 X

1 X

i 1/ C .n C / an x nC

1

4.

an x nCC1

nD0

.n C /2 an x nC

nD0 2  1

2

D x

1

C 

an

2x

nC 1

5.

nD2

C .1 C / a1 x 1 h X C .n C /2 an C an nD2

1 X

2

i x nC

1

:

an 2 for n  2. Thus  D 0, a1 D 0, and an D n2 It follows that 0 D a1 D a3 D a5 D   , and, since a0 D 1, 1 1 ; a4 D 2 2 ; : : : 22 2 4 . 1/n . 1/n D 2 2 D 2n : 2 2 4    .2n/ 2 .nŠ/2

a2 D a2n

One series solution is

6.

8 ˆ
0 and v D .4 2C2/u; u < 0: 8 ˆ
r2 > 0, confirming that the origin is an unstable node. Note that p 3C 3 p 1 r1 a 1C 3 2 p.r1 / D D D 0: p.r2 / D b 2 4

8. For the system

ˆ :

Similarly, dividing the numerator and denominator of the general slope formula by e r1 t enables us to calculate p

v.t / D p.r1 / D lim t!1 u.t /

:

For the green trajectory with om ega limit point at the origin we need u ! 0 and v ! 0 as t ! 1. Thus we need C2 D 0 and the green trajectories have equations p p v D .4 2 2/u; u > 0 and v D .4 2 2/u; u < 0:

3 1 ; 4

the twopsides of the blue straight trajectory are given by 4v . 3 1/ D 0, u > 0 or u < 0.

p 4 2t

p 4 2t

p

3C1 ; 4

p so the green trajectories are given by 4v C.1C 3/u D 0. 9.

Discarding terms of second degree and higher we have 8 ˆ < ˆ :

u0 D 2u v v 0 D u C 2v;

which has the characteristic equation .2 r/2 C 1 D 0 so r D 2 ˙ i . As the real part is non-zero, it is hyperbolic, so it is topologically the same as the fixed point in the full equations. Thus the origin is an unstable focus. 10. As in example 6, .D a/u bv D 0 : cu C .D d /v D 0: This yields the same differential equations for u and v, and the same auxiliary equation, r 2 .a C d /r C .ad bc/ D 0. Accordingly the eigenvalues of A will be its root(s). But there is only one root, so  D .a d /2 4bc D 0 and thus rD

.a C d / : 2

As before .r

a/.r

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d/

bc D 0;

or

p.r/ D 1; q.r/

665

lOMoARcPSD|6566483

SECTION 18.9 (PAGE 1058)

ADAMS and ESSEX: CALCULUS 9

where q.r/ D c=.r d / and p.r/ D .r a/=b: The (identical) second order DEs for u and v have general solutions in this case (see Section 18.5),

13.

(a) The characteristic equation is r 2 C 2r D 0 which implies two eigenvalues: 0,-2. Thus u D C1 C C2 e 2t and v D B1 C B2 e 2t :

(c) The derivatives will also be linear polynomials multiplying e rt . This implies a zero in each. When formed as a ratio, this gives the slope, implying horizontal and vertical tangents at particular values of t . This implies one reversal in direction for each trajectory. Thus we expect that the trajectory direction on leaving the fixed point (large negative t ) has the opposite direction to what it has for large positive t .

12.

The matrix is diagonal, so for repeated roots r D a D d . This yields .D a/u 0v D 0 : 0u C .D a/v D 0: Thus 0 1

2

0 1

0 13

0

1

B C at B C 6 B C B C7 at @ u A D 4C1 @ 1 A C C2 @ 0 A5 e D @ C1 A e : C2 v 0 1 The trajectories are all straight lines passing through the origin, with slope C2 =C1 .

666

0 1

The fixed points are given by 0

1

0 1

0 1

B 0C B C B C 2t @ u A D @ 0 A D 2C2 @ 1 A e : 1 v0 0

(a) If r > 0 the fixed point is unstable. With both roots the same sign, and  D 0 standing between the cases  > 0 and  < 0, the repeated roots case stands between the focus and node cases. (b) From the expression in the previous exercise, the trajectory chosen by setting C2 D 0 will be a straight line with slope p.r/ and equation v D p.r/u. Note that unlike a node or saddle the choice C1 D 0 does not yield a constant for v=u. But for large jt j, the terms in t will dominate the coefficients of e rt . v=u will then also approach a constant, p.r/, meaning that v D p.r/u is an asymptote for t ! ˙1. Because the coefficients C1 and C2 uniquely define a trajectory, C2 must change sign across the asymptote where C2 D 0. Thus the direction of asymptotic growth must reverse too.

1

B C B C 2t B C @ u A D C1 @ 1 A C C2 @ 1 A e : 1 1 v

Substituting these expressions into .Ž/, we find B1 D p.r1 /C1 C C2 =b and B2 D p.r2 /C2 , recalling that p.r/ D q.r/, ensuring that the two remaining equations add nothing new and so there must be two free constants. This yields the desired expression upon substitution.

11.

0

0 1

u D .C1 C C2 t /e rt v D .B1 C B2 t /e rt :

Thus a fixed point requires C2 D 0; from which we conclude that all points satisfying v D u are fixed points. The zero eigenvalue places this case between the saddle and the unstable node, because zero marks the transition between both eigenvalues having the same sign and eigenvalues with opposite sign. (b) A li ne of fixed points v D u bisects the plane. On either side, trajectories with constant slope 1 move away from every fixed point. 14.

15.

The derivatives are zero everywhere, so every point in the phase plane is a fixed point. Small adjustments can take this into all any of the other cases. It is the ultimate nonrobust case, adjacent in terms of parameters to all others. (a) u0 D 0 if either u D 0 or u C v D 3, and v 0 D 0 if either v D 0 or u D 1. Thus there are three fixed points: A D .0; 0/, B D .3; 0/, and C D .1; 2/. Linearizing around   A we obtain the matrix 3 0 A D , which has eigenvalues  D 3 or 0 v 1. Thus A is a saddle. To linearize around B, let U D u 3 and V D v. Then   U 0 D u0 D u.3 u v/ D .U C 3/ 3 .U C 3/ V 0

0

D

3U

V D v D v.u

U.U C V /   1/ D V .U C 3/ 1 D 2V C U V: 3V

 3 3 , 0 2 3. Thus B is also a

The linearization thus has matrix A D which has eigenvalues  D 2 or saddle. To linearize around C let U D u Then U 0 D u0 D u.3 D

U

V 0 D v 0 D v.u

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u V

1 and V D v

 v/ D .U C 1/ 3 U2



UV  v/ D .V C 2/ U C 1/

.U C 1/

2.  .V C 2/

 1 D 2U C U V:

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INSTRUCTOR’S SOLUTIONS MANUAL

The linearization thus has matrix A D and its eigenvalues are given by ˇ ˇ 1  0 D ˇˇ 2

REVIEW EXERCISES 18 (PAGE 1059)



1 2

1 0



4.

ˇ 1 ˇˇ D 2 C  C 2 ˇ

p so  D .1=2/ ˙ 2 i . Therefore C is a stable focus. Examining the signs of u0 and v 0 in various directions from C shows that the circulation of trajectories around the focus is counterclockwise. (b) Since u0 > 0 and v 0 D 0 between 0 and 3 on the u axis, and u0 < 0 and v 0 D 0 at points to the left of 0 and to the right of 3, The u-axis is a separatrix having alpha limit point at A and omega limit point at B. Since u0 D 0, v 0 < 0 for v > 0 and v 0 > 0 for v < 0, the v axis is a separatrix with alpha limit point at infinity and omega limit point at A. The curved blue trajectory in Figure 18.11(b) is a separatrix with alpha limit point at B and omega limit point at C . (c) Since B is the alpha limit point of the separatrix from B to C itsdirection at  B must be  that of the u 3 3 eigenvector of A D corresponding v 0 2 to the positive eigenvalue  D 2. Thus we must have 3u 3v D 2u and 2v D 2v, so v is arbitrary and 3v D 5u. The slope is 5=3.

5.

6.

7.

(d) Since C is a stable focus and is the only fixed point in the open first quadrant of the uv plane, all trajectories there must end up at C ; limt!1 u.t / D 1 and lim t!1 v.t / D 2:

dy D 2xy dx dy D 2x dx ) ln jyj D x 2 C C1 y y D C ex

2.

3.

8.

2

dy D e y sin x dx e y dy D sin x dx ) e y D y D ln.C cos x/

dy xCy D dx y x .x C y/ dx C .x y/ dy D 0 (exact)   2 y2 x C xy D0 d 2 2 x 2 C 2xy y 2 D C dy y C ex D dx x C ey .y C e x / dx C .x C e y / dy D 0 (exact) d .xy C e x C e y / D 0 xy C e x C e y D C d 2y dt 2 dp dt 1 p dy dt

D



dy dt

2

(let p D dy=dt ) dp D dt p2

D p2 ) D C1

t

1 DpD C1 t Z dt D yD C1 t

Review Exercises 18 (page 1059) 1.

dy x2 C y2 D (let y D xv.x/) dx 2xy 1 C v2 dv D vCx dx 2v 1 C v2 1 v2 dv D vD x dx 2v 2v 2v dv dx D v2 1 x 1 C 2 ln.v 1/ D ln C ln C D ln x x y2 C 2 2 1D ) y x D Cx x2 x

cos x C C

d 2y dy C5 C 2y D 0 dt 2 dt Aux: 2r 2 C 5r C 2 D 0 ) r D t=2

4y 00

C C2 e

1=2;

2

2t

4y 0 C 5y D 0

Aux: 4r 2

4r C 5 D 0

1 ˙i 2 y D C1 e x=2 cos x C C2 e x=2 sin x .2r

dy dy D x C 2y ) 2y D x dx dx   dy d .e 2x y/ D e 2x 2y D xe 2x dx dx Z x 2x 1 2x e 2x y D xe 2x dx D e e CC 2 4 x 1 C C e 2x yD 2 4

C1 j C C2

2

y D C1 e 9.

ln jt

10.

1/2 C 4 D 0 ) r D

2x 2 y 00 C y D 0 Aux: 2r.r 1/ C 1 D 0

1 2r C 1 D 0 ) r D .1 ˙ i /  2 y D C1 jxj1=2 cos 12 ln jxj C C2 jxj1=2 sin 2r 2

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1 2

 ln jxj 667

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REVIEW EXERCISES 18 (PAGE 1059)

11.

ADAMS and ESSEX: CALCULUS 9

dy d 2y t C 5y D 0 2 dt dt Aux: r.r 1/ r C 5 D 0

Thus A D 1, B D

t2

y D x2

2

.r 1/ C 4 D 0 ) r D 1 ˙ 2i y D C1 t cos.2 ln jt j/ C C2 t sin.2 ln jt j/

12.

d 3y d 2y dy C 8 C 16 D0 dt 3 dt 2 dt 3 2 Aux: r C 8r C 16r D 0

16.

r.r C 4/2 D 0 ) r D 0; 4; 4

y D C1 C C2 e 13.

4t

C C3 t e

4t

dy d 2y 5 C 6y D e x C e 3x dx 2 dx Aux: r 2 5r C 6 D 0 ) r D 2; 3. Complementary function: y D C1 e 2x C C2 e 3x . Particular solution: y D Ae x C Bxe 3x

C Be

5 C 6/

.6 C 9x

D 2Ae x C Be 3x :

5

15x C 6x/

17.

y Dx

yD

15.



2Axe 2x ;

1=2 and B D 2A D

19. 1. The

 1 2 x C x e 2x C C1 e 2x C C2 e 3x : 2

d 2y dy C2 C y D x2 dx 2 dx 2 Aux: r C 2r C 1 D 0 has solutions r D 1; 1. Complementary function: y D C1 e x C C2 xe x . Particular solution: try y D Ax 2 C Bx C C . Then x 2 D 2A C 2.2Ax C B/ C Ax 2 C Bx C C:

668

2Ax 3 D x 3 ;

x2 dy D 2 ; y.2/ D 1 dx y y 2 dy D x 2 dx

3

dy d 2y 5 C 6y D xe 2x 2 dx dx Same complementary function as in Exercise 13: C1 e 2x C C2 e 3x . For a particular solution we try y D .Ax 2 C Bx/e 2x . Substituting this into the given DE leads to

so that we need A D general solution is

:

1 3 C2 x C C1 x 2 C : 4 x

y3 D x3 C C 1D8CC ) C D

18.

B/e 2x

x

d 2y 2y D x 3 . dx 2 The corresponding homogeneous equation has auxiliary equation r.r 1/ 2 D 0, with roots r D 2 and r D 1, so the complementary function is y D C1 x 2 C C2 =x. A particular solution of the nonhomogeneous equation can have the form y D Ax 3 . Substituting this into the DE gives

yD

1 y D e x C xe 3x C C1 e 2x C C2 e 3x : 2

xe 2x D .2A

C C2 xe

so that A D 1=4. The general solution is

Thus A D 1=2 and B D 1. The general solution is

14.

x

x2

y 00 D Ae x C B.6 C 9x/e 3x 3x

4x C 6 C C1 e

6Ax 3

y 0 D Ae x C B.1 C 3x/e 3x

e x C e 3x D Ae x .1

4, C D 6. The general solution is

3

7

7 ) y D .x 3

y2 dy D 2 ; y.2/ D 1 dx x dy dx 1 1 D 2 ) D y2 x y x 1 1 1D CC ) C D 2 2   2x 1 1 1 D C yD x 2 xC2

7/1=3

C

dy xy , y.0/ D 1. Let y D xv.x/. Then D 2 dx x C y2 v dv D dx 1 C v2 dv v v3 x D v D dx 1 C v2 1 C v2 dx 1 C v2 dv D v3 x 1 ln jvj D ln jxj C ln C 2v 2 x2 1 D 2 D ln.C vx/2 D ln.C 2 y 2 / y2 v vCx

C 2 y 2 D ex y 2 D ex

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2 =y 2

2 =y 2

;

;

y.0/ D 1 ) C 2 D 1

or y D e x

2 =.2y 2 /

:

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INSTRUCTOR’S SOLUTIONS MANUAL

20.

dy C .cos x/y D 2 cos x; y./ D 1 dx     d dy C .cos x/y D 2 cos xe sin x e sin x y D e sin x dx dx e sin x y D 2e sin x C C

y D 2 C Ce 1 D 2 C Ce

yD2 21.

REVIEW EXERCISES 18 (PAGE 1059)

We require 1 D y.0/ D 1 C C1 and 2 D y 0 .0/ D 2 C 2C2 . Thus C1 D 0 and C2 D solution is y D e 2t 2 sin.2t /.

26.

sin x

0

) C D

1

sin x

e

y 00 C 3y 0 C 2y D 0, y.0/ D 1, y 0 .0/ D 2 Aux: r 2 C 3r C 2 D 0 ) r D 1; 2. y D Ae 0

y D Thus B D 00

x

Ae

C Be

x

2x

2Be

2x

)

1DACB

)

2D

A

3, A D 4. The solution is y D 4e

0

2

2B: x

3e

2x

.

22. y C 2y C .1 C  /y D 0, y.1/ D 0, y .1/ D  Aux: r 2 C 2r C 1 C  2 D 0 ) r D 1 ˙  i . y D Ae x cos.x/ C Be x sin.x/ y 0 D e x cos.x/. A C B/ C e x sin.x/. B Thus Ae 1 D 0 and .A B/e and B D e. The solution is y D

1

yD

0

y D

5x

5Ae

C Bxe 5x

5x/e

yD 27.

3x

/:

@M D .x C A/e x cos y sin y @y @N D e x cos y C B sin y C xe x cos y: @x These expressions are equal (and the DE is exact) if A D 1 and B D 1. If so, the left side of the DE is d.x; y/, where

We require e 2 D Ae 2 C Be 2 and 0 D 2Ae C 3Be. Thus A C B D 1 and 2A D 3B, so that A D 3 and B D 2. The solution is y D 3x 2 2x 2 ln x, valid for x > 0. d 2y C 4y D 8e 2t , y.0/ D 1, y 0 .0/ D 2 dt 2 Complementary function: y D C1 cos.2t / C C2 sin.2t /. Particular solution: y D Ae 2t , provided 4A C 4A D 8, that is, A D 1. Thus y D e 2t C C1 cos.2t / C C2 sin.2t /

y 0 D 2e 2t

1 2 C xe x=2 C .12e x=2 C 2e 7

Œ.x C A/e x sin y C cos y dx C xŒe x cos y C B sin y dy D 0 is M dx C N dy. We have

x 2 y 00 3xy 0 C 4y D 0, y.e/ D e 2 , y 0 .e/ D 0 Aux: r.r 1/ 3r C 4 D 0, or .r 2/2 D 0, so that r D 2; 2. y D Ax 2 C Bx 2 ln x y 0 D 2Ax C 2Bx ln x C Bx:

25.

:

:

We require e 5 D .A C B/e 5 and 0 D e 5 . 5A 4B/. Thus A C B D 1 and 5A D 4B, so that B D 5 and A D 4. The solution is y D 4e 5x C 5xe 5x . 24.

3x

which give C1 D 12=7, C2 D 2=7. Thus the IVP has solution

5x

C B.1

2 C xe x=2 C C1 e x=2 C C2 e

0 D y.0/ D 2 C C1 C C2 C1 3C2 ; 1 D y 0 .0/ D 1 C 2

D , so that A D 0 e 1 x sin.x/.

5x

2 and B D 1. The general

Now the initial conditions imply that A/:

23. y 00 C 10y 0 C 25y D 0, y.1/ D e 5 , y 0 .1/ D 0 Aux: r 2 C 10r C 25 D 0 ) r D 5; 5. y D Ae

dy d 2y C5 3y D 6 C 7e x=2 , y.0/ D 0, y 0 .0/ D 1 2 dx dx Aux: 2r 2 C 5r 3 D 0 ) r D 1=2; 3. Complementary function: y D C1 e x=2 C C2 e 3x . Particular solution: y D A C Bxe x=2  x y 0 D Be x=2 1 C 2  x y 00 D Be x=2 1 C : 4 We need   5x x Be x=2 2 C C 5 C 3x 3A D 6 C 7e x=2 : 2 2 2

This is satisfied if A D solution of the DE is

0

2. The

.x; y/ D xe x sin y C x cos y: The general solution is xe x sin y C x cos y D C . 28.

.x 2 C 3y 2 / dx C xy dy D 0. Multiply by x n :

x n .x 2 C 3y 2 / dx C x nC1 y dy D 0 is exact provided 6x n y D .n C 1/x n y, that is, provided n D 5. In this case the left side is d, where

2C1 sin.2t / C 2C2 cos.2t /:

.x; y/ D

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1 6 2 1 8 x y C x : 2 8

669

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REVIEW EXERCISES 18 (PAGE 1059)

ADAMS and ESSEX: CALCULUS 9

The general solution of the given DE is

Divide the first equation by x and subtract from the second equation to get

4x 6 y 2 C x 8 D C:

x sin xu20 D x sin x:

29. x 2 y 00 x.2 C x cot x/y 0 C .2 C x cot x/y D 0 If y D x, then y 0 D 1 and y 00 D 0, so the DE is clearly satisfied by y. To find a second, independent solution, try y D xv.x/. Then y 0 D v Cxv 0 , and y 00 D 2v 0 Cxv 00 . Substituting these expressions into the given DE, we obtain

Thus u20 D 1 and u2 D x. The first equation now gives u10 D cos x, so that u1 D sin x. The general solution of the DE is y D x sin x

2x 2 v 0 C x 3 v 00 .xv C x 2 v 0 /.2 C x cot x/ C xv.2 C x cot x/ D 0

x 3 v 00

x 3 v 0 cot x D 0;

31.

or, putting w D v 0 , w 0 D .cot x/w, that is, dw cos x dx D w sin x ln w D ln sin x C ln C2 v 0 D w D C2 sin x ) v D C1

2 00

0

C2 cos x:

3

30. x y x.2 C x cot x/y C .2 C x cot x/y D x sin x Look for a particular solution of the form y D xu1 .x/ C x cos xu2 .x/, where u10

670

Suppose y 0 D f .x; y/ and y.x0 / D y0 , where f .x; y/ is continuous on the whole xy-plane and satisfies jf .x; y/j  K there. By the Fundamental Theorem of Calculus, we have y.x/

A second solution of the DE is x cos x, and the general solution is y D C1 x C C2 x cos x:

xu10 C x cos xu20 D 0 C .cos x x sin x/u20 D x sin x:

x 2 cos x C C1 x C C2 x cos x:

y0 D y.x/ y.x0 / Z Z x y 0 .t / dt D D

x

x0

x0

  f t; y.t / dt:

Therefore, jy.x/

y0 j  Kjx

x0 j:

Thus y.x/ is bounded above and below by the lines y D y0 ˙ K.x x0 /, and cannot have a vertical asymptote anywhere. Remark: we don’t seem to have needed the continuity of @f =@y, only the continuity of f (to enable the use of the Fundamental Theorem).

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 18.2 (PAGE 1015)

CHAPTER 18-cosv9. ORDINARY DIFFERENTIAL EQUATIONS NOTE: ONLY SOLUTIONS FOR SECTIONS 18.2 AND 18.5 IN Calculus of Several Variables, 9th edition ARE GIVEN HERE. ALL OTHER SOLUTIONS ARE IN THE FILE FOR CHAPTER 18.

6.

e

) 7.

Section 18.2 Solving First-Order Equations (page 1015) 1.

2.

3.

y D 0 is a constant solution. Otherwise dy y D dx 2x dx dy D 2 y x 2 ln y D ln x C C1 ) y2 D C x

y 2 dy D x 2 dx or x 3

x

D xD

y D 1 and y D 1 are constant solutions, Otherwise dy dy D dx D 1 y2 ) dx 1 y2   1 1 1 C dy D dx 2 1Cy 1 y ˇ ˇ 1 ˇˇ 1 C y ˇˇ ln D x C C1 2 ˇ1 yˇ

8.

9.

dy dx Z dy 1 C y2 tan 1 y ) y

or

yD

C e 2x 1 C e 2x C 1

D 1 C y2 Z D dx

DxCC D tan.x C C /:

dy dy D 2 C ey ) D dt dt 2 C ey Z Z y e dy D dt 2e y C 1 1 ln.2e y C 1/ D t C C1 2  2e y C 1 D C2 e 2t ; or y D ln C e

2t

1 2



10. y D 0 and y D 1 are constant solutions. For the other solutions we have dy D y 2 .1 y/ dx Z Z dy D dx D x C K: y 2 .1 y/

y3 D C

4. y D 0 is a constant solution. Otherwise, dy D x2y2 dx Z Z dy D x 2 dx y2 1 1 1 D x3 C C y 3 3 3 ) yD : x3 C C

cos t C ln.cos t C C /:

1Cy D C e 2x 1 y

y D 1=3 is a constant solution. Otherwise 3y 1 dy D dx x Z Z dx dy D 3y 1 x 1 1 ln j3y 1j D ln jxj C ln C 3 3 3y 1 DC x3 1 ) y D .1 C C x 3 /: 3 x2 dy D 2 ) dx y 3 3 y x D C C1 ; 3 3

dx D e x sin t dt Z Z e x dx D sin t dt

Expand the left side in partial fractions: C A B 1 D C 2 C y 2 .1 y/ y y 1 y A.y y 2 / C B.1 y/ C Cy 2 D y 2 .1 y/ ( A C C D 0I ) A B D 0I ) A D B D C D 1: B D 1: Hence,

5.

Y D 0 is a constant solution. Otherwise dY dY D tY ) D t dt dt Y 2 t 2 ln Y D C C1 ; or Y D C e t =2 2

 Z  1 1 1 dy C D C dy y 2 .1 y/ y y2 1 y 1 D ln jyj ln j1 yj: y

Z

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671

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SECTION 18.2 (PAGE 1015)

Therefore,

11.

dy dx

1 x2 d dx y x2

ˇ ˇ ˇ y ˇ ˇ ln ˇˇ 1 yˇ

ADAMS and ESSEX: CALCULUS 9

16.

1 D x C K: y

then

Therefore, x

e 2e y D

2y 1 dy . Let C D 12. We have 2 dx x x Z 2 dx D 2 ln x D ln x 2 , then e  D x 2 , and D x

Hence, y D 17.

d 2 dy .x y/ D x 2 C 2xy dx  dx   2y 1 dy D1 C D x2 D x2 dx x x2 Z ) x2y D dx D x C C

13.

14.

yD

and

Hence, y D 15.

1 x e C Ce 2

x

.

 Z dy 1 dx D e x Cy Dx  D exp dx d x .e y/ D e x .y 0 C y/ D xe x dx Z

ex y D yDx

672

18.

xe x dx D xe x

1 C Ce

x

ex C C

x

e 2e e x dx

Let u D 2e x du D 2e x dx Z 1 1 x e u du D e 2e C C: D 2 2

1 C Ce 2

2e x

dy C 10y D 1; y dt Z  D 10 dt D 10t

.

1 10



D

2 10

dy C 3x 2 y D x 2 ; dx Z  D 3x 2 dx D x 3

y.0/ D 1

d x3 3 3 dy 3 .e y/ D e x C 3x 2 e x y D x 2 e x dx dx Z 1 3 3 3 e x y D x 2 e x dx D e x C C 3 1 2 y.0/ D 1 ) 1 D C C ) C D 3 3 2 x3 1 : yD C e 3 3

R dy Cy D e x . Let  D dx D x, then e  D e x , dx

  dy dy d x .e y/ D e x C ex y D ex C y D e 2x dx dx dx Z 1 ) e x y D e 2x dx D e 2x C C: 2

Z

dy d 10t .e y/ D e 10t C 10e 10t y D e 10t dt dt 1 10t e 10t y.t / D e CC 10  e e 2e 1 2 D CC ) C D y 10 D 10 ) 10 10 10 1 1 yD C e 1 10t : 10 10

C 1 C 2: x x

 Z dy 2 dx D e 2x C 2y D 3  D exp dx d 2x .e y/ D e 2x .y 0 C 2y/ D 3e 2x dx 3 3 e 2x y D e 2x C C ) y D C C e 2x 2 2 We have

R dy C 2e x y D e x . Let  D 2e x dx D 2e x , dx

d  2ex  x dy x C 2e x e 2e y e y D e 2e dx dx   dy x x D e 2e C 2e x y D e 2e e x : dx

2 y D x2 (linear) x Z  1 2  D exp dx D 2 x x dy 2 yD1 dx x 3 y D1 x2 D x C C; so y D x 3 C C x 2

)

We have

19.

x 2 y 0 C y D x 2 e 1=x ; y.1/ D 3e 1 y 0 C 2 y D e 1=x Zx 1 1 dx D D x2 x   d  1=x  1 e y D e 1=x y 0 C 2 y D 1 dx x Z 1=x e y D 1 dx D x C C

y.1/ D 3e ) 3 D 1 C C ) C D 2 y D .x C 2/e 1=x :

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INSTRUCTOR’S SOLUTIONS MANUAL

20.

y 0 C .cos x/y D 2xe sin x ; Z  D cos x dx D sin x

SECTION 18.2 (PAGE 1015)

y./ D 0

25.

dv x.1 C v/ D dx x.1 v/ 1Cv 1 C v2 dv D vD x 1 v Z 1 v Z dx 1 v dx dv D 1 C v2 x 1 1 tan v ln.1 C v 2 / D ln jxj C C1 2 1 x2 C y2 D ln jxj C C1 ln tan 1 .y=x/ 2 x2 2 tan 1 .y=x/ ln.x 2 C y 2 / D C:

2x dx D x 2 C C

y./ D 0 ) 0 D  2 C C ) C D

y D .x

21.

2

2

sin x

 /e

y.x/ D 2 C

Z

x

0

2

:

t dt y.t /

÷

y.0/ D 2

x dy D ; i.e. y dy D x dx dx y y2 D x2 C C

22 D 02 C C ÷ p y D 4 C x2: 22.

y.x/ D 1 C

Z

x

0

C D4

.y.t //2 dt 1 C t2

26. ÷

y.0/ D 1

23.

tan

y.x/ D 1 C

Z

1

x

1

÷

y.1/ D 1

y dy D ; for x > 0 dx x.x C 1/ dy dx dx dx D D y x.x C 1/ x xC1 x C ln C ln y D ln xC1 Cx ; ÷ 1 D C =2 yD xC1 2x : yD xC1

24.

y.x/ D 3 C dy D e y; dx ey D x C C

Z

x

e

y

dt

0

÷

27.

y.0/ D 3

i.e. e y dy D dx ÷

3 D y.0/ D ln C 3

y D ln.x C e /:

y D ln.x C C /

÷

C D e3

Let y D vx

vCx

x/:

y.t / dt t .t C 1/

dy xy D 2 dx x C 2y 2

vx 2 dv D dx .1 C 2v 2 /x 2 dv 2v 3 v x v D D dx 1 C 2v 2 1 C 2v 2 Z Z dx 1 C 2v 2 dv D 2 v3 x 1 C 2 ln jvj D 2 ln jxj C C1 2v 2 2 x C 2 ln jyj D C1 2y 2 x 2 4y 2 ln jyj D Cy 2 :

y2 dy ; i.e. dy=y 2 D dx=.1 C x 2 / D dx 1 C x2 1 D tan 1 x C C y 1D0CC ÷ C D 1

y D 1=.1

Let y D vx

vCx

d sin x .e y/ D e sin x .y 0 C .cos x/y/ D 2x dx Z

e sin x y D

xCy dy D dx x y

x 2 C xy C y 2 dy D dx x2

Let y D vx

x 2 .1 C v C v 2 / dv D vCx dx x2 Z Z dv dx D 1 C v2 x 1 tan v D ln jxj C C   y D tan ln jxj C C x   y D x tan ln jxj C C : Copyright © 2018 Pearson Canada Inc.

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673

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SECTION 18.2 (PAGE 1015)

28.

x 3 C 3xy 2 dy D dx 3x 2 y C y 3

ADAMS and ESSEX: CALCULUS 9

32.

Let y D vx

3

x .1 C 3v / dv D 3 dx x .3v C v 3 / 1 v4 1 C 3v 2 dv v D D x dx 3v C v 3 v.3 C v 2 / Z Z .3 C v 2 /v dv dx D Let u D v 2 1 v4 x du D 2v dv Z 1 3Cu du D ln jxj C C1 2 ˇ1 u2ˇ 3 ˇˇ u C 1 ˇˇ 1 ln ln j1 u2 j D ln jxj C C1 4 ˇu 1ˇ 4 ˇ 2 ˇ ˇ 4 ˇ ˇ y C x2 ˇ ˇ y 4 ˇˇ ˇ ln ˇ x 3 ln ˇˇ 2 ˇ x 4 ˇ D 4 ln jxj C C2 y x2 ˇ ˇ ˇ ˇ x 2 C y 2 3 ˇ 1 ˇ ˇ ln ˇ 2 ˇ D C2 2 4 4 ˇ x y x y ˇ ˇ ˇ 2 ˇ .x C y 2 /2 ˇ ˇ D C2 ln ˇˇ 2 .x y 2 /4 ˇ x 2 C y 2 D C.x 2 y 2 /2 :

29.

30.

31.

y  dy x D y C x cos2 (let y D vx) dx x dv D vx C x cos2 v xv C x 2 dx dv x D cos2 v dx dx sec2 v dv D x tan v D ln jxj C ln jC j y  tan D ln jC xj x y D xtan 1 .ln jC xj/: y dy D e y=x (let y=vx) dx x dv vCx Dv e v dx dx e v dv D x e v D ln jxj C ln jC j ˇ ˇ ˇC ˇ y=x e D ln ˇˇ ˇˇ x ˇ ˇ ˇC ˇ y D x ln ln ˇˇ ˇˇ : x 2

e x sin y C x 2 C y 2 D C:

33.

34.

35.

36.

e xy .1 C xy/ dx C x 2 e xy dy D 0   d xe xy D 0 ) xe xy D C:   y2 2y dy D 0 2x C 1 dx C x2 x   y2 d x2 C x C D0 x y2 D C: x2 C x C x Since a > b > 0 and k > 0,   ab e .b a/k t 1 lim x.t / D lim t!1 t!1 be .b a/k t a ab.0 1/ D b: D 0 a Since b > a > 0 and k > 0,

lim x.t / D lim

t!1

t!1

D lim

 ab e .b

a/k t

.b a/k t be  ab 1 e .a

b ae .a ab.1 0/ D a: D b 0 t!1

1



a

b/k t b/k t

37. The solution given, namely xD

ab e .b be .b

a/k t a/k t

1 a



;

is indeterminate (0/0) if a D b. If a D b the original differential equation becomes dx D k.a dt

x/2 ;

which is separable and yields the solution Z Z 1 dx D k dt D k t C C: D a x .a x/2 Since x.0/ D 0, we have C D

Solving for x, we obtain

xD

2

.xy C y/ dx C .x y C x/ dy D 0   1 2 2 x y C xy D 0 d 2 x 2 y 2 C 2xy D C:

674

d.e x sin y C x 2 C y 2 / D 0

2

vCx

.e x sin y C 2x/ dx C .e x cos y C 2y/ dy D 0

1 1 1 , so D kt C . a a x a

a2 k t : 1 C ak t

This solution also results from evaluating the limit of solution obtained for the case a ¤ b as b approaches a (using l’H^opital’s Rule, say).

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 18.2 (PAGE 1015)

38. Let x.t / be the number of kg of salt in the solution in the tank after t minutes. Thus, x.0/ D 50. Salt is coming into the tank at a rate of 10 g=L  12 L=min D 0:12 kg=min. Since the contents flow out at a rate of 10 L=min, the volume of the solution is increasing at 2 L=min and thus, at any time t , the volume of the solution is 1000 C 2t L. x.t / L. Hence, Therefore the concentration of salt is 1000 C 2t salt is being removed at a rate

40.

vCx

Therefore,

Z

yCx

i d h dx .500 C t /5 x D .500 C t /5 C 5.500 C t /4 x dt dy   5x dx C D .500 C t /5 dy 500 C t D 0:12.500 C t /5 : Z

42.

5

Since x.0/ D 50, we have C D 1:25  1015 and 5

:

After 40 min, there will be x D 0:02.540/ C .1:25  1015 /.540/

5

D 38:023 kg

of salt in the tank. dy 2x 39. We require . Thus D dx 1 C y2 Z

.1 C y 2 / dy D

dy D dx

y : x

y2 dy D 0:1y dt 1; 000; 000 dy 105 y y 2 D dt 106 Z Z dy dt D 105 y y 2 106  Z  1 1 1 t C 5 dy D 6 105 y 10 y 10 t C ln jyj ln j105 yj D 10 105 y D e C .t=10/ y 105 y D C .t=10/ : e C1

:

x D 0:02.500 C t / C .1:25  1015 /.500 C t /

or

The balance in the account after t years is y.t / and y.0/ D 1000. The balance must satisfy

.500 C t /5 dt D 0:02.500 C t /6 C C

) x D 0:02.500 C t / C C.500 C t /

dy D 0; dx

Curves that intersect these hyperbolas at right angles must dy x therefore satisfy D , or x dx D y dy, a separated dx y equation with solutions x 2 y 2 D C , which is also a family of rectangular hyperbolas. (Both families are degenerate at the origin for C D 0.)

Hence, .500 C t /5 x D 0:12

dv D 1 C 2v dx

41. The hyperbolas xy D C satisfy the differential equation

5 dt D 5 ln j500 C t j D ln.500 C t /5 for 500 C t t > 0. Then e  D .500 C t /5 , and Let  D

Let y D vx

dv x D1Cv dx Z Z dv dx D 1Cv x ln j1 C vj D ln jxj C C1 y 1 C D C x ) x C y D C x2 : x Since .1; 3/ lies on the curve, 4 D C . Thus the curve has equation x C y D 4x 2 .

x.t / 5x.t / kg=L  10 L=min D kg=min: 1000 C 2t 500 C t dx 5x D 0:12 dt 500 C t dx 5 C x D 0:12: dt 500 C t

2y dy D1C dx x

C 105

Since y.0/ D 1000, we have

Z

105 eC C 1

1000 D y.0/ D and

2x dx

yD

1 y C y 3 D x 2 C C: 3

105 99e

t=10

The balance after 1 year is

Since .2; 3/ lies on the curve, 12 D 4 C C . Thus C D 8 1 and y C y 3 x 2 D 8, or 3y C y 3 3x 2 D 24. 3

yD

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105 99e

)

1=10

C1

C1

C D ln 99;

:

 $1; 104:01:

675

lOMoARcPSD|6566483

SECTION 18.2 (PAGE 1015)

ADAMS and ESSEX: CALCULUS 9

As t ! 1, the balance can grow to lim y.t / D lim

t!1

105

t!1

e .4:60 0:1t/

C1

D

105 D $100; 000: 0C1

45.

For the account to grow to $50,000, t must satisfy

43. If  D x

100; 000 99e t=10 C 1 99e t=10 C 1 D 2 t D 10 ln 99  46 years:

x0 ,  D y

y0 , and

ax C by C c dy D ; dx ex C f y C g then d dy a. C x0 / C b. C y0 / C c D D d dx e. C x0 / C f . C y0 / C g a C b C .ax0 C by0 C c/ D e C f  C .ex0 C f y0 C g/ a C b D e C f 

46.

provided x0 and y0 are chosen such that ax0 C by0 C c D 0;

ex0 C f y0 C g D 0:

and

44. The system x0 C2y0 4 D 0, 2x0 y0 3 D 0 has solution x0 D 2, y0 D 1. Thus, if  D x 2 and  D y 1, where x C 2y dy D dx 2x y then

 C 2 d D d 2 

4 ; 3

Let  D v

47.

dv 1 C 2v D d 2 v 1 C 2v 1 C v2 dv D vD  d 2 v 2 v  Z  Z 2 v d dv D 1 C v2  1 2 1 ln.1 C v / D ln jj C C1 2 tan v 2  ln. 2 C 2 / D C: 4 tan 1  vC

x dy D 0

M D x 2 C 2y; N D x   1 @M @N 3 (indep. of y) D N @y @x x d 3 1 D dx )  D 3  x x   1 2y 1 C 3 dx dy D 0 x x x2   y d ln jxj D0 x2 y D C1 ln jxj x2 2 y D x ln jxj C C x 2 :

50; 000 D y.t / D ) )

.x 2 C 2y/ dx

 x2 C x ln x C x sin y dy D 0 y x2 M D xe x C x ln y C y; N D C x ln x C x sin y y x @N 2x @M D C 1; D C ln x C 1 C sin y @y y @x y     1 @M @N 1 1 x ln x sin y D D N @y @x N y x d 1 1 D dx )  D  x x    x y C ln x C sin y dy dx C e x C ln y C x y d .e x C x ln y C y ln x cos y/ D 0 e x C x ln y C y ln x cos y D C: .xe x C x ln y C y/ dx C

If .y/M.x; y/ dx C .y/N.x; y/ dy is exact, then   @  @  .y/M.x; y/ D .y/N.x; y/ @y @x @N @M D 0 .y/M C  @y @x   0 1 @N @M D :  M @x @y Thus M and N must be such that 1 M

Hence the solution of the original equation is 4 tan

676

1

y x

1 2

 ln .x

2/2 C .y

 1/2 D C:



depends only on y.

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@N @x

@M @y



lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

48.

SECTION 18.5 (PAGE 1038)

2y 2 .x C y 2 / dx C xy.x C 6y 2 / dy D 0 2

4

2

Thus, an integrating factor is given by

3

.2xy C 2y /.y/ dx C .x y C 6xy /.y/ dy D 0 @M D .4xy C 8y 3 /.y/ C .2xy 2 C 2y 4 /0 .y/ @y @N D .2xy C 6y 3 /.y/: @x For exactness we require .2xy 2 C 2y 4 /0 .y/ D Œ.2xy C 6y 3 / .4xy C 8y 3 /.y/ 3

0

0 .t / D .t /

   cos x sin x y 1 C 2 dx C dy D 0 y x y2 x   sin x y D0 d y x sin x y D C: y x

.2xy C 2y /.y/ 1 y .y/ D .y/ ) .y/ D y .2xy C 2y 3 / dx C .x 2 C 6xy 2 / dy D 0 )

x 2 y C 2xy 3 D C:

.2x C y 3 e y / dy D 0. @N @M D 1, and D Here M D y, N D 2x y 3 e y , @y @x Thus

49. Consider y dx

Section 18.5 Linear Differential Equations with Constant Coefficients (page 1038) y 00 C 7y 0 C 10y D 0

1.

r 2 C 7r C 10 D 0 .r C 5/.r C 2/ D 0

auxiliary eqn

y D Ae y 00

2. auxiliary eqn

r

50. If .xy/ is an integrating factor for M dx C N dy D 0, then @ @ .M / D .N /; or @y @x @N @M D y0 .xy/N C .xy/ : x0 .xy/M C .xy/ @y @x Thus M and N will have to be such that the right-hand side of the equation   1 @N @M 0 .xy/ D .xy/ xM yN @x @y

51.

depends only on the product xy.     y2 x sin x For x cos x C C y dy we have dx x y x sin x y2 ; N D y M D x cos x C x y @M 2y @N sin x x cos x D ; D @y x @x y y   @M sin x x cos x 2y @N D C C @x @y y y x xM yN D x 2 cos x C y 2 C x sin x C y 2   @N @M 1 1 : D xM yN @x @y xy

y 2 D C xy.

The solution is x sin x 2.

0

 3 1 D ) D 3  y y   2x 1 y dx C e dy D 0 y2 y3   x d ey D 0 y2 x e y D C; or x y 2 e y D Cy 2 : y2

1 : t

.t / D



0

d.x 2 y C 2xy 3 / D 0

)

We multiply the original equation by 1=.xy/ to make it exact:

3

y.2xy C 2y / .y/ D

1 t

5t

2y 0

2

t

3D0

C Be 3t

y 00 C 2y 0 D 0

3.

r 2 C 2r D 0

auxiliary eqn

y D A C Be

4.

00

4y

2

4r

4y 4r

0

Thus; r1 D

r2 D

3 ; 2

3/ D 0

and y D Ae

y 00 C 8y 0 C 16y D 0 r 2 C 8r C 16 D 0

auxiliary eqn

y D Ae

y 00

) r D 0;

4t

5; 2

1; r D 3

2

2t

3 D 0 ) .2r C 1/.2r

5.

6.

) rD

3y D 0 1 ; 2

) rD

2t

3y D 0

2r

y D Ae

C Be

C Bt e

.1=2/t

) rD

C Be .3=2/t : 4;

4

4t

2y 0 C y D 0

r 2 2r C 1 D 0 ) .r 1/2 D 0 Thus; r D 1; 1; and y D Ae t C Bt e t : y 00

7.

6y 0 C 10y D 0

r2

auxiliary eqn

6r C 10 D 0

) r D3˙i

y D Ae 3t cos t C Be 3t sin t 8.

9y 00 C 6y 0 C y D 0

9r 2 C 6r C 1 D 0 ) .3r C 1/2 D 0

Thus; r D

1 3;

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1 3;

and y D Ae

.1=3/t

C Bt e

.1=3/t

:

677

lOMoARcPSD|6566483

SECTION 18.5 (PAGE 1038)

ADAMS and ESSEX: CALCULUS 9

y 00 C 2y 0 C 5y D 0

9.

16.

auxiliary eqn r 2 C 2r C 5 D 0 ) r D 1 ˙ 2i y D Ae t cos 2t C Be t sin 2t 10. For y 00 4y 0 C 5y D 0 the auxiliary equation is r 2 4r C 5 D 0, which has roots r D 2 ˙ i . Thus, the general solution of the DE is y D Ae 2t cos t C Be 2t sin t . 11.

For y 00 C 2y 0 C 3y D 0 the auxiliary equation isp r 2 C 2r C 3 D 0, which has solutions r D 1 ˙ 2i . Thus the general solution of the givenpequation is p y D Ae t cos. 2t / C Be t sin. 2t /.

12. Given that y 00 C y 0 C y D 0, hence r 2 C r C 1 D 0. Since a D 1, b D 1 and c D 1, the discriminant is D D b 2 4ac D 3 < 0 and .b=2a/ D 21 and p general solution is p ! D 3=2. Thus, the   p  3 3 .1=2/t t C Be .1=2/t sin t . y D Ae cos 2 2 8 00 < 2y C 5y 0 3y D 0 13. y.0/ D 1 : 0 y .0/ D 0 The DE has auxiliary equation 2r 2 C 5y 3 D 0, with roots r D 12 and r D 3. Thus y D Ae t=2 C Be 3t . A Now 1 D y.0/ D A C B, and 0 D y 0 .0/ D 3B. 2 Thus B D 1=7 and A D 6=7. The solution is 6 1 y D e t=2 C e 3t . 7 7 14.

00

Given that y C 10y C 25y D 0, hence r 2 C 10r C 25 D 0 ) .r C 5/2 D 0 ) r D y0 D

5t

5e

C Bt e

5t

0 D y.1/ D Ae

2 D y 0 .1/ D

5t

:

2t

cos t C Be

y D . 2Ae

5

5e

C Be

Given that a > 0, b > 0 and c > 0: Case 1: If D D b 2 4ac > 0 then the two roots are p b ˙ b 2 4ac : r1;2 D 2a Since b2 p ˙ b2 p b ˙ b2

5

.A C B/ C Be

2t

C Be

2t 2t

5

.Ae

2t

4ac < b 4ac < 0

therefore r1 and r2 are negative. The general solution is y.t / D Ae r1 t C Be r2 t :

y.t / D Ae r1 t C Bt e r2 t :

;

sin t

/ cos t

4ac < b 2

t!1

5

Now 2 D y.0/ D A ) A D 2, and 2 D y 0 .0/ D 2A C B ) B D 6. Therefore y D e 2t .2 cos t C 6 sin t /.

678

17.

Case 2: If D D b 2 4ac D 0 then the two equal roots r1 D r2 D b=.2a/ are negative. The general solution is

we have A D 2e 5 and B D 2e 5 . Thus, y D 2e 5 e 5t C 2t e 5 e 5t D 2.t 1/e 5.t 1/ . 8 00 < y C 4y 0 C 5y D 0 y.0/ D 2 : 0 y .0/ D 0 The auxiliary equation for the DE is r 2 C 4r C 5 D 0, which has roots r D 2 ˙ i . Thus 0

which is, along with e t , a solution of the CASE II DE y 00 2y 0 C y D 0.

If t ! 1, then e r1 t ! 0 and e r2 t ! 0. Thus, lim y.t / D 0.

Since

y D Ae

!0

5. Thus,

5t

.A C Bt / C Be

e .1C/t e t !0  e tCh e t D t lim h h!0   d t e D t et Dt dt

lim y .t / D lim

0

y D Ae

15.

The auxiliary equation r 2 .2 C /r C .1 C / factors to .r 1 /.r 1/ D 0 and so has roots r D 1 C  and r D 1. Thus the DE y 00 .2 C /y 0 C .1 C /y D 0 has general solution y D Ae .1C/t C Be t . The function e .1C/t e t is of this form with A D B D 1=. y .t / D  We have, substituting  D h=t ,

C 2Be

2t

/ sin t:

If t ! 1, then e r1 t ! 0 and e r2 t ! 0 at a faster rate than Bt ! 1. Thus, lim y.t / D 0. t!1

Case 3: If D D b 2 y D Ae

4ac < 0 then the general solution is

.b=2a/t

cos.!t / C Be

.b=2a/t

sin.!t /

p 4ac b 2 . If t ! 1, then the amplitude of 2a both terms Ae .b=2a/t ! 0 and Be .b=2a/t ! 0. Thus, lim y.t / D 0. where ! D t!1

18. The auxiliary equation ar 2 C br C c D 0 has roots r1 D

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b

p 2a

D

;

r2 D

p bC D ; 2a

lOMoARcPSD|6566483

INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 18.5 (PAGE 1038)

where D D p b 2 4ac. Note that a.r2 r1 / D D D .2ar1 C b/. If y D e r1 t u, then y 0 D e r1 t .u0 Cr1 u/, and y 00 D e r1 t .u00 C2r1 u0 Cr12 u/. Substituting these expressions into the DE ay 00 C by 0 C cy D 0, and simplifying, we obtain e r1 t .au00 C 2ar1 u0 C bu0 / D 0;

25.

r2

v D .r2

26.

uD

Z

C e .r2

r1 /t

xy 0

27. r1 /t

dt D Be .r2

: Hence

r1 /t

C A;

19. y 000 4y 00 C 3y 0 D 0 Auxiliary: r 3 4r 2 C 3r D 0 r.r 1/.r 3/ D 0 ) r D 0; 1; 3 General solution: y D C1 C C2 e t C C3 e 3t .

28.

29.

20. y .4/ 2y 00 C y D 0 Auxiliary: r 4 2r 2 C 1 D 0

30.

y .4/ C 2y 00 C y D 0 Auxiliary: r 4 C 2r 2 C 1 D 0

31.

.r 2 1/2 D 0 ) r D 1; 1; 1; 1 General solution: y D C1 e t C C2 t e t C C3 e t C C4 t e t .

22. y .4/ C 4y .3/ C 6y 00 C 4y 0 C y D 0 Auxiliary: r 4 C 4r 3 C 6r 2 C 4r C 1 D 0 4

.r C 1/ D 0 ) r D 1; 1; 1; 1 General solution: y D e t .C1 C C2 t C C3 t 2 C C4 t 3 /.

23. If y D e 2t , then y 000 2y 0 4y D e 2t .8 4 4/ D 0. The auxiliary equation for the DE is r 3 2r 4 D 0, for which we already know that r D 2 is a root. Dividing the left side by r 2, we obtain the quotient r 2 C 2r C 2. Hence the other two auxiliary roots are 1 ˙ i . General solution: y D C1 e 2t C C2 e t cos t C C3 e t sin t . Aux. eqn: .r 2

r

2/2 .r 2

4/2 D 0

Ce

2t

C Bx 3 :

) r D ˙1

Consider x 2 y 00 xy 0 C 5y D 0. Since a D 1, b D 1, and c D 5, therefore .b a/2 < 4ac. Then k D .a b/=2a D 1 and ! 2 D 4. Thus, the general solution is y D Ax cos.2 ln x/ C Bx sin.2 ln x/. x 2 y 00 C xy 0 D 0 aux: r.r 1/ C r D 0 Thus y D A C B ln x:

) r D 0; 0:

Given that x 2 y 00 C xy 0 C y D 0. Since a D 1, b D 1, c D 1 therefore .b a/2 < 4ac. Then k D .a b/=2a D 0 and ! 2 D 1. Thus, the general solution is y D A cos.ln x/ C B sin.ln x/. x 3 y 000 C xy 0 y D 0. Trying y D x r leads to the auxiliary equation r.r

1/.r

3

2

r

.r

2/ C r

3r C 3r

1D0

1D0

1/3 D 0 ) r D 1; 1; 1:

Thus y D x is a solution. To find the general solution, try y D xv.x/. Then y 0 D xv 0 C v; Now x 3 y 000 C xy 0

y 00 D xv 00 C 2v 0 ;

y 000 D xv 000 C 3v 00 :

y D x 4 v 000 C 3x 3 v 00 C x 2 v 0 C xv 2

2 000

00

xv

0

D x .x v C 3xv C v /; and y is a solution of the given equation if v 0 D w is a solution of x 2 w 00 C 3xw 0 C w D 0. This equation has auxiliary equation r.r 1/ C 3r C 1 D 0, that is .r C 1/2 D 0, so its solutions are

.r C 1/2 .r 2/2 .r 2/2 .r C 2/2 D 0 r D 2; 2; 2; 2; 1; 1; 2; 2: The general solution is y D e 2t .C1 C C2 t C C3 t 2 C C4 t 3 / C e t .C5 C C6 t /

1

x 2 y 00 C xy 0 y D 0 aux: r.r 1/ C r 1 D 0 B y D Ax C : x

.r 2 C 1/2 D 0 ) r D i; i; i; i General solution: y D C1 cos t C C2 sin t C C3 t cos t C C4 t sin t .

24.

3y D 0

r.r 1/ r 3 D 0 ) r 2 2r 3 D 0 ).r 3/.r C 1/ D 0 ) r1 D 1 and r2 D 3

and y D e r1 t u D Ae r1 t C Be r2 t .

21.

x 2 y 00

Thus; y D Ax

r1 /v;

which has general solution v D C e .r2

2r C 1 D 0

.r 1/2 D 0; r D 1; 1: Thus y D Ax C Bx ln x:

or, more simply, u00 .r2 r1 /u0 D 0. Putting v D u0 reduces this equation to first order: 0

x 2 y 00 xy 0 C y D 0 aux: r.r 1/ r C 1 D 0

2C3 ln x C2 C x x v D C1 C C2 ln x C C3 .ln x/2 : v0 D w D

The general solution of the given equation is, therefore,

.C7 C C8 t /:

y D C1 x C C2 x ln x C C3 x.ln x/2 :

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679

lOMoARcPSD|6566483

SECTION 18.5 (PAGE 1038)

32. Since

ADAMS and ESSEX: CALCULUS 9

dx D e t D x, we have dt

Since a sum of squares cannot vanish unless each term vanishes, g.t / D 0 for all t .

dz dy dx dy D Dx ; dt dx dt dx dx dy d 2 y dx d 2z D Cx 2 2 dt dt dx dx dt 2 dy 2 d y : Cx Dx dx dx 2

37. If f .t / is any solution of .†/, let g.t / D f .t / A cos !t B sin !t where A D f .0/ and B! D f 0 .0/. Then g is also solution of .†/. Also g.0/ D f .0/ A D 0 and g 0 .0/ D f 0 .0/ B! D 0. Thus, g.t / D 0 for all t by Exercise 24, and therefore f .x/ D A cos !t C B sin !t . Thus, it is proved that every solution of .†/ is of this form.

Accordingly, z D z.t / satisfies dz d 2z C .b a/ C cz dt 2 dt 2 d y dy dy Dax 2 C ax C .b a/x C cy D 0: dx 2 dx dx a

38.

4ac b 2 b which is and ! 2 D 2a 4a2 kt positive for Case III. If y D e u, then We are given that k D

  y 0 D e k t u0 C ku   y 00 D e k t u00 C 2ku0 C k 2 u :

t

33. By the previous exercise, z.t / D y.e / D y.x/ must satisfy the constant coefficient equation d 2z dt 2

2

dz C 2z D 0: dt

Substituting into ay 00 C by 0 C cy D 0 leads to

The auxiliary equation for this equation is r 2 which has roots r D 1 ˙ i . Thus

  0 D e k t au00 C .2ka C b/u0 C .ak 2 C bk C c/u   D e k t au00 C 0 C ..b 2 =.4a/ .b 2 =.2a/ C c/u   D a e k t u00 C ! 2 u :

2r C 2 D 0,

z D C1 e t cos t C C2 e t sin t: Since t D ln x, the given Euler equation has solution

Thus u satisfies u00 C ! 2 u D 0, which has general solution

y D C1 x cos.ln x/ C C2 x sin.ln x/:

u D A cos.!t / C B sin.!t /

34. If y D A cos !t C B sin !t then y 00 C ! 2 y D

A! 2 cos !t

by the previous problem. Therefore ay 00 C by 0 C cy D 0 has general solution

B! 2 sin !t

C ! 2 .A cos !t C B sin !t / D 0

y D Ae k t cos.!t / C Be k t sin.!t /:

for all t . So y is a solution of (†). 35. If f .t / is any solution of .†/ then f 00 .t / D all t . Thus,

! 2 f .t / for

2  2 i d h 2 ! f .t / C f 0 .t / dt D 2! 2 f .t /f 0 .t / C 2f 0 .t /f 00 .t / D 2! 2 f .t /f 0 .t /

39.

2! 2 f .t /f 0 .t / D 0

 2  2 for all t . Thus, ! 2 f .t / C f 0 .t / is constant. (This can be interpreted as a conservation of energy statement.) 36. If g.t / satisfies .†/ and also g.0/ D g 0 .0/ D 0, then by Exercise 20,  2  2 ! g.t / C g 0 .t /  2  2 D ! 2 g.0/ C g 0 .0/ D 0: 2

680

40.

8 00 < y C 100y D 0 y.0/ D 0 : 0 y .0/ D 3 y D A cos.10t / C B sin.10t / A D y.0/ D 0; 10B D y 0 .0/ D 3 3 yD sin.10t / 10 Circular frequency = 10, freq = 5=, period = =5, amplitude = 3=10 Because y 00 C 4y D 0, therefore y D A cos 2t C B sin 2t . Now y.0/ D 2 ) A D 2;

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y 0 .0/ D

5)B D

5 2:

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INSTRUCTOR’S SOLUTIONS MANUAL

SECTION 18.5 (PAGE 1038)

Thus, y D 2 cos 2t 25 sin 2t . circular frequency = ! D 2, frequency = 1 ! D  0:318 2  2 D   3:14 period = !q amplitude = .2/2 C . 52 /2 ' 3:20

 41. y D A cos !.t

  c/ C B sin !.t

therefore, y D A cos 20 t C B sin 20 t and y.0/ D

1 2 1 y 0 .0/ D 2 ) B D D : 20 10

 c/

(easy tocalculate y 00 C ! 2 y D 0)  y D A cos.!t / cos.!c/ C sin.!t / sin.!c/   C B sin.!t / cos.!c/ cos.!t / sin.!c/   D A cos.!c/ B sin.!c/ cos !t   C A sin.!c/ C B cos.!c/ sin !t

45.

D A cos !t C B sin !t where A D A cos.!c/ B sin.!c/ and B D A sin.!c/ C B cos.!c/

42. For y 00 C y D 0, we have y D A sin t C B cos t . Since, y.2/ D 3 D A sin 2 C B cos 2 y 0 .2/ D 4 D A cos 2 B sin 2;

46.

where A1 D A cos !t0 B sin !t0 and B1 D A sin !t0 C B cos !t0 . Under the conditions of this problem we know that e k t cos !t and e k t sin !t are independent solutions of ay 00 C by 0 C cy D 0, so our function y must also be a solution, and, since it involves two arbitrary constants, it is a general solution.

4 cos 2/ sin t C .4 sin 2 C 3 cos 2/ cos t 2/ 4 sin.t 2/:

47.  a/

44. From Example 9, the spring constant is k D 9  104 gm=sec2 . For a frequency of 10 Hz (i.e., a circular frequency ! D 20 rad=sec.), a mass m satisfying p k=m D 20 should be used. So, 9  104 k D D 22:8 gm: mD 400 2 400 2

8 < y 00 C 400 2 y D 0 y.0/ D 1 : 0 y .0/ D 2

t0 /

D e k t ŒA1 cos !t C B1 sin !t ;

Thus,

The motion is determined by

t0 /B sin !.t

D e k t ŒA cos !t cos !t0 C A sin !t sin !t0 C B sin !t cos !t0 B cos !t sin !t0 

A D 3 sin 2 4 cos 2 B D 4 sin 2 C 3 cos 2:

8 < y 00 C ! 2 y D 0 43. y.a/ D A : 0 y .a/ D B   B  y D A cos !.t a/ C sin !.t !

1 Thus, y D cos 20 t C sin 20 t , with y in cm and t 10 in r second, gives the displacement at time t . The amplitude 1 2 /  1:0005 cm. is . 1/2 C . 10 ! k Frequency D , !2 D (k = spring const, m = mass) 2 m Since the spring does not change, ! 2 m D k (constant) For m D 400 gm, ! D 2.24/ (frequency = 24 Hz) 4 2 .24/2 .400/ If m D 900 gm, then ! 2 D 900 2  24  2 D 32. so ! D 3 32 D 16 Hz Thus frequency = 2 4 2 .24/2 400 For m D 100 gm, ! D 100 ! D 48 Hz. so ! D 96 and frequency = 2 Using the addition identities for cosine and sine, y D e k t ŒA cos !.t

therefore

y D .3 sin 2 D 3 cos.t

1)AD

Expanding the hyperbolic functions in terms of exponentials, y D e k t ŒA cosh !.t t0 /B sinh !.t  A !.t t0 / A !.t t0 / D ek t e C e 2 2  B !.t t0 / B !.t t0 / e C e 2 2 D A1 e .kC!/t C B1 e .k

t0 /

!/t

where A1 D .A=2/e !t0 C .B=2/e !t0 and B1 D .A=2/e !t0 .B=2/e !t0 . Under the conditions of this problem we know that Rr D k ˙ ! are the two real roots of the auxiliary equation ar 2 C br C c D 0, so e .k˙!/t are independent solutions of ay 00 C by 0 C cy D 0, and our function y must also be a solution. Since it involves two arbitrary constants, it is a general solution.

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SECTION 18.5 (PAGE 1038)

ADAMS and ESSEX: CALCULUS 9

8 00 < y C 2y 0 C 5y D 0 48. y.3/ D 2 : 0 y .3/ D 0

This IVP for the equation of simple harmonic motion has solution

The DE has auxiliary equation r 2 C 2r C 5 D 0 with roots r D 1 ˙ 2i . By the second previous problem, a general solution can be expressed in the form y D e t ŒA cos 2.t 3/ C B sin 2.t 3/ for which y0 D

 1  c u.x/ 2 k   c D 2 c .c k 2 a/ cos.kx/ C kb sin.kx/ k c b D 2 .1 cos.kx/ C a cos.kx/ C sin.kx/: k k

y.x/ D

The initial conditions give 3

0

0 D y .3/ D

Thus A D 2e 3 and B D solution

A 3

e

.A C 2B/

A=2 D

y D e 3 t Œ2 cos 2.t

3/

e 3 . The IVP has

sin 2.t

3/:

8 00 < y C 4y 0 C 3y D 0 49. y.3/ D 1 : 0 y .3/ D 0

The DE has auxiliary equation r 2 C 4r C 3 D 0 with roots r D 2 C 1 D 1 and r D 2 1 D 3 (i.e. k ˙ !, where k D 2 and ! D 1). By the second previous problem, a general solution can be expressed in the form y D e 2t ŒA cosh.t 3/ C B sinh.t 3/ for which y0 D

2e

2t

Ce

3/ C B sinh.t

ŒA cosh.t

2t

3/

3/ C B cosh.t

ŒA sinh.t

3/:

The initial conditions give 1 D y.3/ D e 0

0 D y .3/ D

6

e

A 6

. 2A C B/

Thus A D e 6 and B D 2A D 2e 6 . The IVP has solution y D e6 50. Let u.x/ D c Also u0 .x/ D u00 .x/ D

682

2t

2

Œcosh.t

kb sin.kx/

so that

e t ŒA cos 2.t 3/ C B sin 2.t 3/ C e t Œ 2A sin 2.t 3/ C 2B cos 2.t 3/:

2 D y.3/ D e

k 2 a/ cos.kx/

u.x/ D .c

3/ C 2 sinh.t

3/:

51.

Since x 0 .0/ D 0 and x.0/ D 1 > 1=5, the motion will be governed by x 00 D x C .1=5/ until such time t > 0 when x 0 .t / D 0 again. Let u D x .1=5/. Then u00 D x 00 D .x 1=5/ D u, u.0/ D 4=5, and u0 .0/ D x 0 .0/ D 0. This simple harmonic motion initial-value problem has solution u.t / D .4=5/ cos t . Thus x.t / D .4=5/ cos t C .1=4/ and x 0 .t / D u0 .t / D .4=5/ sin t . These formulas remain valid until t D  when x 0 .t / becomes 0 again. Note that x./ D .4=5/ C .1=5/ D .3=5/. Since x./ < .1=5/, the motion for t >  will be governed by x 00 D x .1=5/ until such time t >  when x 0 .t / D 0 again. Let v D x C .1=5/. Then v 00 D x 00 D .x C 1=5/ D v, v./ D .3=5/ C .1=5/ D .2=5/, and v 0 ./ D x 0 ./ D 0. Thius initial-value problem has solution v.t / D .2=5/ cos.t / D .2=5/ cos t , so that x.t / D .2=5/ cos t .1=5/ and x 0 .t / D .2=5/ sin t . These formulas remain valid for t   until t D 2 when x 0 becomes 0 again. We have x.2/ D .2=5/ .1=5/ D 1=5 and x 0 .2/ D 0. The conditions for stopping the motion are met at t D 2; the mass remains at rest thereafter. Thus

2

k y.x/. Then u.0/ D c k a. k 2 y 0 .x/, so u0 .0/ D k 2 b. We have   k 2 y 00 .x/ D k 2 c k 2 y.x/ D k 2 u.x/

84 1 < 5 cos t C 5 2 1 x.t / D 5 cos t 5 :1

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5

if 0  t   if  < t  2 if t > 2

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INSTRUCTOR’S SOLUTIONS MANUAL

APPENDIX I (PAGE A-10)

APPENDICES

1.

Appendix I

Complex Numbers (page A-10)

zD

Re.z/ D

5 C 2i;

zD zD

3  and Arg .w/ D , then 4 2  5 3 C D , so arg .zw/ D 4 2 4 5 3 Arg .zw/ D 2 D . 4 4  5 and Arg .w/ D , then 17. If Arg .z/ D 6 4  13 5 D , so arg .z=w/ D 6 4 12 13 11 Arg .z=w/ D C 2 D . 12 12 18. jzj D 2; arg .z/ D  ) z D 2.cos  C i sin / D 16.

5;

5 C 2i

Im.z/ D 2 y z-plane

6 x zD4

i

19. zD

i 20.

Fig. APX I-1 i;

Re.z/ D 4;

Im.z/ D

1

3. z D

 i;

Re.z/ D 0;

Im.z/ D



4. z D

6;

2. z D 4

5.

6; Im.z/ D 0 p jzj D 2; Arg .z/ D 3=4

zD

1 C i; p z D 2 .cos.3=4/ C i sin.3=4//

6.

z D 2; jzj D 2; Arg .z/ D  z D 2.cos  C i sin /

7.

z D 3i; jzj D 3; Arg .z/ D =2 z D 3.cos.=2/ C i sin.=2//

8.

9.

10.

21.

Re.z/ D

22. 23.

24.

z D 5i; jzj D 5; Arg .z/ D =2 z D 5.cos. =2/ C i sin. =2// p z D 1 C 2i; jzj D 5;  D Arg .z/ D tan 1 2 p z D 5.cos  C i sin  / p z D 2 C i; jzj D 5;  D Arg .z/ D  tan p z D 5.cos  C i sin  /  D Arg .z/ D

 C tan

1

z D 3 4i; jzj D 5; z D 5.cos  C i sin  /

12.

z D 3 4i; jzj D 5;  D Arg .z/ D tan 1 .4=3/ z D 5.cos  C i sin  / p z D 3 i; jzj D 2; Arg .z/ D =6 z D 2.cos. =6/ C i sin. =6// p p zD 3 3i; jzj D 2 3; Arg .z/ D 2=3 p z D 2 3.cos. 2=3/ C i sin. 2=3//

13.

14.

15.

4 4 C 3i sin 5 5 4 Arg .z/ D 5

.4=3/

jzj D 5;  D arg .z/ D  ) sin  D 3=5; cos  D 4=5 z D 4 C 3i   3 3 3 ) z D cos C i sin jzj D 1; arg .z/ D 4 4 4 1 1 ) zD p Cp i 2 2     jzj D ; arg .z/ D ) z D  cos C i sin 6 6 6 p   3 C i ) zD 2 2 jzj D 0 ) z D 0 for any value of arg .z/ 1  1   jzj D ; arg .z/ D ) zD i sin cos 2 3 2 3 3 p 3 1 i ) zD 4 4 5 C 3i D 5

3i

3

5i D

26.

4i D

4i

27.

2

28.

jzj D 2 represents all points on the circle of radius 2 centred at the origin.

29.

jzj  2 represents all points in the closed disk of radius 2 centred at the origin.

30.

jz 2i j  3 represents all points in the closed disk of radius 3 centred at the point 2i .

31.

jz 3 C 4i j  5 represents all points in the closed disk of radius 5 centred at the point 3 4i .

32.

arg .z/ D =3 represents all points on the ray from the origin in the first quadrant, making angle 60ı with the positive direction of the real axis.

33.

  arg .z/  7=4 represents the closed wedge-shaped region in the third and fourth quadrants bounded by the ray from the origin to 1 on the real axis and the ray from the origin making angle 45ı with the positive direction of the real axis.

34.

.2 C 5i / C .3

z D 3 cos jzj D 3;

2

25.

.1=2/

1

11.

If Arg .z/ D

3 C 5i

i D2Ci

i / D 5 C 4i

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683

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APPENDIX I (PAGE A-10)

35. i

.3

2i / C .7

3i / D

i / D 16

37. .1 C i /.2

3i / D 2 C 2i

38.

.a C bi /.2a

3 C 7 C i C 2i

i 2 D 17

36. .4 C i /.4

ADAMS and ESSEX: CALCULUS 9

3i

3i 2 D 5

3i D 4 i

bi / D .a C bi /.2a C bi / D 2a

3

2

49.

2

b) z D 2=z can be rewritten jzj2 D zz D 2, which has no solutions since the square of jzj is nonnegative for all complex z.

2

b C 3abi

3

39. .2 C i / D 8 C 12i C 6i C i D 2 C 11i 40. 41. 42. 43.

2 i .2 D 2Ci 4

3 4i i /2 D i2 5

50.

1 C 7i .1 C 3i /.2 C i / 1 C 3i D D 2 i 4 i2 5 1Ci 1Ci .1 C i /. 3 2i / D D D i.2 C 3i / 3 C 2i 9C4

a) z D 2=z can be rewritten jzj2 D zz D 2, so isp satisfied by all numbers z on the circle of radius 2 centred at the origin.

51. 1 5i 13

p If z p D w Dp 1, then zw D 1, so zw D 1.pBut if we use p z D 1 D ip and the same value for w, then p z w D i 2 D 1 ¤ zw. The three cube roots of 1 D cos  C i sin  are of the form cos  Ci sin  where  D =3,  D , and  D 5=3. Thus they are

.1 C 2i /.2 3i / 8Ci D D1 .2 i /.3 C 2i / 8Ci

p 1 3 Ci ; 2 2

44. If z D x C yi and w D u C vi , where x, y, u, and v are real, then z C w D x C u C .y C v/i D x C u .y C v/i D x

52. yi C u

vi D z C w:

45. Using the fact that jzwj D jzjjwj, we have z w

46.

47.

48.

D



zw jwj2



54.

55.

3

cos.3 / C i sin.3 / D .cos  C i sin  / 3

2

D cos  C 3i cos  sin  Thus cos.3 / D cos3 

3 cos  sin 

i sin 

sin3  D 3 sin 

3 cos  4 sin3 :

56.

3 : 2

p

3

p

i;

3

i:

p

  3 3 C i sin The three cube roots of 1Ci D 2 cos 4 4 1=6 are of the form 2 .cos  C i sin  / where  D =4,  D 11=12, and  D 19=12. The four p fourth roots of 4 D 4.cos 0 C i sin 0/ are of the form 2.cos  C i sin  / where  D 0,p D =2, , p p and p 2, and i 2.  D 3=2. Thus they are 2, i 2, p i 3 D 0 hassolutions that are the  p 2 2 C i sin four fourth roots of 1 C i 3 D 2 cos . 3 3 1=4 Thus they are of the form 2 .cos  C i sin  /, where  D =6, 2=3, 7=6, and 5=3. They are the complex numbers The equation z 4 C 1

˙2

3

3 cos  sin2  D 4 cos3 

sin.3 / D 3 cos2  sin 

684

2

p

  3 3 8i D 8 cos C i sin are 2 2 of the form 2.cos  C i sin  / where  D =2,  D 7=6, and  D 11=6. Thus they are 2i;

53.

i

The three cube roots of

zw zw z D D D : jwj2 ww w

p p    z D 3 C i 3 D 2 3 cos C i sin 6 6   p 2 2 w D 1 C i 3 D 2 cos C i sin 3 3   p 5 5 C i sin zw D 4 3 cos 6 6  p p   z D i 3 D 3 cos C i sin w 2 2   p 3 3 z D 1 C i D 2 cos C i sin 4 4    w D 3i D 3 cos C i sin 2 2   p 5 5 zw D 3 2 cos C i sin D 3 3i 4 4 p  2  1 z  1 D cos C i sin D C i w 3 4 4 3 3

1 2

1;

1=4

p

! 3 1 C i ; 2 2

˙2

1=4

1 2

p

! 3 i : 2

The equation z 5 C a5 D 0 (a > 0) has solutions that are the five fifth roots of a5 D a .cos  C i sin /; they are of the form a.cos  C i sin  /, where  D =5, 3=5, , 7=5, and 9=5.

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INSTRUCTOR’S SOLUTIONS MANUAL

APPENDIX II (PAGE A-19)

57. The n nth roots of unity are

9.

!1 D 1

2 2 C i sin n n 4 4 C i sin D !22 !3 D cos n n 6 6 !4 D cos C i sin D !23 n n :: : 2.n 1/ 2.n 1/ !n D cos C i sin D !2n n n

The function w D z 2 D x 2 y 2 C 2xyi transforms the line y D 1 to u D x 2 1, v D 2x, which is the parabola v 2 D 4u C 4 with vertex at w D 1 and opening to the right.

!2 D cos

10. The function w D 1=z D .x yi /=.x 2 C y 2 / transforms the line x D 1 to the curve given parametrically by uD 1

:

u2 C v 2 D

!1 C !2 C !3 C    C !n D 1 C !2 C !22 C    C !2n 1 !2n 0 D D D 0: 1 !2 1 !2

vD

y : 1 C y2

This curve is, in fact, a circle,

Hence, 1

Appendix II Complex Functions (page A-19) In Solutions 1–12, z D x C yi and w D u C vi , where x, y, u, and v are real. The function w D z transforms the closed rectangle 0  x  1, 0  y  2 to the closed rectangle 0  u  1, 2  v  0.

2. The function w D z transforms the line x C y D 1 to the line u v D 1.

13.

8. The function w D z 2 D x 2 y 2 C 2xyi transforms the line x D 1 to u D 1 y 2 , v D 2y, which is the parabola v 2 D 4 4u with vertex at w D 1, opening to the left.

f .z/ D z 2 D .x C yi /2 D x 2

y 2 C 2xyi

f .z/ D z 3 D .x C yi /3 D x 3

3xy 2 C .3x 2 y

u D x2 y2; v D 2xy @u @v @u @v D 2x D ; D 2y D @x @y @y @x @v @u Ci D 2x C 2yi D 2z: f 0 .z/ D @x @x 14.

y 3 /i

u D x 3 3xy 2 ; v D 3x 2 y y 3 @v @u @v @u D 3.x 2 y 2 / D ; D 6xy D @x @y @y @x @u @v f 0 .z/ D Ci D 3.x 2 y 2 C 2xyi / D 3z 2 : @x @x

5. The function w D 1=z D z=jzj2 transforms the closed quarter-circular disk 0  jzj  2, 0  arg .z/  =2 to the closed region lying on or outside the circle jwj D 1=2 and in the fourth quadrant, that is, having =2  arg .w/  0. 6. The function w D iz rotates the z-plane 90ı , so transforms the wedge =4  arg .z/  =3 to the wedge =4  arg .z/  =6. p 7. The function w D z transforms the ray arg .z/ D =3 (that is, Arg .z/ D 5=3) to the ray arg .w/ D 5=6.

The function w D e z D e x cos y C i e x sin y transforms the horizontal strip 1 < x < 1, =4  y  =2 to the wedge =4  arg .w/  =2, or, equivalently, u  0, v  u.

12. The function w D e iz D e y .cos x C i sin x/ transforms the vertical half-strip 0 < x < =2, 0 < y < 1 to the first-quadrant part of the unit open disk jwj D e y < 1, 0 < arg .w/ D x < =2, that is u > 0, v > 0, u2 C v 2 < 1.

3. The function w D z 2 transforms the closed annular sector 1  jzj  2, =2  arg .z/  3=4 to the closed annular sector 1  jwj  4,   arg .w/  3=2. 4. The function w D z 3 transforms the closed quarter-circular disk 0  jzj  2, 0  arg .z/  =2 to the closed threequarter disk 0  jwj  8, 0  arg .w/  3=2.

1 C y2 D u; .1 C y 2 /2

with centre w D 1=2 and radius 1/2. 11.

1.

1 ; 1 C y2

15.

1 x yi D 2 z x C y2 x y uD 2 ; vD 2 x C y2 x C y2 @u @v @v y2 x2 @u 2xy D D D 2 ; D 2 @x .x C y 2 /2 @y @y .x C y 2 /2 @x .z/2 @v .x 2 y 2 / C 2xyi @u D D Ci D f 0 .z/ D 2 2 2 @x @x .x C y / .zz/2 f .z/ D

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1 : z2

685

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APPENDIX II (PAGE A-19)

16.

2

f .z/ D e z D e x x2

2

y2

y2

ADAMS and ESSEX: CALCULUS 9

.cos.2xy/ C i sin.2xy// x2

21.

y2

uDe cos.2xy/; vDe sin.2xy/ @v @u 2 2 D e x y .2x cos.2xy/ 2y sin.2xy// D @x @y @v @u 2 2 D e x y .2y cos.2xy/ C 2x sin.2xy// D @y @x @u @v f 0 .z/ D Ci @x @x 2 2 D e x y Œ2x cos.2xy/ 2y sin.2xy/ C i.2y cos.2xy/ C 2x sin.2xy// D .2x C 2yi /e x

17.

y2

yi

e

Thus cos y D

e yi

yi

Ce 2

e

yi

and sin y D

e

e zi C e 2

zi

and sin z D

D 2i sin y:

yi

yi

e zi

cosh z D

ez C e 2

and sinh z D

ez

e

20.

d cos z dz d sin z dz d cosh z dz d sinh z dz

D D D D

d dz d dz d dz d dz

686

zi

, e 2zi D 1

Œcos.2x/ C i sin.2x/ D 1

By Exercises 20 and 21, cosh z D 0 if and only if cos.iz/ D 0, that is, if and only if z D .2n C 1/ i=2 for integer n. Similarly, sinh z D 0 if and only if sin.iz/ D 0, that is, if and only if z D n i for integer n.

24.

e z D e xCyi D e x cos y C i e x sin y

D e x yi D e x cos y e x sin y ex C e x ex e x ez C e z D cos y C i sin y cosh z D 2 2 2 D cosh x cos y C i sinh x sin y Re.cosh z/ D cosh x cos y; Im.cosh z/ D sinh x sin y: e

ez

z

e

ex

e

x

e

e iz D e iz

De

yCxi y xi

D

De

y

y

cos y C i

ex C e 2

x

sin y 2 2 D sinh x cos y C i cosh x sin y Re.sinh z/ D sinh x cos y; Im.cosh z/ D cosh x sin y:

26.

e zi C e zi i e zi e zi D D sin z 2 2 zi zi zi zi ie C e e e D D cos z 2i 2i z z z z e e e Ce D D sinh z 2 2 z z z z e e e Ce D D cosh z 2 2

z

sinh z D

2

e iz C e iz D cosh z 2 iz iz e 1 e D sin z i sinh.iz/ D i 2 z z e Ce cos.iz/ D D cosh z 2 z z e e e z C ez sin.iz/ D Di D i sinh z 2i 2 cosh.iz/ D

23.

z

are periodic with period 2 i .

1

Thus the only complex zeros of sin z are its real zeros at z D n for integers n.

25.

z

1

, sin.2x/ D 0; e 2y cos.2x/ D 1 , y D 0; cos.2x/ D 1 D, y D 0; x D 0; ˙; ˙2; : : :

zi

are periodic with period 2, and

2y

,e

.

e 2i

, e 2zi D

Œcos.2x/ C i sin.2x/ D

sin z D 0 , e zi D e

2

e zC2 i D e x .cos.y C 2/ C i sin.y C 2// D e x .cos y C i sin y/ D e z : z Thus e is periodic with period 2 i . So is e z D 1=e z . Since e i.zC2/ D e ziC2 i D e zi , therefore e zi and also e zi are periodic with period 2. Hence cos z D

19.

22.

yi

e 2i

zi

e

, sin.2x/ D 0; e 2y cos.2x/ D 1 , y D 0; cos.2x/ D 1  3 D, y D 0; x D ˙ ; ˙ ; : : : 2 2 Thus the only complex zeros of cos z are its real zeros at z D .2n C 1/=2 for integers n.

.cos.2xy/ C i sin.2xy// D 2ze z :

D 2 cos y;

2y

,e

e yi D cos y C i sin y (for real y). Replacing y by y, we get e yi D cos y i sin y (since cos is even and sin is odd). Adding and subtracting these two formulas gives e yi C e

18.

2

cos z D 0 , e zi D

cos x C i e

D e cos x

y

sin x

y

i e sin x

e y C ey e y ey e iz C e iz D cos x C i sin x cos z D 2 2 2 D cos x cosh y i sin x sinh y Re.cos z/ D cos x cosh y; Im.cos z/ D sin x sinh y e y ey e y C ey e iz D cos x C i sin x 2i 2i 2i D sin x cosh y C i cos x sinh y Re.sin z/ D sin x cosh y; Im.sin z/ D cos x sinh y:

sin z D

27. 28.

e iz

z 2 C 2iz D 0 ) z D 0 or z D z

2

2z C i D 0 ) .z

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2i

1/ D 1 i   p 7 7 C i sin D 2 cos 4 4   7 7 C i sin ) z D 1 ˙ 21=4 cos 8 8

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29.

z 2 C 2z C 5 D 0 ) .z C 1/2 D 4 ) z D 1 ˙ 2i

30.

z2

2iz

31.

z3

3iz 2

33.

By long division (details omitted) we discover that z 5 C 3z 4 C 4z 3 C 4z 2 C 3z C 1 D z 3 C 3z 2 C 3z C 1 z2 C 1 D .z C 1/3 :

1 D 0 ) .z i /2 D 0 ) z D i (double root) 2z D z.z 2

3iz

) z D 0 or z 2 3iz 2 D 0   1 3 2 D i ) z D 0 or z 2 4   3 1 ) z D 0 or z D ˙ i 2 2 ) z D 0 or z D i or z D 2i

32.

APPENDIX III (PAGE A-26)

2/ D 0

Thus P .z/ has the five zeros: i , 36.

z 4 C 1 D 0 ) z 2 D i or z 2 D i 1 i 1Ci ) zD˙ p ; zD˙ p 2   2  1Ci 1 i 4 z C1D z z p p  2   2 1 i 1Ci zC p  zC p 2 2 !  !  2  1 1 1 2 1 D z p C C zC p 2 2 2 2 p p 2 2 D .z 2z C 1/.z C 2z C 1/

34. Since P .z/ D z 4 4z 3p C 12z 2 16z C 16 has real 3i is a zero of P .z/, then so is coefficients, if z1 D 1 z1 . Now z1 / D .z

1/2 C 3 D z 2

2z C 4:

By long division (details omitted) we discover that z4

4z 3 C 12z 2 16z C 16 D z2 z 2 2z C 4

35. Since P .z/ D z 5 C 3z 4 C 4z 3 C 4z 2 C 3z C 1 has real coefficients, if z1 D i is a zero of P .z/, then so is z2 D i . Now .z

z1 /.z

z2 / D .z

i /.z C i / D z 2 C 1:

1, and

1,

1.

2

Since P .z/ D z 2z 8z C 8z C 31z 30 has real coefficients, if z1 D 2 C i is a zero of P .z/, then so is z2 D 2 i . Now

z5

z2 / D z 2 C 4z C 5:

z1 /.z

2z 4

8z 3 C 8z 2 C 31z z 2 C 4z C 5 2 6z C 11z 6:

D z3

Observe that z3 D 1 is a zero of z 3 long division again: z3

6z 2 C 11z z 1

6

D z2

Hence P .z/ has the five zeros 4

37. If w D z C z jw

3

2iz

z 4 j D jz 3

30

6z 2 C 11z

5z C 6 D .z 2 C i,

2

6. By

2/.z

3/:

i , 1, 2, and 3.

3 and jzj D 2, then jz 4 j D 16 and 2iz

3j  8 C 4 C 3 D 15 < 16:

By the mapping principle described in the proof of Theorem 2, the image in the w-plane of the circle jzj D 2 is a closed curve that winds around the origin the same number of times that the image of z 4 does, namely 4 times.

Appendix III Continuous Functions (page A-26) 1.

To be proved: If a < b < c, f .x/  g.x/ for a  x  c, limx!b f .x/ D L, and limx!b g.x/ D M , then L  M . Proof: Suppose, to the contrary, that L > M . Let  D .L M /=3, so  > 0. There exist numbers ı1 > 0 and ı2 > 0 such that if a  x  b, then jx jx

2z C 4:

Thus z1 and z1 are both double zeros of P .z/. These are the only zeros.

i,

3

By long division (details omitted) we discover that

2z 2 C 4 D 0 ) .z 2 1/2 D 3 p p or z2 D 1 C i 3 z2 D 1 i 3    5 5   z 2 D 2 cos C i sin ; z 2 D 2 cos C i sin 3 3 3 3   p 5 5 z D ˙ 2 cos C i sin ; or 6 6   p   z D ˙ 2 cos C i sin 6 ! 6 ! r r i i 3 3 Cp p ; zD˙ zD˙ 2 2 2 2

z1 /.z

4

.z

z4

.z

5

Thus if jx

bj < ı1 ) jf .x/ bj < ı2 ) jg.x/

bj < ı D minfı1 ; ı2 ; b

f .x/ g.x/ > L  M

Lj <  M j < : a; c

DL M

bg, then

2 D

L

M 3

> 0:

This contradicts the fact that f .x/  g.x/ on Œa; b. Therefore L  M .

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2. To be proved: If f .x/  K on Œa; b/ and .b; c, and if limx!b f .x/ D L, then L  K.

8.

Proof: If L > K, then let  D .L K/=2; thus  > 0. There exists ı > 0 such that ı < b a and ı < c b, and such that if 0 < jx bj < ı, then jf .x/ Lj < . In this case L K f .x/ > L  D L > K; 2 which contradicts the fact that f .x/  K on Œa; b/ and .b; c. Therefore L  K.

x!a

9.

a) Let f .x/ D C , g.x/ D x. Let  > 0 be given and let ı D . For any real number x, if jx aj < ı, then jf .x/ jg.x/

f .a/j D jC C j D 0 < ; g.a/j D jx aj < ı D :

Thus limx!a f .x/ D f .a/ and limx!a g.x/ D g.a/, and f and g are both continuous at every real number a. 5. A polynomial is constructed by adding and multiplying finite numbers of functions of the type of f and g in Exercise 4. By Theorem 1(a), such sums and products are continuous everywhere, since their components have been shown to be continuous everywhere. 6. If P and Q are polynomials, they are continuous everywhere by Exercise 5. If Q.a/ ¤ 0, then P .a/ P .x/ D by Theorem 1(a). Hence P =Q is limx!a Q.x/ Q.a/ continuous everywhere except at the zeros of Q.

If m and n are integers and n is odd, then . x/m=n D cx m=n , where c D . 1/m=n is either 1 or 1 depending on the parity of m. Since x m=n is continuous at each positive number a, so is cx m=n . Thus . x/m=n is continuous at each positive number, and x m=n is continuous at each negative number. If r D m=n > 0, then limx!0C x r D 0 by Exercise 3. Hence limx!0 x r D . 1/r limx!0C x r D 0, also. Therefore limx!0 x r D 0, and x r is continuous at x D 0.

Thus limx!0C x r D 0. 4.

x!a

and x m=n is continuous at each positive number.

0 < x r < ı r D :

)

x!a

D .a1=n /m D am=n ;

3. Let  > 0 be given. Let ı D  1=r , (r > 0). Then 0 0 we have  m  m lim x m=n D lim x 1=n D lim x 1=n

10. Let  > 0 be given. Let ı D . If a is any real number then ˇ ˇ ˇ ˇ ˇjxj jajˇ  jx aj <  if jx aj < ı:

Thus limx!a jxj D jaj, and the absolute value function is continuous at every real number.

11.

By the definition of sin, P t D .cos t; sin t /, and Pa D .cos a; sin a/ are two points on the unit circle x 2 C y 2 D 1. Therefore aj D length of the arc from P t to Pa > length of the chord from P t to Pa p D .cos t cos a/2 C .sin t sin a/2 :

jt

If  > 0 is given, and jt inequality implies that j cos t j sin t

aj < ı D , then the above

cos aj  jt sin aj  jt

aj < ; aj < :

Thus sin is continuous everywhere. 7.

Suppose n is a positive integer and a > 0. Let  > 0 be given. Let b D a1=n , and let ı D minfa.1 2 n /; b n 1 g. If jx aj < ı, then x > a=2n , and if y D x 1=n , then y > b=2. Thus ˇ ˇ 1=n ˇx

ˇ ˇ a1=n ˇ D jy

bj jy n b n j C y n 2 b C    C bn aj bn 1  < D : 1 bn 1

D

yn 1


0 and  > 0. Let ı D min ; 2 2 1 2 a < whenever t is If jx aj < ı, then x > , so 2 t a between a and x. Thus j ln x

ln aj 1 between t D a and t D x t 2 a aj < D : a 2

D area under y D
0 be given. Assume (making  smaller if necessary) that  < e a . Since  ln 1

      C ln 1 C D ln 1 ea ea

2 e 2a



a

f .c/  f .x/  f .d /

< 0;

      . we have ln 1 C a < ln 1 e ea    Let ı D ln 1 C a . If jx aj < ı, then e       ln 1 < x a < ln 1 C a a e e   x a < e < 1 C 1 ea ea  x a 1j < a je e je x e a j D e a je x a 1j < : x

for all x in Œa; b. Since g is increasing, so is its inverse g 1 . Therefore

for all x in Œa; b, and f is bounded on that interval.

Appendix IV The Riemann Integral (page A-31)

1.

x

Thus limx!a e D e and e is continuous at every point a in its domain.

 L.f; P / D 1 1  U.f; P / D 1 1

Suppose a  xn  b for each n, and lim xn D L. Then a  L  b by Theorem 3. Let  > 0 be given. Since f is continuous on Œa; b, there exists ı > 0 such that if a  x  b and jx Lj < ı then jf .x/ f .L/j < . Since lim xn D L, there exists an integer N such that if n  N then jxn Lj < ı. Hence jf .xn / f .L/j <  for such n. Therefore lim.f .xn / D f .L/. t 16. Let g.t / D . For t ¤ 0 we have 1 C jt j

15.

g 0 .t / D

1 C jt j jt j 1 1 C jt j t sgn t D D > 0: .1 C jt j/2 .1 C jt j/2 .1 C jt j/2

h!0

g.h/

g.0/ h

D lim

h!0

2.

1 D 1: 1 C jhj

f .x/ 1 C jf .x/j

is also continuous there, being the composition of continuous functions. Also, h.x/ is bounded on Œa; b, since ˇ  ˇ ˇ ˇ ˇg f .x/ ˇ 

jf .x/j  1: 1 C jf .x/j

By assumption in this problem, h.x/ must assume maximum and minimum values; there exist c and d in Œa; b such that       g f .c/  g f .x/  g f .d /

Then

  C0C0D1 3 3   2   C1 C0D1C : 3 3 3

0

Thus g is continuous and increasing on R. If f is continuous on Œa; b, then   h.x/ D g f .x/ D

 ; 1 C 3 ; 2g. 3

Since U.f; P / L.f; P / < , f is integrable on Œ0; 2. Since L.f; P / < 1 < U.f; P / for every , therefore Z 2 f .x/ dx D 1.

If t D 0, g is also differentiable, and has derivative 1: g 0 .0/ D lim



1 if 0  x  1 0 if 1 < x  2 Let 0 <  < 1. Let P D f0; 1

f .x/ D

1 if x D 1=n .n D 1; 2; 3; : : :/ 0 otherwise If P is any partition of Œ0; 1 then L.f; P / D 0. Let 2 0 <   2. Let N be an integer such that N C1 >  N .  A partition P of Œ0; 1 can be constructed so that the first  two points of P are 0 and , and such that each of the 2 1 N points .n D 1; 2; 3; : : : ; n/ lies in a subinterval n 1  . Since every number of P having length at most 2N n h i with n a positive integer lies either in 0; or one of 2 these other N subintervals of P , and since max f .x/ D 1 for these subintervals and max f .x/ D 0 for all other   D . subintervals of P , therefore U.f; P /  C N 2 2N By Theorem 3, f is integrable on Œ0; 1. Evidently f .x/ D

Z

3.

n

1 0

f .x/ D

n

f .x/ dx D least upper bound L.f; P / D 0:

1=n if x D m=n in lowest terms 0 otherwise

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Clearly L.f; P / D 0 for every partition P of Œ0; 1. Let  > 0 be given. To show that f is integrable we must exhibit a partition P for which U.f; P / < . We can assume  < 1. Choose a positive integer N such that 2=N < . There are only finitely many integers n such that 1  n  N . For each such n, there are only finitely many integers m such that 0  m=n  1. Therefore there are only finitely many points x in Œ0; 1 where f .x/ > =2. Let P be a partition of Œ0; 1 such that all these points are contained in subintervals of the partition having total length less than =2. Since f .x/  1 on these subintervals, and f .x/ < =2 on all other subintervals P , therefore U.f; P /  1  .=2/ C .=2/  1 D ; and f is R1 integrable on Œ0; 1. Evidently 0 f .x/ dx D 0, since all lower sums are 0. I I  4. Suppose, to the contrary, that I > I  . Let  D , 3  so  > 0. By the definition of I and I , there exist partitions P1 and P2 of Œa; b, such that L.f; P1 /  I  and U.f; P2 /  I  C . By Theorem 2, L.f; P1 /  U.f; P2 /, so 3 D I

I   L.f; P1 / C 

Therefore U.f C g; P / Hence 6.

a

b

Af .x/ dx D A

Z

b

f .x/ dx:

a

It therefore remains to be proved only that the integral of a sum of functions is the sum of the integrals. Suppose that Z

a

b

f .x/ dx D I;

and

Z

a

U.g; P2 /

g.x/ dx D J:

   I < L.f; P1 / C 2 2    J < L.g; P2 / C : 2 2

Let P be the common refinement of P1 and P2 . Then the above inequalities hold with P replacing P1 and P2 . If m1  f .x/  M1 and m2  g.x/  M2 on any interval, then m1 C m2  f .x/ C g.x/  M1 C M2 there. It follows that U.f C g; P /  U.f; P / C U.g; P /; L.f; P / C L.g; P /  L.f C g; P /:

690

b

then there exist partitions P1 of Œa; b, and P2 of Œb; c such that  L.f; P1 /  I < L.f; P1 / C 2  L.f; P2 /  J < L.f; P2 / C 2 (with similar inequalities for upper sums). Let P be the partition of Œa; c formed by combining all the subdivision points of P1 and P2 . Then L.f; P / D L.f; P1 / C L.f; P2 /  I C J < L.f; P / C : Similarly, U.f; P /

 < I C J  U.f; P /. Therefore Z

7.

c a

f .x/ dx D I C J:

Let Z

b

a

and

f .x/ dx D I;

Z

a

b

g.x/ dx D J;

where f .x/  g.x/ on Œa; b. We want to show that I  J . Suppose, to the contrary, that I > J . Then there would exist a partition P of Œa; b for which

b

If  > 0, then there exist partitions P1 and P2 of Œa; b such that U.f; P1 /

Assume a < b < c; the other cases are similar. Let  > 0. If Z b Z c f .x/ dx D I; and f .x/ dx D J; a

Since  > 0, it follows that 3  2. This contradiction shows that we must have I  I  .

Z

Z b  f .x/ C g.x/ dx D I C J . a

U.f; P2 / C   2:

5. Multiplying a function by a constant multiplies all its Riemann sums by the same constant. If the constant is positive, upper and lower sums remain upper and lower; if the constant is negative upper sums become lower and vice versa. Therefore

  I C J  L.f C g; P / C :

I < L.f; P / C

I

J 2

and U.g; P /

;

I

J 2

< J:

I CJ > U.g; P /  L.g; P /. However, 2 f .x/  g.x/ on Œa; b implies that L.f; P /  L.g; P / for any partition. Thus we have a contradiction, and so I  J. Thus L.f; P / >

Since jf .x/j  f .x/  jf .x/j for any x, we can apply the above result to obtain Z

b a

jf .x/j dx 

Z

b a

f .x/ dx 

Z

a

ˇZ ˇ Z ˇ b ˇ b ˇ ˇ Therefore ˇ f .x/ dx ˇ  jf .x/j dx. ˇ a ˇ a

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b

jf .x/j dx:

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8. We have Z

APPENDIX IV (PAGE A-31)

By repeated applications of the triangle inequality, a a

f .x/ dx D D D

Z

Z

0 a a

Z0 a 0

f .x/ dx C

Z

f . x/ dx C

a

f .x/ dx

0

Z

jf .xk

a

1/

f .a/j D jf .xk

1/

f .x0 /j < k

1:

f .x/ dx 0

If x is any point in Œa; b, then x belongs to one of the intervals Œxk 1 ; xk , so, by the triangle inequality again,

Œf . x/ C f .x/ dx:

If f is odd, last integral is 0. If f is even, the last Z the a integral is 2f .x/ dx.

jf .x/ f .a/j  jf .x/ f .xk

1 /jCjf .xk 1 /

f .a/j < k  N:

0

9. Let  > 0 be given. Let ı D  2 =2. Let 0  x  1 and 0p y  1. If p x <  2 =4 and y <  2 =4 then p p j x yj  x C y < . If jx yj < ı and either x   2 =4 or y   2 =4 then p jx yj 2 2 p yj D p D : j x p <   2 xC y p Thus f .x/ D x is uniformly continuous on Œ0; 1. 10. Suppose f is uniformly continuous on Œa; b. Taking  D 1 in the definition of uniform continuity, we can find a positive number ı such that jf .x/ f .y/j < 1 whenever x and y are in Œa; b and jx yj < ı. Let N be a positive integer such that h D .b a/=N satisfies h < ı. If xk D a Ckh, (0  k  N ), then each of the subintervals of the partition P D fx0 ; x1 ; : : : ; xN g has length less than ı. Thus jf .xk /

f .xk

1 /j

0), and that f is integrable on Œa; b. Let  > 0 be given, and let ı D =K. If x and y belong to Œa; b and jx yj < ı, then jF .x/

ˇZ x ˇ Z y ˇ ˇ F .y/j D ˇˇ f .t / dt f .t / dt ˇˇ ˇZax ˇ a ˇ ˇ  ˇ Dˇ f .t / dt ˇˇ  Kjx yj < K D : K y

(See Theorem 3(f) of Section 6.4.) Thus F is uniformly continuous on Œa; b.

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