Calculus 3 Solution Manual
-
Upload
adrian-antonio-torres -
Category
Documents
-
view
519 -
download
25
description
Transcript of Calculus 3 Solution Manual
Calculus III
Instructor’s Solution Manual
Tunc Geveci
Spring 2011
ii
Contents
11 Vectors 1
11.1 Cartesian Coordinates in 3D and Surfaces . . . . . . . . . . . . . . . . . . . . . . 1
11.2 Vectors in Two and Three Dimensions . . . . . . . . . . . . . . . . . . . . . . . . 6
11.3 The Dot Product . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11
11.4 The Cross Product . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16
12 Functions of Several Variables 19
12.1 Tangent Vectors and Velocity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19
12.2 Acceleration and Curvature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21
12.3 Real-Valued Functions of Several Variables . . . . . . . . . . . . . . . . . . . . . 27
12.4 Partial Derivatives . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31
12.5 Linear Approximations and the Differential . . . . . . . . . . . . . . . . . . . . . 39
12.6 The Chain Rule . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 42
12.7 Directional Derivatives and the Gradient . . . . . . . . . . . . . . . . . . . . . . . 51
12.8 Local Maxima and Minima . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 58
12.9 Absolute Extrema and Lagrange Multipliers . . . . . . . . . . . . . . . . . . . . . 63
13 Multiple Integrals 69
13.1 Double Integrals Over Rectangles . . . . . . . . . . . . . . . . . . . . . . . . . . . 69
13.2 Double Integrals Over Non-Rectangular Regions . . . . . . . . . . . . . . . . . . 72
13.3 Double Integrals in Polar Coordinates: . . . . . . . . . . . . . . . . . . . . . . . . 79
13.4 Applications of Double Integrals . . . . . . . . . . . . . . . . . . . . . . . . . . . 84
13.5 Triple Integrals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 88
13.6 Triple Integrals in Cylindrical and Spherical Coordinates . . . . . . . . . . . . . . 94
14 Vector Analysis 107
14.1 Vector Fields, Divergence and Curl . . . . . . . . . . . . . . . . . . . . . . . . . . 107
14.2 Line Integrals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 109
14.3 Line Integrals of Conservative Vector Fields . . . . . . . . . . . . . . . . . . . . . 118
14.4 Parametrized Surfaces and Tangent Planes . . . . . . . . . . . . . . . . . . . . . 124
14.5 Surface Integrals . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 130
14.6 Green’s Theorem . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 140
14.7 Stokes’ Theorem . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 143
14.8 Gauss’ Theorem . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 146
iii
iv CONTENTS
Chapter 11
Vectors
11.1 Cartesian Coordinates in 3D and Surfaces
1.
If x = c then2c+ y + 4z = 8⇒ y + 4z = 8− 2c.
These are lines.
If y = c then2x+ c+ 4z = 8⇒ 2x+ 4z = 8− c.
These are lines.
If z = c then2x+ y + 4c = 8⇒ 2x+ y = 8− 4c.
These are lines.
2.
1
2 CHAPTER 11. VECTORS
If x = c thenz = 4c− 3y.
These are lines.
If y = c thenz = 4x− 3c.
These are lines.
If z = c thenc = 4x− 3y.
These are lines.
3.
If x = c thenz = 4c2 + 9y2
These are parabolas.
If y = c thenz = 4x2 + 9c2
These are parabolas.
If z = c thenc = 4x2 + 9y2
These are ellipses if c > 0. If c = 0 the curve is reduced to a single point, the origin. The surfacedoes not have any points below the xy-plane corresponding to c < 0.
4.
If x = c thenc = y2 + 4z2
These are ellipses if c > 0. If c = 0 the curve is reduced to a single point, the origin. The surfacedoes not have any points corresponding to c < 0.
11.1. CARTESIAN COORDINATES IN 3D AND SURFACES 3
If y = c thenx = c2 + 4z2
These are parabolas.
If z = c thenx = y2 + 4c2
These are parabolas.
5.
If x = c thenc2 + 2y2 + 4z2 = 4⇒ 2y2 + 4z2 = 4− c2.
These are ellipses if −2 < c < 2. The curve is reduced to a single point if c = ±2. The surfacedoes not have any points corresponding to x < −2 or x > 2.If y = c then
x2 + 2c2 + 4z2 = 4⇒ x2 + 4z2 = 4− 2c2
These are ellipses if −√2 < c < √2. The curve is reduced to a single point if c = ±√2. Thesurface does not have any points corresponding to y >
√2 or y < −√2.
If z = c thenx2 + 2y2 + 4c2 = 4⇒ x2 + 2y2 = 4− 4c2
These are ellipses if −1 < c < 1. The curve is reduced to a single point if c = ±1. The surfacedoes not have any points corresponding to z > 1 or z < −1.6.
If x = c then4c2 + y2 + 9z2 = 4⇒ y2 + 9z2 = 4− 4c2
These are ellipses if −1 < c < 1. The curve is reduced to a single point if c = ±1. The surfacedoes not have any points corresponding to x < −1 or x > 1.If y = c then
4x2 + c2 + 9z2 = 4⇒ 4x2 + 9z2 = 4− c2
4 CHAPTER 11. VECTORS
These are ellipses if −2 < c < 2. The curve is reduced a single point if c = ±2. The surfacedoes not have any points corresponding to y > 2 or y < −2.If z = c then
4x2 + y2 + 9c2 = 4⇒ 4x2 + y2 = 4− 9c2
These are ellipses if −2/3 < c < 2/3. The curve is reduced to a single point if c = ±2/3. Thesurface does not have any points corresponding to z > 2/3 or z < −2/3.7.
If x = c thenc2 − 9y2 − 4z2 = 1⇒ 9y2 + 4z2 = c2 − 1
These are ellipses if c < −1 or c > 1. The curve is reduced to a single point if c = ±1. Thesurface does not have any points corresponding to −1 < x < 1.If y = c then
x2 − 9c2 − 4z2 = 1⇒ x2 − 4z2 = 1 + 9c2
These are hyperbolas.
If z = c thenx2 − 9y2 − 4c2 = 1⇒ x2 − 9y2 = 1 + 4c2
These are hyperbolas.
8.
If x = c then4y2 − c2 − 2z2 = 1⇒ 4y2 − 2z2 = 1 + c2
These are hyperbolas.
If y = c then4c2 − x2 − 2z2 = 1⇒ x2 + 2z2 = 4c2 − 1
11.1. CARTESIAN COORDINATES IN 3D AND SURFACES 5
These are ellipses if c > 1/2 or c < −1/2. The surface does not have any points correspondingto −1/2 < y < 1/2.If z = c then
4y2 − x2 − 2c2 = 1⇒ 4y2 − x2 = 1 + 2c2These are hyperbolas.
9.
If x = c theny2 − c2 + z2 = 1⇒ y2 + z2 = 1 + c2
These are circles.
If y = c thenc2 − x2 + z2 = 1⇒ −x2 + z2 = 1− c2
These are hyperbolas.
If z = c theny2 − x2 + c2 = 1⇒ y2 − x2 = 1− c2
These are hyperbolas.
10.
If x = c thenc2 + y2 − z2 = 4⇒ y2 − z2 = 4− c2
These are hyperbolas.
If y = c thenx2 + c2 − z2 = 4⇒ x2 − z2 = 4− c2
These are hyperbolas.
If z = c thenx2 + y2 − c2 = 4⇒ x2 + y2 = 4 + c2
These are circles.
6 CHAPTER 11. VECTORS
11.2 Vectors in Two and Three Dimensions
1.
P1 = (1, 2) , P2 = (3, 5) , Q1 = (2, 1)
a)
v = (2, 3)
b) −−→OQ2 =
−−→OQ1 + v = (2, 1) + (2, 3) = (4, 4) .
Therefore, Q2 = (4, 4) .
1 2 3 4x
1
2
3
4
5
y
P1
P2
Q1
Q2
2.
P1 = (−2, 3) , P2 = (−4, 2) , Q1 = (1, 3)a)
v = (−2,−1)b) −−→
OQ2 =−−→OQ1 + v =(1, 3) + (−2,−1) = (−1, 2) .
Therefore, Q2 = (−1, 2) .
-6 -4 -2 -1 1 2 3 5x
2
3
4
5
y
P1
P2
Q1
Q2
3.
P1 = (2,−3) , P2 = (4, 2) , Q1 = (3, 2)a)
v =(2, 5)
b) −−→OQ2 =
−−→OQ1 + v = (3, 2) + (2, 5) = (5, 7)
11.2. VECTORS IN TWO AND THREE DIMENSIONS 7
Therefore, Q2 = (5, 7).
2 3 4 5x
-3
2
7
y
P1
P2Q1
Q2
4.
P1 = (−2,−1) , P2 = (−4, 2) , Q1 = (−1, 2)a)
v = (−2, 3)b) −−→
OQ2 =−−→OQ1 + v =(−1, 2) + (−2, 3) = (−3, 5)
Therefore, Q2 = (−3, 5) .
-4 -3 -2 -1x
-1
2
5
y
P1
P2
Q1
Q2
5.
a)
v+w = (2, 1) + (3, 4) = (5, 5)
b)
2 3 5
1
4
5
v
wv+w
8 CHAPTER 11. VECTORS
6.
a)
v +w = (2,−3) + (3, 2) = (5,−1)b)
2 3 5
-3
-1
2
3
5
v
w
v+w
7.
a)
v +w = (−2,−1) + (2, 4) = (0, 3)b)
-2 -1 2
-1
3
4
v
w
v+w
8.
a)
v+w = (2, 3) + (−1,−5) = (1,−2)b)
-1 1 2
-5
-3
-2
v
w
v+w
11.2. VECTORS IN TWO AND THREE DIMENSIONS 9
9.
a)
v +w = (2, 4) + (−1, 2) = (1, 6)b)
-1 2
2
4
6
v
w
v+w
10.
a)
v+w = (−4, 2) + (3, 1) = (−1, 3)b)
-4 3-1
2
1
3
v
w
v+w
11.
v −w = (2, 4)− (−2, 2) = (4, 2)
2-2 4
4
2 v
w
v- w
12.
a)
v−w = (−4, 2)− (3, 1) = (−7, 1)
10 CHAPTER 11. VECTORS
b)
-4 3-7
2
1v
w
v- w
13.
2v− 3w = 2 (3,−1)− 3(−2, 5) = (6,−2) + (6,−15) = (12,−17)14.
−4v+ 5w = −4 (2, 4) + 5 (1,−4) = (−8,−16) + (5,−20) = (−3,−36)15.
a) We have
||v|| =p32 + 42 =
√25 = 5.
Therefore,
u =1
||v||v =1
5(3, 4) =
µ3
5,4
5
¶.
b)
3
4
v
u
16.
a) We have
||v|| =q(−2)2 + 22 =
√8.
Therefore,
u =1
||v||v ==1√8(−2, 2) =
µ− 2√
8,2√8
¶=
Ã−√8
4,
√8
4
!
b)
11.3. THE DOT PRODUCT 11
-2
2
v
u
17.
a)
v = 3i+ 2j, w = −2i+4jb)
2v− 3w = 2 (3i+ 2j)− 3 (−2i+4j) = 6i+ 4j+ 6i− 12j = 12i− 8j18.
a)
v = −4i+ j, w = 4i+ 3jb)
2v+w = 2 (−4i+ j) + 4i+ 3j = −8i+ 2j+ 4i+ 3j = −4i+ 5j19.
a)
v = −2i+ 3j+ 6k, w = 4i− 2j+ kb)
−v+ 4w = − (−2i+ 3j+ 6k) + 4 (4i− 2j+ k)= 2i− 3j− 6k+16i− 8j+ 4k = 18i− 11j− 2k
20.
a)
v = −i− 3j+ 5k, w = 7i+ 2j− 2kb)
3v − 2w = 3 (−i− 3j+ 5k)− 2 (7i+ 2j− 2k)= −3i− 9j+ 15k−14i− 4j+ 4k
11.3 The Dot Product
1.
a)
||v|| = 1, ||w|| =√2, v ·w = 1.
b)
θ = arccos
µv ·w
||v|| ||w||¶= arccos
µ1√2
¶=
π
4.
2.
a)
||v|| = 1, ||w|| = √1 + 3 =√4 = 2, v ·w = −1.
12 CHAPTER 11. VECTORS
b)
θ = arccos
µv ·w
||v|| ||w||¶= arccos
µ−12
¶= π − π
3=2π
3.
3.
a)
||v|| =√2, ||w|| =
vuutÃ√3 + 12
!2+
Ã√3− 12
!2=√2,
v ·w =√3 + 1
2+
√3− 12
=√3
b)
θ = arccos
µv ·w
||v|| ||w||¶= arccos
à √3√2√2
!= arccos
Ã√3
2
!=
π
6
4.
a)
||v|| =√2, ||w|| =
√2, v ·w = 0.
b)
θ = arccos
µv ·w
||v|| ||w||¶= arccos (0) =
π
2.
Thus, v and w are orthogonal to each other.
5.
a)
||v|| =√2, ||w|| =
vuutÃ√3 + 12
!2+
Ã1−√32
!2=√2,
v ·w = 1b)
θ = arccos
µv ·w
||v|| ||w||¶= arccos
µ1√2√2
¶= arccos
µ1
2
¶=
π
3.
6.
a)
||v|| =√2, ||w|| =
√2, v ·w = 0.
b) θ = arccos (0) = π/2. The vectors v and w are orthogonal to each other.
7.
a)
||v|| =√5, ||w|| =
√2, v ·w = −1
b)
cos (θ) =v ·w
||v|| ||w|| =−1√5√2= − 1√
10.
c)
θ = arccos
µ− 1√
10
¶∼= 1. 892 55
8.
a)
||v|| =√13, ||w|| =
√20, v ·w = (3) (−2) + (2) (4) = 2
11.3. THE DOT PRODUCT 13
b)
cos (θ) =v ·w
||v|| ||w|| =2√13√20=
2√260
c)
θ = arccos
µ2√260
¶= 1. 446 44
9.
a)
||v|| =√5, ||w|| =
√10, v ·w = (−2) (−1) + (−1) (3) = −1
b)
cos (θ) =v ·w
||v|| ||w|| =−1√5√10= − 1√
50.
c)
θ = arccos
µ− 1√
50
¶= 1. 712 69
10.
a)
||v|| =p1 + 32 + 1 =
√11, ||w|| =
p22 + 1 + 1 =
√6,
v ·w = (1) (2) + (3) (−1) + (−1) (1) = −2b)
cos (θ) =v ·w
||v|| ||w|| =−2√11√6= − 2√
66
c)
θ = arccos
µ− 2√
66
¶= 1. 819 54
11.
a)
||v|| = √4 + 9 =√13⇒ u =
1
||v||v =1√13(2, 3) =
µ2√13,3√13
¶b) The direction cosines of v are
2√13and
3√13
12.
a)
||v|| = √1 + 4 =√5⇒ u =
1
||v||v =1√5(−i+2j) = − 1√
5i+
2√5j
b) The direction cosines of v are
− 1√5and
2√5
13.
a)
||v|| = √9 + 16 = 5⇒ u =1
||v||v =1
5(−3, 4) =
µ−35,4
5
¶b) The direction cosines of v are
−35and
4
5
14 CHAPTER 11. VECTORS
14.
a)
||v|| = √1 + 4 + 1 =√5⇒ u =
1
||v||v =1√5(i− 2j+ k) = 1√
5i− 2√
5j+
1√5k
b) The direction cosines of v are1√5, − 2√
5and
1√5
15.
a)
||w|| = √36 + 4 =√40⇒ u =
1
||w||w =1√40(6, 2) =
µ6√40,2√40
¶b)
compwv = v · u =(3, 4) ·µ
6√40,2√40
¶=
26√40
c)
Pwv =(compwv)u =26√40u =
26√40
µ6√40,2√40
¶=
µ39
10,13
10
¶d)
v2 = v−Pwv =(3, 4)−µ39
10,13
10
¶=
µ− 910,27
10
¶
-2 2 4 6 8
2
4
vw
Pwv
v2
16.
a)
||w|| = √4 + 1 =√5⇒ u =
1
||w||w =1√5(2, 1) =
µ2√5,1√5
¶b)
compwv = v · u =(−2, 1) ·1√5(2, 1) = − 3√
5
c)
Pwv =(compwv)u = −3√5
µ2√5,1√5
¶=
µ−65,−35
¶d)
v2 = v−Pwv =(−2, 1)−µ−65,3
5
¶=
µ−45,2
5
¶
11.3. THE DOT PRODUCT 15
-3 -2 -1 1 2 3
-3
-2
-1
1
2
3
wv
Pwv
v2
17.
a)
||w|| = √4 + 1 =√5⇒ u =
1
||w||w =1√5(2,−1) =
µ2√5,− 1√
5
¶b)
compwv = v · u =(1,−2) ·µ2√5,− 1√
5
¶=
4√5
c)
Pwv =(compwv)u =4√5
µ2√5,− 1√
5
¶=
µ8
5,−45
¶d)
v2 = v −Pwv = (1,−2)−µ8,−4
5
¶=
µ−7,−6
5
¶
1 2 3
-1
-2
Pwv
v
w
v2
18.
a)
||w|| = √9 + 16 = 5⇒ u =1
||w||w =1
5(−3,−4) =
µ−35,−45
¶b)
compwv = v · u = (−2,−6) ·µ−35,−45
¶= 6
c)
Pwv =(compwv)u = 6
µ−35,−45
¶=
µ−185,−24
5
¶
16 CHAPTER 11. VECTORS
d)
v2 = v −Pwv = (−2,−6)−µ−185,−24
5
¶=
µ8
5,−65
¶
-2-4-6
-2
-4
-6
w
v
Pwv
v2
11.4 The Cross Product
1.
v×w =¯¯ i j k
2 1 01 3 0
¯¯ = ¯ 1 0
3 0
¯i−
¯2 01 0
¯j+
¯2 11 3
¯k = 5k
2.
v ×w =¯¯ i j k
0 3 20 −2 1
¯¯ = ¯ 3 2
−2 1
¯i−
¯0 20 1
¯j+
¯0 30 −2
¯k = 7i
3.
v×w =¯¯ i j k
3 1 4−2 3 1
¯¯ =
¯1 43 1
¯i−
¯3 4−2 1
¯j+
¯3 1−2 3
¯k
= −11i− 11j+ 11k
4.
v ×w =¯¯ i j k
−2 1 41 −2 5
¯¯ =
¯1 4−2 5
¯i−
¯ −2 41 5
¯j+
¯ −2 11 −2
¯k
= 13i+ 14j+ 3k
5.
(−1, 3, 0)× (2, 6, 0) =¯¯ i j k
−1 3 02 6 0
¯¯ = ¯ −1 3
2 6
¯k = −12k
Therefore, the area of the parallelogram spanned by (−1, 3) and (2, 6) is
||(−1, 3, 0)× (2, 6, 0)|| = ||−12k|| = 12.
11.4. THE CROSS PRODUCT 17
6.
(−i+ 3j− 2k)× (4i− j− 6k) =
¯¯ i j k
−1 3 −24 −1 −6
¯¯
=
¯3 −2−1 −6
¯i−
¯ −1 −24 −6
¯j+
¯ −1 34 −1
¯k
= −20i− 14j+−11kTherefore, the area of the parallelogram spanned by −i+ 3j− 2k and 4i− j− 6k is
||−20i− 14j+−11k|| =p202 + 142 + 112 =
√717 (∼= 26. 776 9)
7.
u · (v ×w) =¯¯ 2 1 33 1 01 0 4
¯¯ = 2
¯1 00 4
¯−¯3 01 4
¯+ 3
¯3 11 0
¯= 2 (4)− 12 + 3 (−1) = −7
Therefore, the volume of the parallelepiped spanned by u,v and w is |−7| = 7.8.
u · (v×w) =¯¯ 2 2 53 −1 −41 −1 0
¯¯ = 2
¯ −1 −4−1 0
¯− 2
¯3 −41 0
¯+ 5
¯3 −11 −1
¯= 2 (−4)− 2 (4) + 5 (−2) = −26
Therefore, the volume of the parallelepiped spanned by u,v and w is |−26| = 26.9.
3 (x− 1) + 2 (y − 3) + (z − 4) = 0⇔ 3x+ 2y + z = 13
10.
(x− 2)− 2y + 4 (z − 5) = 0⇔ x− 2y + 4z = 2211.
− (x− 3) + (y − 1) + 2 (z + 3) = 0⇔ −x+ y + 2z = −812.
(x− 3)− 4 (y − 1)− (z − 2) = 0⇐⇒ x− 4y − z = −313. We have −−−→
P0P1 = (−1, 0,−1) and −−−→P0P2 = (0,−5, 2) .We set
N =−−−→P0P1 ×−−−→P0P2 =
¯¯ i j k
−1 0 −10 −5 2
¯¯
=
¯0 −1−5 2
¯i−
¯ −1 −10 2
¯j+
¯ −1 00 −5
¯k
= −5i+ 2j+ 5kThe vector N is orthogonal to the plane. Therefore, the equation of the plane is
(−5i+ 2j+ 5k)× ((x− 1) i+ (y − 2) j+ (z − 2)k) = 0
18 CHAPTER 11. VECTORS
⇔−5 (x− 1) + 2 (y − 2) + 5 (z − 2) = 0⇔ −5 + 2y + 5z = 9
14. We have −−−→P0P1 = (−3, 6, 2) and −−−→P0P2 = (−2, 5,−1)
We set
N =−−−→P0P1 ×−−−→P0P2 =
¯¯ i j k
−3 6 2−2 5 −1
¯¯
=6 25 −1 i−
¯ −3 2−2 −1
¯j+
¯ −3 6−2 5
¯k
= −16i− 7j− 3k
The vector N is orthogonal to the plane. Therefore, the equation of the plane is
−16 (x− 3)− 7 (y + 2)− 3 (z + 1) = 0 ⇔ −16x− 7y − 3z = −31⇔ 16x+ 7y + 3z = 31
Chapter 12
Functions of Several Variables
12.1 Tangent Vectors and Velocity
1.
a)
σ0 (t) =d
dt
¡t, sin2 (4t)
¢=
µd
dt(t) ,
d
dtsin2 (4t)
¶= (1, 8 sin (4t) cos (4t))
(= i+ 8 sin (4t) cos (4t) j)
Therefore,
σ0³π3
´=
µ1 + 8 sin
µ4π
3
¶cos
µ4π
3
¶¶=
Ã1, 8
Ã−√3
2
!µ−12
¶!=
³1, 2√3´ ³
= i+ 2√3j´
Thus, ¯¯σ0³π3
´¯¯=√1 + 12 =
√13.
Therefore,
T³π3
´=
1√13
³1, 2√3´=
Ã1√13,2√3√13
! Ã=
1√13i+
2√3√13j
!b) We have
σ³π3
´=
µπ
3, sin2
µ4π
3
¶¶=
µπ
3,3
4
¶Therefore,
L (u) = σ³π3
´+ uσ0
³π3
´=
µπ
3,3
4
¶+ u
³1, 2√3´
=
µπ
3+ u,
3
4+ 2√3u
¶, −∞ < u ≤ +∞.
2.
19
20 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
a)
σ0 (t) =d
dt(2 cos (3t) , sin (t)) = (−6 sin (3t) , cos (t)) .
Therefore,
σ0³π4
´=
µ−6 sin
µ3π
4
¶, cos
³π4
´¶=
Ã−3√2,
√2
2
!Thus, ¯¯
σ0³π4
´¯¯=
r18 +
1
2=
r37
2
Therefore,
T³π4
´=
r2
37
Ã−3√2,
√2
2
!=
µ− 6√
37,1√37
¶b) We have
σ³π4
´=
µ2 cos
µ3π
4
¶, sin
³π4
´¶=
Ã−√2,
√2
2
!.
Therefore,
L (u) = σ³π4
´+ uσ0
³π4
´=
Ã−√2,
√2
2
!+ u
Ã−3√2,
√2
2
!
=
Ã−√2− 3
√2u,
√2
2+
√2
2u
!, u ∈ R
3.
a)
σ0 (t) =µd
dt
µ3t
t2 + 1
¶,d
dt
µ3t2
t2 + 1
¶¶=
Ã−3t2 + 3(t2 + 1)
2 ,6t
(t2 + 1)2
!Therefore,
σ0 (1) =µ0,3
2
¶Thus,
||σ0 (1)|| = 3
2.
Therefore,
T (1) =2
3σ0 (1) = (0, 1) (= j) .
b) We have
σ (1) =
µ3
2,3
2
¶.
Therefore,
L (u) = σ (1) + uσ0 (1) =µ3
2,3
2
¶+ u
µ0,3
2
¶=
µ3
2,3
2+3
2u
¶, u ∈ R.
4.
a)
σ0 (t) =µd
dt(4 cos (3t)) ,
d
dt(4 sin (3t)) ,
d
dt(2t)
¶= (−12 sin (3t) , 12 cos (3t) , 2) .
12.2. ACCELERATION AND CURVATURE 21
Therefore,
σ0³π2
´=
µ−12 sin
µ3π
2
¶, 12 cos
µ3π
2
¶, 2
¶= (12, 0, 2) .
Thus, ¯¯σ0³π2
´¯¯=√144 + 4 =
√148
Therefore,
T³π2
´=
1√148
σ0³π2
´=
1√148
(12, 0, 2) =
µ12√148
, 0,2√148
¶.
b) We have
σ³π2
´=
µ4 cos
µ3π
2
¶, 4 sin
µ3π
2
¶, 2³π2
´¶= (0,−4,π) .
Therefore,
L (u) = σ³π2
´+ uσ0
³π2
´= (0,−4,π) + u (12, 0, 2) = (12u,−4,π + 2u) , u ∈ R.
5.
v (t) = σ0 (t) =
µd
dt
¡e−t sin (t)
¢,d
dt
¡e−t cos (t)
¢¶=
¡e−t (cos (t)− sin (t)) ,−e−t (cos (t) + sin (t))¢
= e−t (cos (t)− sin (t)) i− e−t (cos (t) + sin (t)) j
Therefore,
v (π) =¡−e−π, e−π¢ = −e−πi+ e−πj
Thus, the speed at t = π is
||v (π)|| =pe−2π + e−2π =
√2e−π.
6.
v (t) = σ0 (t) =
µd
dt(t) ,
d
dtarctan (t)
¶=
µ1,
1
t2 + 1
¶= i+
1
t2 + 1j
Therefore,
v (1) =
µ1,1
2
¶= i+
1
2j
Thus, the speed at t = 1 is
||v (1)|| =r1 +
1
4=
√5
2
12.2 Acceleration and Curvature
1. We have
v (t) = σ0 (t) =
µd
dt(6 + 3 cos (4t)) ,
d
dt(6 + 3 sin (4t))
¶= (−12 sin (4t) , 12 cos (4t)) .
22 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
Therefore,
a (t) = v0 (t) = (−48 cos (4t) ,−48 sin (4t)) = −48 cos (4t) i− 48 sin (4t) j
Thus,
a (π/12) = −48 cos³π3
´i− 48 sin
³π3
´j = −48
µ1
2
¶i− 48
Ã√3
2
!j
= −24i− 24√3j
2. We have
v (t) = σ0 (t) =
µd
dt(6t− 6 sin (2t)) , d
dt(6t− 6 cos (2t))
¶= (6− 12 cos (2t) , 6 + 12 sin (2t)) .
Therefore,
a (t) = v0 (t) = (24 sin (2t) , 24 cos (2t)) .
Thus,
a (0) = (0, 24) .
3. We have
v (t) = σ0 (t) =µd
dt(t) ,
d
dtarctan (t)
¶=
µ1,
1
t2 + 1
¶= i+
1
t2 + 1j
Therefore,
a (t) = v0 (t) =d
dt
¡t2 + 1
¢−1j = −2t ¡t2 + 1¢−2 j = − 2t
(t2 + 1)2j.
Thus,
a (1) = −24j = −1
2j.
4. We have
v (t) = σ0 (t) =µd
dt
¡tet¢,d
dtet¶=¡et + tet, et
¢=¡et + tet
¢i+ etj
Therefore,
a (t) = v0 (t) =¡2et + tet
¢i+ etj
Thus,
a (2) = 4e2i+ e2j
5. We have
σ0 (t) =d
dt(4 + 2 cos (t) , 3 + 2 sin (t)) = (−2 sin (t) , 2 cos (t)) = 2 (− sin (t) , cos (t))
and
||σ0 (t)|| = 2qsin2 (t) + cos2 (t) = 2.
Therefore,
T (t) =σ0 (t)||σ0 (t)|| =
1
2(2 (− sin (t) , cos (t))) = (− sin (t) , cos (t))
12.2. ACCELERATION AND CURVATURE 23
Thus,
T (π/6) =³− sin
³π6
´, cos
³π6
´´=
Ã−12,
√3
2
!=1
2
³−1,√3´.
We have
dT
dt=d
dt(− sin (t) , cos (t)) = (− cos (t) ,− sin (t)) = − (cos (t) , sin (t))
and ¯¯dT
dt
¯¯= ||− (cos (t) , sin (t))|| =
qcos2 (t) + sin2 (t) = 1.
Therefore,
N (t) =T0 (t)||T0 (t)|| = T
0 (t) = − (cos (t) , sin (t)) .
Thus,
N (π/6) = −³cos³π6
´, sin
³π6
´´= −
Ã√3
2,1
2
!= −1
2
³√3, 1´.
6. We have
σ0 (t) =d
dt(cos (3t) , sin (3t) , 4t) = (−3 sin (3t) , 3 cos (3t) , 4)
and
||σ0 (t)|| =q9 sin2 (3t) + 9 cos2 (3t) + 16 =
√25 = 5.
Therefore,
T (t) =σ0 (t)||σ0 (t)|| =
1
5(−3 sin (3t) , 3 cos (3t) , 4) =
µ−35sin (3t) ,
3
5cos (3t) ,
4
5
¶.
Thus,
T (π/2) =
µ−35sin
µ3π
2
¶,3
5cos
µ3π
2
¶,4
5
¶=
µ3
5, 0,
4
5
¶=1
5(3, 0, 4) .
We have
dT
dt=
d
dt
µ−35sin (3t) ,
3
5cos (3t) ,
4
5
¶=
µ−95cos (3t) ,−9
5sin (3t) , 0
¶= −9
5(cos (3t) , sin 3t, 0)
and ¯¯dT
dt
¯¯=
¯¯−95(cos (3t) , sin 3t, 0)
¯¯=9
5
qcos2 (3t) + sin2 (3t) =
9
5.
Therefore,
N (t) =T0 (t)||T0 (t)|| =
5
9
µ−95(cos (3t) , sin (3t) , 0)
¶= − (cos (3t) , sin (3t) , 0)
Thus
N (π/2) = −µcos
µ3π
2
¶, sin
µ3π
2
¶, 0
¶= (0, 1, 0) .
24 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
Therefore,
B (π/2) = T (π/2)×N (π/2) =1
5(3, 0, 4)× (0, 1, 0) =
=1
5
¯¯ i j k
3 0 40 1 0
¯¯ = 1
5(−4i+ 3k) .
7.
a) We have
σ0 (t) =d
dt(2 cos (t) , 3 sin (t)) = (−2 sin (t) , 3 cos (t))
so that
||σ0 (t)|| =q4 sin2 (t) + 9 cos2 (t).
Therefore,
s (t) =
Z t
0
||σ0 (τ)|| dτ =Z t
0
q4 sin2 (τ) + 9 cos2 (τ)dτ .
b)
s (π) =
Z π
0
q4 sin2 (τ) + 9 cos2 (τ)dτ ∼= 7. 932 72
8.
a) We have
σ0 (t) =d
dt
¡tet, et
¢=¡et + tet, et
¢= et (1 + t, 1)
so that
||σ0 (t)|| = etq(1 + t)2 + 1 = et
pt2 + 2t+ 2.
Therefore,
s (t) =
Z t
0
||σ0 (τ)|| dτ =Z t
0
eτpτ2 + 2τ + 2dτ .
b)
s (1) =
Z 1
0
eτpτ2 + 2τ + 2dτ ∼= 3. 227 01
9. We have
σ0 (t) =d
dt(3 cos (t) , 2 sin (t) , 0) = (−3 sin (t) , 2 cos (t) , 0)
and
σ00 (t) =d
dt(−3 sin (t) , 2 cos (t) , 0) = (−3 cos (t) ,−2 sin (t) , 0) .
Thus,
σ0 (π/2) = (−3, 0, 0) and σ00 (π/2) = (0,−2, 0) .Therefore,
||σ0 (π/2)||3 = 23 = 8.
We have
σ00 (π/2)× σ0 (π/2) =
¯¯ i j k
0 −2 0−3 0 0
¯¯ = −6k
12.2. ACCELERATION AND CURVATURE 25
so that
||σ00 (π/2)× σ0 (π/2)|| = 6.Therefore,
κ (π/2) =||σ00 (π/2)× σ0 (π/2)||
||σ0 (π/2)||3 =6
8=3
4.
10. We have
σ0 (t) =d
dt
¡t, et, 0
¢=¡1, et, 0
¢and
σ00 (t) =d
dt
¡1, et, 0
¢=¡0, et, 0
¢.
Thus,
σ0 (2) =¡1, e2, 0
¢and σ00 (2) =
¡0, e2, 0
¢.
Therefore,
||σ0 (2)||3 =³p
1 + e4´3=¡1 + e4
¢3/2.
We have
σ00 (2)× σ0 (2) =
¯¯ i j k
0 e2 01 e2 0
¯¯ = −e2k
so that
||σ00 (2)× σ0 (2)|| = e2.Therefore,
κ (2) =||σ00 (2)× σ0 (2)||
||σ0 (2)||3 =e2
(1 + e4)3/2
11. We have
v (t) = σ0 (t) =d
dt(cos (2t) , sin (2t) , 0) = (−2 sin (2t) , 2 cos (2t) , 0)
so that the speed is
||v (t)|| =q4 sin2 (2t) + 4 cos2 (2t) = 2.
Therefored
dt||v (t)|| = d
dt(2) = 0.
Thus, the tangential component of the acceleration is always 0 (this is merely a circular motion).
We have
σ0 (π/6) = (−2 sin (π/3) , 2 cos (π/3) , 0) =Ã−2Ã√
3
2
!, 2
µ1
2
¶, 0
!=³−√3, 1, 0
´so that
||σ0 (π/6)|| = √3 + 1 = 2.We have
σ00 (t) =d
dt(−2 sin (2t) , 2 cos (2t) , 0) = (−4 cos (2t) ,−4 sin (2t) , 0) ,
so that
σ00 (π/6) = (−4 cos (π/3) ,−4 sin (π/3) , 0) =Ã−4µ1
2
¶,−4
Ã√3
2
!, 0
!= −2
³1,√3, 0´.
26 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
Therefore,
σ00 (π/6)× σ0 (π/6) =
¯¯ i j k
−2 −2√3 0
−√3 1 0
¯¯ = (−2− 6)k = −8k
so that
||σ00 (π/6)× σ0 (π/6)|| = 8.Thus,
κ (π/6) =||σ00 (π/6)× σ0 (π/6)||
||σ0 (π/6)||3 =8
23= 1.
Therefore, the normal component of the acceleration is
κ (π/6) ||v (π/6)||2 = (1) ¡23¢ = 8.12. We have
v (t) = σ0 (t) =d
dt
¡t, t2, 0
¢= (1, 2t, 0)
so that the speed is
||v (t)|| =p1 + 4t2.
Therefored
dt||v (t)|| = d
dt
p1 + 4t2 =
1
2√1 + 4t2
(8t) =4t√1 + 4t2
.
Thus, the tangential component of the acceleration at t = 1 is
d
dt||v (t)||
¯t=1
=4√5.
We have
σ0 (1) = (1, 2, 0)
so that
||σ0 (1)|| =√5.
We have
σ00 (t) =d
dt(1, 2t, 0) = (0, 2, 0)
Therefore,
σ00 (1)× σ0 (1) =
¯¯ i j k
0 2 01 2 0
¯¯ = −2k
so that
||σ00 (1)× σ0 (1)|| = 2.Thus,
κ (1) =||σ00 (1)× σ0 (1)||
||σ0 (1)||3 =2¡√5¢3 = 2
53/2.
Therefore, the normal component of the acceleration is
κ (1) ||v (1)||2 =µ2
53/2
¶(5) =
2
5
√5
12.3. REAL-VALUED FUNCTIONS OF SEVERAL VARIABLES 27
12.3 Real-Valued Functions of Several Variables
In the plots of the level curves for problems 1-6, the smaller values of f are indicated by thedarker color.
1.
a)
b)
2.
a)
b)
28 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
3.
a)
b)
4.
a)
b)
5.
a)
12.3. REAL-VALUED FUNCTIONS OF SEVERAL VARIABLES 29
b)
6.
a)
b)
7.
30 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
The level surfaces are spheres. In the pictures, the outer sphere is shown partially in order to
show the inner sphere.
8.
The level surfaces are ellipsoids. In the pictures, the outer ellipsoid is shown partially in order
to show the inner ellipsoid.
9. The pictures show two level surfaces of f .
12.4. PARTIAL DERIVATIVES 31
10. The pictures show two level surfaces of f .
12.4 Partial Derivatives
1.∂
∂x
¡4x2 + 9y2
¢= 8x,
∂
∂y
¡4x2 + 9y2
¢= 18y
2.∂
∂x
¡6x2 − 5y2¢ = 12x, ∂
∂y
¡6x2 − 5y2¢ = −10y
3.∂
∂x
p2x2 + y2 =
∂
∂x
¡2x2 + y2
¢1/2=1
2
¡2x2 + y2
¢−1/2(4x) =
2xp2x2 + y2
,
∂
∂y
p2x2 + y2 =
∂
∂y
¡2x2 + y2
¢1/2=1
2
¡2x2 + y2
¢−1/2(2y) =
yp2x2 + y2
4.∂
∂r
¡r2 cos (θ)
¢= 2r cos (θ) ,
∂
∂θ
¡r2 cos (θ)
¢= −r2 sin (θ)
5.∂
∂xe−x
2−y2 = −2xe−x2−y2 , ∂
∂ye−x
2−y2 = −2ye−x2−y2
7.
∂
∂xln¡x2 + y2
¢=
Ãd
duln (u)
¯u=x2+y2
!µ∂
∂x
¡x2 + y2
¢¶=
µ1
x2 + y2
¶(2x) =
2x
x2 + y2,
32 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
∂
∂yln¡x2 + y2
¢=
Ãd
duln (u)
¯u=x2+y2
!µ∂
∂y
¡x2 + y2
¢¶=
µ1
x2 + y2
¶(2y) =
2y
x2 + y2,
8.
∂
∂r
³er
2
tan (θ)´= 2rer
2
tan (θ) ,∂
∂θ
³er
2
tan (θ)´= er
2
µ1
cos2 (θ)
¶=
er2
cos2 (θ)
9.
∂
∂xarctan
Ãyp
x2 + y2
!=
Ãd
duarctan (u)
¯u=y/√x2+y2
!̶
∂x
Ãyp
x2 + y2
!!
=
⎛⎜⎜⎝ 1
1 +y2
x2 + y2
⎞⎟⎟⎠µy ∂
∂x
¡x2 + y2
¢−1/2¶
=
µx2 + y2
x2 + 2y2
¶µy
µ−12
¡x2 + y2
¢−3/2(2x)
¶¶= − xy
¡x2 + y2
¢(x2 + 2y2) (x2 + y2)3/2
= − xy
(x2 + 2y2)px2 + y2
,
∂
∂yarctan
Ãyp
x2 + y2
!=
Ãd
duarctan (u)
¯u=y/√x2+y2
!̶
∂y
Ãyp
x2 + y2
!!
=
⎛⎜⎜⎝ 1
1 +y2
x2 + y2
⎞⎟⎟⎠⎛⎝px2 + y2 − y
³∂∂y
¡x2 + y2
¢1/2´x2 + y2
⎞⎠
=
µx2 + y2
x2 + 2y2
¶⎛⎝px2 + y2 − y³12
¡x2 + y2
¢−1/2(2y)
´x2 + y2
⎞⎠=
µx2 + y2
x2 + 2y2
¶Ãx2 + y2 − y2(x2 + y2)
3/2
!=
x2
(x2 + 2y2)px2 + y2
12.4. PARTIAL DERIVATIVES 33
10.
∂
∂xarccos
Ãxp
x2 + y2
!=
Ãd
duarccos (u)
¯u=x/√x2+y2
!̶
∂x
Ãxp
x2 + y2
!!
=
Ã− 1√
1− u2¯u=x/√x2+y2
!⎛⎜⎜⎜⎜⎝px2 + y2 − x
Ã2x
2px2 + y2
!x2 + y2
⎞⎟⎟⎟⎟⎠
=
⎛⎜⎜⎜⎜⎝− 1s1− x2
x2 + y2
⎞⎟⎟⎟⎟⎠Ãx2 + y2 − x2(x2 + y2)
3//2
!
= − y2sy2
x2 + y2(x2 + y2)3//2
= − y2
|y| (x2 + y2)
11.
∂
∂x
Ã1p
x2 + y2 + z2
!=
∂
∂x
¡x2 + y2 + z2
¢−1/2=
Ãd
duu−1/2
¯u=x2+y2+z2
!µ∂
∂x
¡x2 + y2 + z2
¢¶
=
Ã−12u−3/2
¯u=x2+y2+z2
!(2x)
= − x
(x2 + y2 + z2)3/2
Similarly,
∂
∂y
Ã1p
x2 + y2 + z2
!= − y
(x2 + y2 + z2)3/2,
∂
∂z
Ã1p
x2 + y2 + z2
!= − z
(x2 + y2 + z2)3/2
12.
∂
∂x
¡xyzex−y+2z
¢= yzex−y+2z + xyzex−y+2z,
∂
∂y
¡xyzex−y+2z
¢= xzex−y+2z − xyzex−y+2z,
∂
∂z
¡xyzex−y+2z
¢= xyex−y+2z + 2xyzex−y+2z
34 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
13.
∂
∂xarcsin
Ã1p
x2 + y2 + z2
!=
Ãd
duarcsin (u)
¯u=1/√x2+y2+z2
!̶
∂x
1px2 + y2 + z2
!
=
Ã1√1− u2
¯u=1/√x2+y2+z2
!Ã− x
(x2 + y2 + z2)3/2
!
=
⎛⎜⎜⎝ 1r1− 1
x2 + y2 + z2
⎞⎟⎟⎠Ã− x
(x2 + y2 + z2)3/2
!
=
à px2 + y2 + z2p
x2 + y2 + z2 − 1
!Ã− x
(x2 + y2 + z2)3/2
!= − xp
x2 + y2 + z2 − 1 (x2 + y2 + z2)14.
∂
∂ρ(ρ cos (ϕ) sin (θ)) = cos (ϕ) sin (θ) ,
∂
∂ϕ(ρ cos (ϕ) sin (θ)) = −ρ sin (ϕ) sin (θ) ,
∂
∂θ(ρ cos (ϕ) sin (θ)) = ρ cos (ϕ) cos (θ)
15.
a) We have
∂f
∂x(x, y) =
∂
∂x
px2 + y2 =
1
2px2 + y2
(2x) =xp
x2 + y2,
and∂f
∂y(x, y) =
∂
∂y
px2 + y2 =
1
2px2 + y2
(2y) =yp
x2 + y2.
Thus,∂f
∂x(3, 1) =
3√32 + 1
=3√10and
∂f
∂y(3, 1) =
1√32 + 1
=1√10
Therefore, the vector
i+∂f
∂x(3, 1)k = i+
3√10k
is tangential to C1 at (3, 1, f (3, 1)) =¡3, 1,√10¢.
The vector
j+∂f
∂y(3, 1)k = j+
1√10k
is tangential to C2 at¡3, 1,√10¢.
b) The line that is tangent to C1 at (3, 1, f (3, 1)) =¡3, 1,√10¢is parametrized by
L1 (u) =³3, 1,√10´+ u
µ1, 0,
3√10
¶=
µ3 + u, 1,
√10 +
3√10u
¶,
12.4. PARTIAL DERIVATIVES 35
i.e.,
x (u) = 3 + u,
y (u) = 1,
z (u) =√10 +
3
10
√10u,
where u is an arbitrary real number.Similarly, The line that is tangent to C1 at (3, 1, f (3, 1)) =
¡3, 1,√10¢is parametrized by
L2 (u) =³3, 1,√10´+ u
µ0, 1,
1√10
¶=
µ3, 1 + u,
√10 +
1√10u
¶, u ∈ R.
16.
a) We have∂f
∂x(x, y) =
∂
∂x
¡10− x2 − y2¢ = −2x
and∂f
∂y(x, y) =
∂
∂x
¡10− x2 − y2¢ = −2y.
Thus,∂f
∂x(2, 1) = −4 and ∂f
∂y(2, 1) = −2.
Therefore, the vector
i+∂f
∂x(2, 1)k = i− 4k
is tangential to C1 at (2, 1, f (2, 1)) = (2, 1, 51).The vector
j+∂f
∂y(2, 1)k = j− 2k
is tangential to C2 at (2, 1, 5) .
b) The line that is tangent to C1 at (2, 1, f (2, 1)) = (2, 1, 5) is parametrized by
L1 (u) = (2, 1, 5) + u (1, 0,−4) = (2, 1, 5) + (u, 0,−4u)= (2 + u, 1, 5− 4u) .
The line that is tangent to C2 at (2, 1, 5) is parametrized by
L2 (u) = (2, 1, 5) + u (0, 1,−2) = (2, 1, 5) + u (0, 1,−2)= (2, 1 + u, 5− 2u) .
17.
a) We have∂f
∂x(x, y) =
∂
∂x
³ex
2+y2´= 2xex
2+y2
and∂f
∂y(x, y) =
∂
∂x
³ex
2+y2´= 2yex
2+y2 .
36 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
Thus,∂f
∂x(1, 0) = 2e and
∂f
∂y(1, 0) = 0.
Therefore, the vector
i+∂f
∂x(1, 0)k = i+ 2ek
is tangential to C1 at (1, 0, f (1, 0)) = (1, 0, e).The vector
j+∂f
∂y(1, 0)k = j
is tangential to C2 at (1, 0, e) .
b) The line that is tangent to C1 at (1, 0, f (1, 0)) = (1, 0, e) is parametrized by
L1 (u) = (1, 0, e) + u (1, 0, 2e) = (1, 0, e) + (u, 0, 2eu)
= (1 + u, 0, e+ 2eu) , u ∈ R.The line that is tangent to C2 at (1, 0, e) is parametrized by
L2 (u) = (1, 0, e) + u (0, 1, 0) = (1, 0, e) + (0, u, 0)
= (1, u, e) , u ∈ R.
18.
a) We have∂f
∂x(x, y) =
∂
∂x
¡x2 − y2¢ = 2x
and∂f
∂y(x, y) =
∂
∂x
¡x2 − y2¢ = −2y.
Thus,∂f
∂x(3, 2) = 6 and
∂f
∂y(3, 2) = −4.
Therefore, the vector
i+∂f
∂x(3, 2)k = i+ 6k
is tangential to C1 at (3, 2, f (3, 2)) = (3, 2, 5).The vector
j+∂f
∂y(3, 2)k = j− 4k
is tangential to C2 at (3, 2, 5) .
b) The line that is tangent to C1 at (3, 2, f (3, 2)) = (3, 2, 5) is parametrized by
L1 (u) = (3, 2, 5) + u (1, 0, 6) = (3, 2, 5) + (u, 0, 6u)
= . (3 + u, 2, 5 + 6u) , u ∈ R.The line that is tangent to C2 at (2, 1, 5) is parametrized by
L2 (u) = (3, 2, 5) + u (0, 1,−4) = (3, 2, 5) + (0, u,−4u)= (3, 2 + u, 5− 4u) , u ∈ R.
12.4. PARTIAL DERIVATIVES 37
19.
∂f
∂x(x, y) =
∂
∂x
¡4x2 + 9y2
¢= 8x,
∂f
∂y(x, y) =
∂
∂7
¡4x2 + 9y2
¢= 18y,
∂2f
∂x2(x, y) =
∂
∂x(8x) = 8,
∂2f
∂x∂y(x, y) =
∂
∂x(18y) = 0
20.
∂f
∂x(x, y) =
∂
∂x
¡x2 + y2
¢−1/2= −1
2
¡x2 + y2
¢−3/2(2x) = − x
(x2 + y2)3/2
∂2f
∂y∂x(x, y) =
∂
∂y
³−x ¡x2 + y2¢−3/2´ = −x ∂
∂y
¡x2 + y2
¢−3/2= −x
µ−32
¶¡x2 + y2
¢−5/2(2y) =
3xy
(x2 + y2)5/2,
∂f
∂y(x, y) =
∂
∂y
¡x2 + y2
¢−1/2= −1
2
¡x2 + y2
¢−3/2(2y) = − y
(x2 + y2)3/2,
∂2f
∂y2(x, y) =
∂
∂y
Ã− y
(x2 + y2)3/2
!= (−1)
Ã1
(x2 + y2)3/2
!− y
µ∂
∂y
¡x2 + y2
¢−3/2¶= − 1
(x2 + y2)3/2− y
µ−32
¡x2 + y2
¢−5/2(2y)
¶= − 1
(x2 + y2)3/2+
3y2
(x2 + y2)5/2
=− ¡x2 + y2¢+ 3y2(x2 + y2)
5/2=−x2 + 2y2(x2 + y2)
5/2
21.∂f
∂x(x, y) =
∂
∂xe−x
2+y2 = −2xe−x2+y2 ,
∂2f
∂x2(x, y) =
∂
∂x
³−2xe−x2+y2
´= −2e−x2+y2 + 4x2e−x2+y2 ,
∂2f
∂y∂x(x, y) =
∂
∂y
³−2xe−x2+y2
´= −2x (2y) e−x2+y2 = −4xye−x2+y2
22.
∂f
∂y(x, y) =
∂
∂ysin³p
x2 − y2´
= cos³p
x2 − y2´Ã 1
2px2 − y2 (−2y)
!= − yp
x2 − y2 cos³p
x2 − y2´
38 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
∂2f
∂x∂y(x, y) =
∂
∂x
Ã− yp
x2 − y2 cos³p
x2 − y2´!
= −yµ
∂
∂x
¡x2 − y2¢−1/2¶ cos³px2 − y2´
− ypx2 − y2
µ∂
∂xcos³p
x2 − y2´¶
= −yµ1
2
¡x2 − y2¢−3/2 2x¶ cos³px2 − y2´
+yp
x2 − y2 sin³p
x2 − y2´ÃÃ 1
2px2 − y2 (2x)
!!=
xy
(x2 − y2)3/2cos³p
x2 − y2´+
xy
x2 − y2 sin³p
x2 − y2´
23.∂f
∂z(x, y, z) =
∂
∂z
¡xyzex−y+2z
¢= xyex−y+2z + 2xyzex−y+2z,
∂2f
∂x∂z(x, y, z) =
∂
∂x
¡xyex−y+2z + 2xyzex−y+2z
¢= yex−y+2z + xyex−y+2z + 2yzex−y+2z + 2xyzex−y+2z,= ex−y+2z (y + xy + 2yz + 2xyz)
∂2f
∂y∂z(x, y, z) =
∂
∂y
¡xyex−y+2z + 2xyzex−y+2z
¢= xex−y+2z − xyex−y+2z + 2xzex−y+2z − 2xyzex−y+2z= ex−y+2z (x− xy + 2xz − 2xyz)
24.∂f
∂θ(ρ,ϕ, θ) =
∂
∂θ(ρ cos (ϕ) sin (θ)) = ρ cos (ϕ) cos (θ) ,
∂2f
∂ϕ∂θ(ρ,ϕ, θ) =
∂
∂ϕ(ρ cos (ϕ) cos (θ)) = −ρ sin (ϕ) cos (θ) ,
∂2f
∂ρ∂θ(ρ,ϕ, θ) =
∂
∂ρ(ρ cos (ϕ) cos (θ)) = cos (ϕ) cos (θ)
25.
fy (x, y) =∂
∂yln¡x2 + 4y2
¢=
1
x2 + 4y2(8y) =
8y
x2 + 4y2.
fxy (x, y) =∂
∂x
µ8y
x2 + 4y2
¶= 8y
∂
∂x
¡x2 + 4y2
¢−1= 8y
³− ¡x2 + 4y2¢−2 (2x)´ = − 16xy
(x2 + 4y2)2
fx (x, y) =∂
∂xln¡x2 + 4y2
¢=
1
x2 + 4y2(2x) =
2x
x2 + 4y2,
12.5. LINEAR APPROXIMATIONS AND THE DIFFERENTIAL 39
fyx (x, y) =∂
∂y
µ2x
x2 + 4y2
¶= 2x
∂
∂y
¡x2 + 4y2
¢−1= 2x
³− ¡x2 + 4y2¢−2 (8y)´ = − 16xy
(x2 + 4y2).
Thus, fyx = fxy.
26.
fy (x, y) =∂
∂y
³x2yex
2−2y2´
= x2ex2−2y2 + x2y
³−4yex2−2y2
´= x2ex
2−2y2 − 4x2y2ex2−2y2 ,
fxy (x, y) =∂
∂x
³x2ex
2−2y2 − 4x2y2ex2−2y2´
= 2xex2−2y2 + x2
³2xex
2−2y2´− 8xy2ex2−2y2 − 4x2y2
³2xex
2−2y2´
= ex2−2y2 ¡2x+ 2x3 − 8xy2 − 8x3y2¢
fx (x, y) =∂
∂x
³x2yex
2−2y2´
= 2xyex2−2y2 + x2y (2x) ex
2−2y2
= 2xyex2−2y2 + 2x3yex
2−2y2 ,
fyx (x, y) =∂
∂y
³2xyex
2−2y2 + 2x3yex2−2y2
´= 2xex
2−2y2 + 2xy³−4yex2−2y2
´+ 2x3ex
2−2y2 + 2x3y³−4yex2−2y2
´= ex
2−2y2 ¡2x− 8xy2 + 2x3 − 8x3y2¢Thus, fyx = fxy.
12.5 Linear Approximations and the Differential
1.
a) We have
∂f
∂x(x, y) =
∂
∂x
¡x2 + y2
¢3/2=3
2
¡x2 + y2
¢1/2(2x) = 3x
px2 + y2,
∂f
∂y(x, y) = 3y
px2 + y2,
Therefore,∂f
∂x(3, 4) = 45,
∂f
∂y(3, 4) = 60, and f (3, 4) = 125.
Thus,
L (x, y) = 125 + 45 (x− 3) + 60(y − 4).b)
f (3.1, 3.9) ∼= L (3.1, 3.9)= 125 + 45 (0.1) + 60 (−0.1) = 123.5
40 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
c) According to a calculator, f (3.1, 3.9) ∼= 123. 652. The absolute error is|f (3.1, 3.9)− 123.5| ∼= 0.152.
2.
a)∂f
∂x(x, y) = −e−x sin (y) , ∂f
∂y(x, y) = e−x cos (y) .
Therefore,∂f
∂x(0,π/2) = −1 and ∂f
∂y(0,π/2) = 0, and f (0,π/2) = 1.
Thus,
L (x, y) = 1− x.b)
f (0.2,π/2 + 0.1) ∼= L (0.2,π/2 + 0.1) = 1− 0.2 = 0.8.c) According to a calculator, f (0.2,π/2 + 0.1) ∼= 0.814 641. The absolute error is
|f (0.2,π/2 + 0.1)− 0.8| ∼= 1.4× 10−23.
a)∂
∂xf (x, y) = − y
x2 + y2,
∂
∂yf (x, y) =
x
x2 + y2,
so that∂
∂xf³√3, 1´= −1
4, and
∂
∂yf³√3, 1´=
√3
4, and f
³√3, 1´=
π
6.
Therefore,
L (x, y) =π
6− 14
³x−√3´+
√3
4(y − 1) .
b)
f (1.8, 0.8) ∼= L (1.8, 0.8) = π
6− 14
³1.8−
√3´+
√3
4(0.8− 1) ∼= 0.420 009
c) According to a calculator f (1.8, 0.8) ∼= 0.418 224. The absolute error is|f (1.8, 0.8)− L (1.8, 0.8)| ∼= 1.8× 10−3
4.
a)∂
∂xf (x, y) = 2xex
2+y2 ,∂
∂yf (x, y) = 2yex
2+y2 .
Therefore,∂
∂xf (1, 0) = 2e,
∂
∂yf (1, 0) = 0, and f (1, 0) = e.
Thus,
L (x, y) = e+ 2e (x− 1) .b)
f (1.1,−0.2) ∼= L (1.1,−0.2) = e+ 2e (0.1) = 1.2e ∼= 3. 261 94c) According to a calculator f (1.1,−0.2) ∼= 3. 490 34. The absolute error is
|f (1.1,−0.2)− 1.2e| ∼= 0.23
12.5. LINEAR APPROXIMATIONS AND THE DIFFERENTIAL 41
5.
a)
∂f
∂x(x, y, z) =
xpx2 + y2 + z2
,∂f
∂y(x, y, z) =
ypx2 + y2 + z2
,
∂f
∂z(x, y, z) =
zpx2 + y2 + z2
.
Therefore,∂f
∂x(1, 2, 3) =
1√14,∂f
∂y(1, 2, 3) =
2√14,∂f
∂z(1, 2, 3) =
3√14.
and f (1, 2, 3) =√14.
Thus,
L (x, y, z) =√14 +
1√14(x− 1) + 2√
14(y − 2) + 3√
14(z − 3) .
b)
f (0.9, 2.2, 2.9) ∼= L (0.9, 2.2, 2.9)=√14 +
1√14(−0.1) + 2√
14(0.2) +
3√14(−0.1)
∼= 3. 741 66
c). According to a calculator f (0.9, 2.2, 2.9) ∼= f (0.9, 2.2, 2.9). The absolute error is
|f (0.9, 2.2, 2.9)− L (0.9, 2.2, 2.9)| ∼= 8× 10−3
6.
a)∂
∂xf (x, y) =
xpx2 + y2
,∂
∂yf (x, y) =
ypx2 + y2
Therefore,
df =xp
x2 + y2dx+
ypx2 + y2
dy.
b)
f (12.1, 4.9)− f (12, 5) ∼= df (12, 5, 0.1,−0.1)=12
13(0.1) +
5
13(−0.1) .
Therefore,
f (12.1, 4.9) ∼= f (12, 5) + 1213(0.1) +
5
13(−0.1)
= 13 +12
13(0.1) +
5
13(−0.1) ∼= 13. 053 8
c) According to a calculator f (12.1, 4.9) ∼= 13. 054 5. The absolute error is
|f (12.1, 4.9)− 13. 053 8| ∼= 1.5× 10−3
7.
42 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
a)∂
∂xf (x, y, z) =
yz
2√xyz
,∂
∂yf (x, y, z) =
xz
2√xyz
,∂
∂zf (x, y, z) =
xy
2√xyz
.
Therefore,
df =yz
2√xyz
dx+xz
2√xyz
dy +xy
2√xyz
dz.
b)
f (0.9, 2.9, 3.1)− f (1, 3, 3) ∼= df (1, 3, 3,−0.1,−0.1, 0.1)=
9
2 (3)(−0.1) + 3
2 (3)(−0.1) + 3
2 (3)(0.1) = −0.15
Therefore,
f (0.9, 2.9, 3.1) ∼= f (1, 3, 3)− 0.15 = 3− 0.15 = 2. 85c) According to a calculator f (0.9, 2.9, 3.1) ∼= 2. 844 47. The absolute error is
|f (0.9, 2.9, 3.1)− 2. 85| ∼= 5.5× 10−3
8.
a)∂f
∂x(x, y) =
2x
(x2 + y2)2+ 1
,∂f
∂y(x, y) =
2y
(x2 + y2)2+ 1
.
Therefore,
df =2x
(x2 + y2)2 + 1dx+
2y
(x2 + y2)2 + 1dy.
b)
f (0.1,−1.2)− f (0,−1) ∼= df (0,−1, 0.1,−0.2) = −22(−0.2) = 0.2.
Therefore,
f (0.1,−1.2) ∼= f (0,−1) + 0.2 = arctan (1) + 0.2 = π
4+ 0.2 ∼= 0.985 398
c) According to a calculator f (0.1,−1.2) ∼= 0.967 047. The absolute error i
|f (0.1,−1.2)− 0.985 398| ∼= 0.018
12.6 The Chain Rule
1.
a) If we set z = f (x, y), we have
∂z
∂x=
∂
∂x
px2 + y2 =
1
2px2 + y2
(2x) =xp
x2 + y2,
and∂z
∂y=
∂
∂y
px2 + y2 =
1
2px2 + y2
(2y) =yp
x2 + y2.
We havedx
dt=d
dt(sin (t)) = cos (t) and
dy
dt=d
dt(2 cos (t)) = −2 sin (t)
12.6. THE CHAIN RULE 43
Therefore,
d
dtf (x (t) , y (t)) =
dz
dt=
∂z
∂x
dx
dt+
∂z
∂y
dy
dt
=
Ãxp
x2 + y2
!cos (t) +
Ãyp
x2 + y2
!(−2 sin (t))
=sin (t) cos (t)− 4 cos (t) sin (t)q
sin2 (t) + 4 cos2 (t)= − 3 sin (t) cos (t)q
sin2 (t) + 4 cos2 (t)
b) We have
f (x (t) , y (t)) = f (sin (t) , 2 cos (t)) =
qsin2 (t) + 4 cos2 (t).
Therefore,
d
dtf (x (t) , y (t)) =
d
dt
qsin2 (t) + 4 cos2 (t)
=1
2qsin2 (t) + 4 cos2 (t)
(2 sin (t) cos (t)− 8 cos (t) sin (t))
= − 3 sin (t) cos (t)qsin2 (t) + 4 cos2 (t)
2.
a) If we set z = f (x, y), we have
∂z
∂x=
∂
∂xe−x
2+y2 = −2xe−x2+y2 ,
and∂z
∂y=
∂
∂ye−x
2+y2 = 2ye−x2+y2 .
We havedx
dt=d
dt(2t− 1) = 2 and dy
dt=d
dt(t+ 1) = 1.
Therefore,
d
dtf (x (t) , y (t)) =
dz
dt=
∂z
∂x
dx
dt+
∂z
∂y
dy
dt
=³−2xe−x2+y2
´(2) +
³2ye−x
2+y2´(1)
= e−x2+y2 (−4x+ 2y)
= e−(2t−1)2+(t+1)2 (−4 (2t− 1) + 2 (t+ 1))
= e6t−3t2
(6− 6t) .
b) We have
f (x (t) , y (t)) = f (2t− 1, t+ 1) = e−(2t−1)2+(t+1)2 = e6t−3t2 .Therefore,
d
dtf (x (t) , y (t)) =
d
dte6t−3t
2
= e6t−3t2
(6− 6t) .3.
44 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
a) If we set z = f (x), we havedz
dx=d
dxln (x) =
1
x.
We also have
∂x
∂u=
∂
∂u
µ1√
u2 + v2
¶=
Ã− 1
2 (u2 + v2)3/2
!(2u) = − u
(u2 + v2)3/2,
and
∂x
∂v=
∂
∂v
µ1√
u2 + v2
¶=
Ã− 1
2 (u2 + v2)3/2
!(2v) = − v
(u2 + v2)3/2.
Therefore,
∂
∂uf (x (u, v)) =
∂z
∂u=dz
dx
∂x
∂u=
µ1
x
¶Ã− u
(u2 + v2)3/2
!
=pu2 + v2
Ã− u
(u2 + v2)3/2
!= − u
u2 + v2
and
∂
∂vf (x (u, v)) =
∂z
∂v=dz
dx
∂x
∂v=
µ1
x
¶Ã− v
(u2 + v2)3/2
!
=pu2 + v2
Ã− v
(u2 + v2)3/2
!= − v
u2 + v2.
b) We have
f (x (u, v)) = f
µ1√
u2 + v2
¶= ln
³pu2 + v2
´.
Therefore.
∂
∂uf (x (u, v)) =
∂
∂uln
µ1√
u2 + v2
¶=
∂
∂u
³− ln
³pu2 + v2
´´= −
µ1√
u2 + v2
¶µu√
u2 + v2
¶= − u
u2 + v2,
and
∂
∂vf (x (u, v)) =
∂
∂vln
µ1√
u2 + v2
¶=
∂
∂v
³− ln
³pu2 + v2
´´= −
µ1√
u2 + v2
¶µv√
u2 + v2
¶= − v
u2 + v2.
4.
12.6. THE CHAIN RULE 45
a) If we set z = f (x) we have
dz
dx=d
dxsin¡x2¢= 2x cos
¡x2¢.
We have∂x
∂u=
∂
∂u(u− 4v) = 1 and ∂x
∂v=
∂
∂v(u− 4v) = −4.
Therefore,
∂
∂uf (x (u, v)) =
∂z
∂u=
dz
dx
∂x
∂u
=¡2x cos
¡x2¢¢(1)
= 2x cos¡x2¢= 2 (u− 4v) cos
³(u− 4v)2
´and
∂
∂vf (x (u, v)) =
∂z
∂v=
dz
dx
∂x
∂v=¡2x cos
¡x2¢¢(−4)
= −8x cos ¡x2¢= −8 (u− 4v) cos
³(u− 4v)2
´b) We have
f (u, v) = sin³(u− 4v)2
´.
Therefore,
∂
∂uf (x (u, v)) = cos
³(u− 4v)2
´(2 (u− 4v)) = 2 (u− 4v) cos
³(u− 4v)2
´,
∂
∂vf (x (u, v)) = cos
³(u− 4v)2
´(2 (u− 4v)) (−4) = −8 (u− 4v) cos
³(u− 4v)2
´.
5.
a) If we set z = f (x, y) we have
∂z
∂x=
∂
∂xarcsin
Ãyp
x2 + y2
!=
1s1− y2
x2 + y2
µy∂
∂x
¡x2 + y2
¢−1/2¶
=
px2 + y2√x2
µy
µ−12
¡x2 + y2
¢−3/2¶(2x)
¶= − y
x2 + y2,
and
∂z
∂y=
∂
∂yarcsin
Ãyp
x2 + y2
!=
1s1− y2
x2 + y2
⎛⎜⎜⎝px2 + y2 − y
µy√x2+y2
¶x2 + y2
⎞⎟⎟⎠=
px2 + y2√x2
Ãx2
(x2 + y2)3/2
!=
x
x2 + y2.
46 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
We also have
∂x
∂u=
∂
∂u(u cos (v)) = cos (v) ,
∂x
∂v=
∂
∂v(u cos (v)) = −u sin (v) ,
and∂y
∂u=
∂
∂u(u sin (v)) = sin (v) ,
∂y
∂v=
∂
∂v(u sin (v)) = u cos (v) .
Therefore,
∂
∂uf (x (u, v) , y (u, v)) =
∂z
∂u
=dz
dx
∂x
∂u+dz
dy
∂y
∂u
=
µ− y
x2 + y2
¶cos (v) +
µx
x2 + y2
¶sin (v)
=− (u sin (v)) cos (v) + (u cos (v)) sin (v)
u2 cos2 (v) + u2 sin2 (v)
= 0,
and
∂
∂vf (x (u, v) , y (u, v)) =
∂z
∂v
=dz
dx
∂x
∂v+dz
dy
∂y
∂v
=
µ− y
x2 + y2
¶(−u sin (v)) +
µx
x2 + y2
¶(u cos (v))
=u2 sin2 (v) + u2 cos2 (v)
u2 cos2 (v) + u2 sin2 (v)= 1.
b) We have
f (x (u, v) , y (u, v)) = f (u cos (v) , u sin (v))
= arcsin
⎛⎝ u sin (v)qu2 cos2 (v) + u2 sin2 (v)
⎞⎠= arcsin (sin (v)) = v.
Therefore,∂
∂uf (x (u, v) , y (u, v)) = 0 and
∂
∂vf (x (u, v) , y (u, v)) = 1.
6.
a) If we set z = f (x, y) we have
∂z
∂x=
∂
∂xarctan
³yx
´=
1
1 +³yx
´2 ³− yx2´ = x2
x2 + y2
³− yx2
´= − y
x2 + y2,
and∂z
∂y=
∂
∂yarctan
³yx
´=
1
1 +³yx
´2 µ 1x¶=
x2
x2 + y2
µ1
x
¶=
x
x2 + y2
12.6. THE CHAIN RULE 47
We also have
∂x
∂u=
∂
∂u(u+ 2v) = 1,
∂x
∂v=
∂
∂v(u+ 2v) = 2,
and
∂y
∂u=
∂
∂u(u− 2v) = 1, ∂y
∂v=
∂
∂v(u− 2v) = −2.
Therefore,
∂
∂uf (x (u, v) , y (u, v)) =
∂z
∂u
=dz
dx
∂x
∂u+dz
dy
∂y
∂u
=
µ− y
x2 + y2
¶(1) +
µx
x2 + y2
¶(1)
=x− yx2 + y2
=4v
2u2 + 8v2=
2v
u2 + 4v2
and
∂
∂vf (x (u, v) , y (u, v)) =
∂z
∂v
=dz
dx
∂x
∂v+dz
dy
∂y
∂v
=
µ− y
x2 + y2
¶(2) +
µx
x2 + y2
¶(−2)
= −2 (x+ y)x2 + y2
=−4u
2u2 + 8v2= − 2u
u2 + 4v2.
b) We have
f (x (u, v) , y (u, v)) = f (u+ 2v, u− 2v) = arctanµu− 2vu+ 2v
¶.
Therefore,
∂
∂uf (x (u, v) , y (u, v)) =
∂
∂uarctan
µu− 2vu+ 2v
¶=
1
1 +
µu− 2vu+ 2v
¶2Ã(u+ 2v)− (u− 2v)
(u+ 2v)2
!
=(u+ 2v)2
(u+ 2v)2+ (u− 2v)2
Ã4v
(u+ 2v)2
!=
4v
2u2 + 8v2=
2v
u2 + 4v2,
48 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
and
∂
∂vf (x (u, v) , y (u, v)) =
∂
∂varctan
µu− 2vu+ 2v
¶=
1
1 +
µu− 2vu+ 2v
¶2Ã−2 (u+ 2v)− 2 (u− 2v)
(u+ 2v)2
!
=(u+ 2v)2
(u+ 2v)2+ (u− 2v)2
Ã−4u
(u+ 2v)2
!=
−4u2u2 + 8v2
= − 2u
u2 + 4v2,
7. As in the text,
∂z
∂r= cos (θ)
∂z
∂x+ sin (θ)
∂z
∂y
∂z
∂θ= −r sin (θ) ∂z
∂x+ r cos (θ)
∂z
∂y.
Therefore,
µ∂z
∂r
¶2+1
r2
µ∂z
∂θ
¶2=
µcos (θ)
∂z
∂x+ sin (θ)
∂z
∂y
¶2+1
r2
µ−r sin (θ) ∂z
∂x+ r cos (θ)
∂z
∂y
¶2= cos2 (θ)
µ∂z
∂x
¶2+ 2 cos (θ) sin (θ)
µ∂z
∂x
¶µ∂z
∂y
¶+ sin2 (θ)
µ∂z
∂y
¶2+sin2 (θ)
µ∂z
∂x
¶2− 2 cos (θ) sin (θ)
µ∂z
∂x
¶µ∂z
∂y
¶+ cos2 (θ)
µ∂z
∂y
¶2=
¡cos2 (θ) + sin2 (θ)
¢µ∂z
∂x
¶2+¡cos2 (θ) + sin2 (θ)
¢µ∂z∂y
¶2=
µ∂z
∂x
¶2+
µ∂z
∂y
¶2.
8. We have
∂x
∂t= et cos (θ) ,
∂y
∂t= et sin (θ) ,
∂x
∂θ= −et sin (θ) , ∂y
∂θ= et cos (θ) .
Therefore,
∂z
∂t=
∂z
∂x
∂x
∂t+
∂z
∂y
∂y
∂t= et cos (θ)
∂z
∂x+ et sin (θ)
∂z
∂y,
∂z
∂θ=
∂z
∂x
∂x
∂θ+
∂z
∂y
∂y
∂θ= −et sin (θ) ∂z
∂x+ et cos (θ)
∂z
∂y.
12.6. THE CHAIN RULE 49
Thus,µ∂z
∂t
¶2+
µ∂z
∂θ
¶2=
µet cos (θ)
∂z
∂x+ et sin (θ)
∂z
∂y
¶2+
µ−et sin (θ) ∂z
∂x+ et cos (θ)
∂z
∂y
¶2= e2t
Ãcos2 (θ)
µ∂z
∂x
¶2+ 2 cos (θ) sin (θ)
∂z
∂x
∂z
∂y+ sin2 (θ)
µ∂z
∂y
¶2!
+e2t
Ãsin2 (θ)
µ∂z
∂x
¶2− 2 cos (θ) sin (θ) ∂z
∂x
∂z
∂y+ cos2 (θ)
µ∂z
∂y
¶2!
= e2t
õ∂z
∂x
¶2+
µ∂z
∂y
¶2!.
Therefore,
e−2t"µ
∂z
∂t
¶2+
µ∂z
∂θ
¶2#=
µ∂z
∂x
¶2+
µ∂z
∂y
¶2.
9.
a) Set w (x, t) = x+ at, so that u = f (w (x, t)). By the chain rule,
∂u
∂t=df
dw(w (x, t))
∂w
∂t=df
dw(w (x, t)) a = a
df
dw(w (x, t)) .
Therefore,
∂2u
∂t2= a
∂
∂t
µdf
dw(w (x, t))
¶= a
µd2f
dw2(w (x, t))
∂w
∂t
¶= a
d2f
dw2(w (x, t)) a = a2
d2f
dw2(x+ at)
Similarly,∂u
∂x=df
dw(w (x, t))
∂w
∂x=df
dw(w (x, t)) (1) =
df
dw(w (x, t))
and
∂2u
∂x2=
∂
∂x
µdf
dw(w (x, t))
¶=d2f
dw2(w (x, t))
∂w
∂x
=d2f
dw2(w (x, t)) (1) =
d2f
dw2(x− at)
Therefore,∂2u
∂t2= a2
∂2u
∂x2.
b) If f (w) = sin (w) and a = π/4 then
u (x, t) = f³x+
π
4t´= sin
³x+
π
4t´.
In particular,
u (x, 0) = sin (x) , u (x, 2) = sin³x+
π
2
´= cos (x) ,
u (x, 4) = sin (x+ π) = − cos (x)c)
50 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
sin(x)
-10 -5 5 10
-1.0
-0.5
0.5
1.0
x
y
cos(x)
-10 -5 5 10
-1
1
x
y
-cos(x)
-10 -5 5 10
-1
1
x
y
10.
a)
2z∂z
∂x− 2x = 0⇒ ∂z
∂x=x
z,
2z∂z
∂x− 2y = 0⇒ ∂z
∂y=y
z
b)
∂z
∂x
¯x=1,y=2,z=−3
= −13,∂z
∂y
¯x=1,y=2,z=−3
= −23.
Therefore, the tangent plane is the graph of the equation
z = −3− 13(x− 1)− 2
3(y − 2) .
1
yx
2
z
-3
11.
a)
2z∂z
∂x+ 2x = 0⇒ ∂z
∂x= −x
z,
2z∂z
∂x− 2y = 0⇒ ∂z
∂y=y
z
b)
∂z
∂x
¯x=3,y=6,z=6
= −36= −1
2,∂z
∂y
¯x=3,y=3,z=6
=6
6= 1.
Therefore, the tangent plane is the graph of the equation
z = 6− 12(x− 3) + (y − 6) .
12.7. DIRECTIONAL DERIVATIVES AND THE GRADIENT 51
z
6
3
y6 x
12.7 Directional Derivatives and the Gradient
1.
a)∂f
∂x(x, y) =
∂
∂x
¡4x2 + 9y2
¢= 8x and
∂f
∂y(x, y) =
∂
∂y
¡4x2 + 9y2
¢= 18y.
Therefore,
∇f (x, y) = 8xi+ 18yjb)
∇f (3, 4) = 24i+ 72j,and
||v|| = √4 + 1 =√5⇒ u =
1√5(−2, 1) =
µ− 2√
5,1√5
¶.
Therefore,
Duf (3, 4) = ∇f (3, 4) · u = (24i+ 72j) ·µ− 2√
5i+
1√5j
¶= − 48√
5+72√5=24√5
5
2.
a)∂f
∂x(x, y) =
∂
∂x
¡x2 − 4x− 3y2 + 6y + 1¢ = 2x− 4,
and∂f
∂y(x, y) =
∂
∂y
¡x2 − 4x− 3y2 + 6y + 1¢ = 6− 6y.
Therefore,
∇f (x, y) = (2x− 4) i+ (6− 6y) jb)
∇f (0, 0) = −4i+ 6j,and
||v|| = √1 + 1 =√2⇒ u =
1√2(1,−1) =
µ1√2,− 1√
2
¶.
Therefore,
Duf (0, 0) = ∇f (0, 0) · u = (−4i+ 6j) ·µ1√2i− 1√
2j
¶= − 4√
2− 6√
2= − 10√
2= −5
√2
52 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
3.
a)∂f
∂x(x, y) =
∂
∂xex
2−y2 = 2xex2−y2 and
∂f
∂y(x, y) =
∂
∂yex
2−y2 = −2yex2−y2 .
Therefore,
∇f (x, y) = 2xex2−y2i− 2yex2−y2jb)
∇f (2, 1) = 4e3i− 2e3j,and
||v|| =√10⇒ u =
1√10(−1, 3) =
µ− 1√
10,3√10
¶.
Therefore,
Duf (2, 1) = ∇f (2, 1) · u =¡4e3i− 2e3j¢ ·µ− 1√
10i+
3√10j
¶= − 4e
3
√10− 6e3√
10= −√10e3
4.
a)∂f
∂x(x, y) =
∂
∂x(sin (x) cos (y)) = cos (x) cos (y) ,
and∂f
∂y(x, y) =
∂
∂y(sin (x) cos (y)) = − sin (x) sin (y) .
Therefore,
∇f (x, y) = cos (x) cos (y) i− sin (x) sin (y) j.b)
∇f (π/3,π/4) = cos (π/3) cos (π/4) i− sin (π/3) sin (π/4) j
=
µ1
2
¶Ã√2
2
!i−
Ã√3
2
!Ã√2
2
!j =
√2
4i−√6
4j
and
||v|| = √4 + 9 =√13⇒ u =
1√13(2,−3) =
µ2√13,− 3√
13
¶.
Therefore,
Duf (π/3,π/4) = ∇f (π/3,π/4) · u =
Ã√2
4i−√6
4j
!·µ
2√13i− 3√
13j
¶=
√2
2√13+3√6
4√13=2√2 + 3
√6
4√13
5.
a)∂f
∂x(x, y, z) =
∂
∂x
¡x2 − y2 + 2z2¢ = 2x, ∂f
∂y(x, y, z) =
∂
∂y
¡x2 − y2 + 2z2¢ = −2y,
and∂f
∂z(x, y, z) =
∂
∂z
¡x2 − y2 + 2z2¢ = 4z.
12.7. DIRECTIONAL DERIVATIVES AND THE GRADIENT 53
Therefore,
∇f (x, y, z) = 2xi− 2yj+ 4zk.b)
∇f (1,−1, 2) = 2i+ 2j+ 8kand
||v|| =√3⇒ u =
1√3(1,−1, 1) =
µ1√3,− 1√
3,1√3
¶.
Therefore,
Duf (1,−1, 2) = ∇f (1,−1, 2) · u= (2i+ 2j+ 8k) ·
µ1√3i− 1√
3j+
1√3k
¶=
2√3− 2√
3+
8√3=
8√3
6.
a)
∂f
∂x(x, y, z) =
∂
∂x
¡x2 + y2 + z2
¢−1/2= −1
2
¡x2 + y2 + z2
¢−3/2(2x) = − x
(x2 + y2 + z2)3/2,
∂f
∂y(x, y, z) = − y
(x2 + y2 + z2)3/2,∂f
∂z(x, y, z) = − z
(x2 + y2 + z2)3/2
Therefore,
∇f (x, y, z) = − x
(x2 + y2 + z2)3/2i− y
(x2 + y2 + z2)3/2j− z
(x2 + y2 + z2)3/2k.
b)
∇f (2,−2, 1) = − 227i+
2
27j− 1
27k
and
||v|| =√26⇒ u =
1√26(3, 4, 1) =
µ3√26,4√26,1√26
¶.
Therefore,
Duf (2,−2, 1) = ∇f (2,−2, 1) · u=
µ− 227i+
2
27j− 1
27k
¶·µ
3√26i+
4√26j+
1√26k
¶= − 6
27√26+
8
27√26− 1
27√26=
1
27√26
7.
a) We have
∂f
∂x(x, y) =
∂
∂x
¡x2 + y2
¢−1/2= −1
2
¡x2 + y2
¢−3/2(2x) = − x
(x2 + y2)3/2,
∂f
∂y(x, y) =
∂
∂y
¡x2 + y2
¢−1/2= −1
2
¡x2 + y2
¢−3/2(2y) = − y
(x2 + y2)3/2.
54 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
Therefore,
∇f (x, y) = − x
(x2 + y2)3/2i− y
(x2 + y2)3/2j
Thus,
v = ∇f (2, 3) = − 2
133/2i− 3
133/2j
The corresponding rate of increase of f is
||v|| =sµ
2
133/2
¶2+
µ3
133/2
¶2=1
13
b)
w = −∇f (2, 3) = 2
133/2i+
3
133/2j
The corresponding rate of decrease of f is 1/13.
8.
a) We have
∂f
∂x(x, y) =
∂
∂xln³p
x2 + y2´=1
2
∂
∂xln¡x2 + y2
¢=1
2
µ1
x2 + y2
¶(2x) =
x
x2 + y2,
∂f
∂y(x, y) =
∂
∂yln³p
x2 + y2´=
y
x2 + y2.
Therefore,
∇f (x, y) = x
x2 + y2i+
y
x2 + y2j
Thus,
v = ∇f (3, 4) = 3
25i+
4
25j
The corresponding rate of increase of f is
||v|| =sµ
3
25
¶2+
µ4
25
¶2=1
5.
b)
w = −∇f (3, 4) = − 325i− 4
25j
The corresponding rate of decrease of f is 1/5.
9.
a) We have
∂f
∂x(x, y) =
∂
∂xex
2−y2 = 2xex2+y2 ,
∂f
∂y(x, y) =
∂
∂yex
2−y2 = −2yex2−y2 .
Therefore,
∇f (x, y) = 2xex2−y2i− 2yex2−y2j.Since
σ³π6
´=³2 cos
³π6
´, 2 sin
³π6
´´= 2
Ã√3
2,1
2
!=³√3, 1´,
12.7. DIRECTIONAL DERIVATIVES AND THE GRADIENT 55
and
∇f³√3, 1´= 2√3e2i− 2e2j = 2
√3e2i− 2e2j.
We havedσ
dt(t) = −2 sin (t) i+ 2 cos (t) j⇒ dσ
dt
³π6
´= −i+
√3j.
Therefore,
d
dtf (σ (t))
¯t=π/6
= ∇f³σ³π6
´´· dσdt
³π6
´=
³2√3e2i− 2e2j
´·³−i+
√3j´
= −2√3e2 − 2
√3e2 = −4
√3e.
b) We have ¯¯dσ
dt
³π6
´¯¯=¯¯−i+
√3j¯¯=√4 = 2,
so that
u =1
2
dσ
dt
³π6
´=1
2
³−i+
√3j´= −1
2i+
√3
2j
is the unit vector in the tangential direction. Therefore,
Ddσ/dtf (σ (π/6)) = Ddσ/dtf³√3, 1´
= ∇f³√3, 1´· u
=³2√3e2i− 2e2j
´·Ã−12i+
√3
2j
!= −
√3e2 −
√3e2 = −2
√3e2.
10.
a) We have
∂f
∂x(x, y) =
∂
∂xarctan
Ãyp
x2 + y2
!=
1
1 +y2
x2 + y2
µ∂
∂x
¡y¡x2 + y2
¢¢−1/2¶
=x2 + y2
x2 + 2y2y
µ−12
¡x2 + y2
¢−3/2¶(2x)
= − xy
(x2 + 2y2)px2 + y2
,
and
∂f
∂y(x, y) =
∂
∂yarctan
Ãyp
x2 + y2
!=
1
1 +y2
x2 + y2
⎛⎜⎜⎝px2 + y2 − y
µy√x2+y2
¶x2 + y2
⎞⎟⎟⎠=
x2 + y2
x2 + 2y2
Ãx2
(x2 + y2)3/2
!
=x2
(x2 + 2y2)px2 + y2
,
56 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
Therefore,
∇f (x, y) = − xy
(x2 + 2y2)px2 + y2
i+x2
(x2 + 2y2)px2 + y2
j.
Since
σ (2) =
µ−35,4
5
¶,
and
∇fµ−35,4
5
¶= 2√3e2i− 2e2j = 2
√3e2i− 2e2j.
We havedσ
dt(t) = −2 sin (t) i+ 2 cos (t) j⇒ dσ
dt
³π6
´= −i+
√3j.
Therefore,
d
dtf (σ (t))
¯t=π/6
= ∇f³σ³π6
´´· dσdt
³π6
´=
³2√3e2i− 2e2j
´·³−i+
√3j´
= −2√3e2 − 2
√3e2 = −4
√3e.
b) We have ¯¯dσ
dt
³π6
´¯¯=¯¯−i+
√3j¯¯=√4 = 2,
so that
u =1
2
dσ
dt
³π6
´=1
2
³−i+
√3j´= −1
2i+
√3
2j
is the unit vector in the tangential direction. Therefore,
Ddσ/dtf (σ (π/6)) = Ddσ/dtf³√3, 1´
= ∇f³√3, 1´· u
=³2√3e2i− 2e2j
´·Ã−12i+
√3
2j
!= −
√3e2 −
√3e2 = −2
√3e2.
11.
a) Let f (x, y) = 2x2 + 3y2. We have
∇f (x, y) = 4xi+ 6yj.Therefore,
∇f (2, 3) = 8i+ 18jis orthogonal to the curve f (x, y) = 35 at (2, 3).
b) The tangent line is the graph of the equation
8 (x− 2) + 18 (y − 3) = 0
12.
a) Let f (x, y) = x2 − y2. Then,∇f (x, y) = 2xi− 2yj.
12.7. DIRECTIONAL DERIVATIVES AND THE GRADIENT 57
Therefore,
∇f³3,√5´= 6i− 2
√5j
is orthogonal to the curve f (x, y) = 4 at¡3,√5¢.
b) The tangent line is the graph of the equation
6 (x− 3)− 2√5³y −√5´= 0.
13.
a) Let
f (x, y) = e25−x2−y2 .
Then,
∇f (x, y) = −2xe25−x2−y2i− 2ye25−x2−y2j,so that
∇f (3, 4) = −6i− 8jis orthogonal to the curve f (x, y) = 1 at (3, 4).
b) The tangent line is the graph of the equation
−6 (x− 3)− 8 (y − 4) = 0.14.
a) Let f (x, y, z) = z − x2 + y2. We have∇f (x, y, z) = −2xi+ 2yj+ k
Therefore
∇f (4, 3, 7) = −8i+ 6j+ kis orthogonal to the surface at (4, 3, 7).b) The plane that is tangent to the surface at (4, 3, 7) is the graph of the equation
−8 (x− 4) + 6 (y − 3) + (z − 7) = 0.15.
a) Let f (x, y, z) = x2 − y2 + z2. We have∇f (x, y, z) = 2xi− 2yj+ 2zk
Therefore
∇f (2, 2, 1) = 4i− 4j+ 2kis orthogonal to the surface at (2, 2, 1).b) The plane that is tangent to the surface at (2, 2, 1) is the graph of the equation
4 (x− 2)− 4 (y − 2) + 2 (z − 1) = 0.16.
a) Let f (x, y, z) = x2 − y2 − z2. We have∇f (x, y, z) = 2xi− 2yj− 2zk
Therefore
∇f (3, 2, 2) = 6i− 4j− 4k
58 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
is orthogonal to the surface at (3, 2, 2).b) The plane that is tangent to the surface at (3, 2, 2) is the graph of the equation
6 (x− 3)− 4 (y − 2)− 4 (z − 2) = 0.17.
Let f (x, y, z) = x− sin (y) cos (z). We have∇f (x, y, z) = i− cos (y) cos (z) j+ sin (y) sin (z)k
Therefore
∇f (1,π/2, 0) = iis orthogonal to the surface at (1,π/2, 0).b) The plane that is tangent to the surface at (1,π/2, 0) is the graph of the equation
x− 1 = 0⇔ x = 1.
12.8 Local Maxima and Minima
1.∂f
∂x(x, y) = 2x+ y + 1,
∂f
∂y(x, y) = −2y + x− 1.
Therefore, ∂xf (x, y) = 0 and ∂yf (x, y) = 0⇔2x+ y + 1 = 0,
−2y + x− 1 = 0
Thus, the critical point is (−1/5,−3/5).We have
∂2f
∂x2= 2,
∂2f
∂y2= −2 and ∂2f
∂y∂x= 1
Therefore,
D =∂2f
∂x2∂2f
∂y2−µ
∂2f
∂y∂x
¶2= (2) (−2)− 1 = −4− 1 < 0.
Thus, f has a saddle point at (−1/5,−3/5).
0
1
10
5
z
-3
-2
-1x
-1
0
1
-5
0
y -2
-3
2.∂f
∂x(x, y) = 2x− y, ∂f
∂y(x, y) = 2y − x+ 1.
Therefore, ∂xf (x, y) = 0 and ∂yf (x, y) = 0⇔2x− y = 0,
2y − x+ 1 = 0
12.8. LOCAL MAXIMA AND MINIMA 59
Thus, the critical point is (−1/3,−2/3).We have
∂2f
∂x2= 2,
∂2f
∂y2= 2 and
∂2f
∂y∂x= −1
Therefore,
D =∂2f
∂x2∂2f
∂y2−µ
∂2f
∂y∂x
¶2= (2) (2) + 1 = 5 > 0,
and ∂2xxf = 2 > 0. Therefore, f has a local (and absolute) minimum at (−1/3,−2/3).
15
10
z5
0
10
-3-3
-1
y
01
x
-1-2 -2
3.
∂f
∂x(x, y) = 2x+ 2y,
∂f
∂y(x, y) = 2y + 2x.
Therefore, ∂xf (x, y) = 0 and ∂yf (x, y) = 0⇔2x+ 2y = 0,
2y + 2x = 0
Thus, any point on the line y = −x is a critical point.We have
∂2f
∂x2= 2,
∂2f
∂y2= 2 and
∂2f
∂y∂x= 2
Therefore,
D =∂2f
∂x2∂2f
∂y2−µ
∂2f
∂y∂x
¶2= (2) (2)− ¡22¢ = 0..
We expect that the quadratic function f attains its absolute maximum or minimum on the line
y = −x. Indeed,f (x, y) = x2 + y2 + 2xy − 10
= (x+ y)2 − 10,so that f (x, y) ≥ −10 for each (x, y), and f (x, y) = −10 iff y = −x.
-10
20
10
0
z
3
3
2
2
1
1
-2
0
0
yx
-1-1-2
-3 -3
60 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
4.∂f
∂x(x, y) = 2x+ 3y,
∂f
∂y(x, y) = 2y + 3x− 3.
Therefore, ∂xf (x, y) = 0 and ∂yf (x, y) = 0⇔2x+ 3y = 0,
2y + 3x− 3 = 0
Thus, the critical point is (9/5,−6/5).We have
∂2f
∂x2= 2,
∂2f
∂y2= 2 and
∂2f
∂y∂x= 3
Therefore,
D =∂2f
∂x2∂2f
∂y2−µ
∂2f
∂y∂x
¶2= (2) (2)− 32 = 4− 9 < 0.
Thus, f has a saddle point at (−9/5,−6/5).
10
30
z20
0
-3
-2-2
-1 0
0
1
1
y
x-1
5.
∂f
∂x(x, y) = 2x− 3y + 5, ∂f
∂y(x, y) = −3x− 2 + 12y.
Therefore, ∂xf (x, y) = 0 and ∂yf (x, y) = 0⇔2x− 3y + 5 = 0,
−3x+ 12y − 2 = 0
Thus, the critical point is (−18/5,−11/15).We have
∂2f
∂x2= 2,
∂2f
∂y2= 12 and
∂2f
∂y∂x= −3
Therefore,
D =∂2f
∂x2∂2f
∂y2−µ
∂2f
∂y∂x
¶2= (2) (12)− 9 = 15 > 0,
and ∂2xxf = 2 > 0. Therefore, f has a local (and absolute) minimum at (−18/5,−11/15).
100
120
80
60z
40
20
02 1 0 -1
y
-2
x
-2 0-4-6-3 -4
12.8. LOCAL MAXIMA AND MINIMA 61
6.∂f
∂x(x, y) = 3− 3x2 − 3y2, ∂f
∂y(x, y) = −6xy
Thus, ∂xf (x, y) = 0 and ∂yf (x, y) = 0⇔3− 3x2 − 3y2 = 0,
−6xy = 0
From the second equation, x = 0 or y = 0. If x = 0, then
3− 3y2 = 0⇔ y2 = 1⇔ y = ±1.Therefore, (0, 1) and (0,−1) are critical points.If y = 0 then
3− 3x2 = 0⇔ x2 = 1⇔ x = ±1.Therefore, (1, 0) and (−1,−0) are critical points.We have
∂2f
∂x2= −6x, ∂2f
∂y2= −6x and ∂2f
∂y∂x= −6y
Therefore,
D (x, y) =∂2f
∂x2∂2f
∂y2−µ
∂2f
∂y∂x
¶2= (−6x) (−6x)− (−6y)2 = 36 ¡x2 − y2¢ .
(x, y) D (x, y) fxx (x, y) critical point
(1, 0) 36 −6 local maximum
(−1, 0) 36 6 local minimum
(0, 1) −36 0 saddle point
(0,−1) −36 0 saddle point
-10
z 0
10
20
-20
2
2
1
-1 x
1
0
y-1
0-2 -2
7.
∂f
∂x= −4x3 − 4y, ∂f
∂y(x, y) = −4y3 − 4x.
Therefore, ∂xf (x, y) = 0 and ∂yf (x, y) = 0⇔x3 + y = 0⇔ y = −x3y3 + x = 0⇔ x = −y3.
If we set y = −x3 in the second equation we obtain
x = − ¡−x3¢3 = x9 ⇔ x− x9 = 0⇔ x¡1− x8¢ = 0.
62 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
Therefore, x = 0, 1 or −1. Since y = −x3, we have y = 0, −1 and 1, respectively. Thus, thecritical points are (0, 0), (1,−1) and (−1, 1).We have
∂2f
∂x2= −12x2, ∂2f
∂y2= −12y2 and ∂2f
∂y∂x= −4
Therefore,
D (x, y) =∂2f
∂x2∂2f
∂y2−µ
∂2f
∂y∂x
¶2=¡−12x2¢ ¡−12y2¢− (−4)2 = 144x2y2 − 16
(x, y) D (x, y) fxx (x, y) critical point
(0, 0) −16 0 saddle point
(1,−1) 128 −12 local maximum
(−1, 1) 128 −12 local maximum
1
y
0
-1-1
x0
1
-20
0
z-10
8.
f (x, y) = x3 − 12xy + 8y3
∂f
∂x= 3x2 − 12y, ∂f
∂y(x, y) = 24y2 − 12x
Therefore, ∂xf (x, y) = 0 and ∂yf (x, y) = 0⇔
x2 − 4y = 0,
2y2 − x = 0.
From the second equation x = 2y2. Substituting in the first equation,¡2y2¢2 − 4y = 0⇔ y4 − y = 0⇔ y
¡y3 − 1¢ = 0.
Thus, y = 0 or y = 1. The corresponding values of x are 0 and 1. Therefore, the critical pointsare (0, 0) and (2, 1).We have
∂2f
∂x2= 6x,
∂2f
∂y2= 48y and
∂2f
∂y∂x= −12
Therefore,
D (x, y) =∂2f
∂x2∂2f
∂y2−µ
∂2f
∂y∂x
¶2= (6x) (48y)− (−12)2 = 288xy − 144.
(x, y) D (x, y) fxx (x, y) critical point
(0, 0) −144 0 saddle point
(2, 1) 432 12 local minimum
12.9. ABSOLUTE EXTREMA AND LAGRANGE MULTIPLIERS 63
0
4
2
xy
02
-100
-2-2
z 0
100
12.9 Absolute Extrema and Lagrange Multipliers
1. We have f (x, y) = x+ y and we set g (x, y) = x2+ y2, so that we will determine the extremaof f (x, y) subject to the constraint g (x, y) = 4 (i.e., the extrema of f on the circle of radius 2centered at the origin).
We have
∇f (x, y) = (1, 1) and ∇g (x, y) = (2x, 2y) .Therefore,
∇f (x, y) = λ∇g (x, y)⇔ 1 = 2λx and 1 = 2λy.
Thus, we need to solve the following system of equations:
1 = 2λx,
1 = 2λy,
x2 + y2 = 4
(the last equation is the constraint equation, g (x, y) = 4).From the first two equations,
x =1
2λand y =
1
2λ.
We substitute these expressions in the last equation:µ1
2λ
¶2+
µ1
2λ
¶2= 4 ⇒ 1
4λ2+
1
4λ2= 4
⇒ 2 = 16λ2
⇒ λ = ± 1√8= ± 1
2√2.
Therefore,
x = y = ± 1
2λ= ± 1
2
µ1
2√2
¶ = ±√2.
Thus, the necessary conditions for the extrema of f subject to the constraint x2 + y2 = 4 are
satisfied at the points¡√2,√2¢and
¡−√2,−√2¢. We havef³√2,√2´= 2√2 and f
³−√2,−√2´= −2
√2.
Therefore, the maximum value of f on the circle x2 + y2 = 4 is f¡√2,√2¢= 2√2 and the
minimum value is f¡−√2,−√2¢ = −2√2.
64 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
2. We have f (x, y) = 3x − 4y and we set g (x, y) = x2 + y2, so that we will determine theextrema of f (x, y) subject to the constraint g (x, y) = 9 (i.e., the extrema of f on the circle ofradius 3 centered at the origin).
We have
∇f (x, y) = (3,−4) and ∇g (x, y) = (2x, 2y) .Therefore,
∇f (x, y) = λ∇g (x, y)⇔ 3 = 2λx and − 4 = 2λy.Thus, we need to solve the following system of equations:
3 = 2λx,
−4 = 2λy,
x2 + y2 = 9
(the last equation is the constraint equation, g (x, y) = 9).From the first two equations,
x =3
2λand y = − 4
2λ.
We substitute these expressions in the last equation:µ3
2λ
¶2+
µ4
2λ
¶2= 9 ⇒ 9
4λ2+16
4λ2= 9
⇒ 25
9= 4λ2
⇒ λ = ±56
Therefore,
x =3
2λ=
3
2
µ5
6
¶ =9
5and y = − 4
2λ= − 4
2
µ5
6
¶ = −125,
or
x =3
2λ= − 3
2
µ5
6
¶ = −95and y = − 4
2λ=
4
2
µ5
6
¶ =12
5
Thus, the necessary conditions for the extrema of f subject to the constraint x2 + y2 = 9 are
satisfied at the points µ9
5,−12
5
¶and
µ−95,12
5
¶We have
f
µ9
5,−12
5
¶=7
5and f
µ−95,12
5
¶= −47
5.
Therefore, the maximum value of f on the circle x2 + y2 = 9 is
f
µ9
5,−12
5
¶=7
5,
and the mimimum value on x2 + y2 = 9 is
f
µ−95,12
5
¶= −47
5.
12.9. ABSOLUTE EXTREMA AND LAGRANGE MULTIPLIERS 65
3. We have f (x, y) = xy and we set g (x, y) = 4x2 + y2, so that we will determine the extremaof f (x, y) subject to the constraint g (x, y) = 8 (i.e., the extrema of f on an elllipse that iscentered at the origin).
We have
∇f (x, y) = (y, x) and ∇g (x, y) = (8x, 2y) .Therefore,
∇f (x, y) = λ∇g (x, y)⇔ y = 8λx and x = 2λy.
Thus, we need to solve the following system of equations:
y = 8λx,
x = 2λy,
4x2 + y2 = 8
(the last equation is the constraint equation, g (x, y) = 16).From the first equation, y = 8λx. We replace y in the second equation:
x = 16λ2x
We cannot have x = 0: Then y = 0, and (0, 0) does not satisfy the constraint equation.Therefore,
16λ2 = 1⇒ λ = ±14.
and we set y = 8λx in the last equation:
4x2 + 64λ2x2 = 8.
Since 16λ2 = 1,4x2 + 4x2 = 8⇒ 8x2 = 8⇒ x2 = 1⇒ x = ±1.
If λ = 1/4 and x = 1 then
y = 8λx = 8
µ1
4
¶(1) = 2,
If λ = −1/4 and x = 1 theny = 8λx = 8
µ−14
¶(1) = −2,
If λ = 1/4 and x = −1 theny = 8λx = 8
µ1
4
¶(−1) = −2,
If λ = −1/4 and x = −1 then
y = 8λx = 8
µ−14
¶(−1) = 2.
Therefore, the critical points are
(1, 2) , (1,−2) , (−1,−2) , (−1, 2) .
We have
f (1, 2) = 2, f (1,−2) = −2, f (−1,−2) = 2, f (−1, 2) = −2.Therefore, the minimum value of f (x, y) subject to 4x2 + y2 = 8 is -−2, the maximum value is
2.
66 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
4. We have f (x, y) = x + y2 and we set g (x, y) = 2x2 + y2, so that we will determine theextrema of f (x, y) subject to the constraint g (x, y) = 1 (i.e., the extrema of f on an elllipsethat is centered at the origin).
We have
∇f (x, y) = (1, 2y) and ∇g (x, y) = (4x, 2y) .Therefore,
∇f (x, y) = λ∇g (x, y)⇔ 1 = 4λx and 2y = 2λy.
Thus, we need to solve the following system of equations:
4λx = 1,
2 (1− λ) y = 0,
2x2 + y2 = 1
(the last equation is the constraint equation, g (x, y) = 1).From the last equation, we have y = 0 or λ = 1. If y = 0 then
2x2 = 1⇒ x = ± 1√2.
If y 6= 0 then λ = 1. From the first equation
x =1
4λ=1
4.
Substituting in the last equation,
2
µ1
4
¶2+ y2 = 1⇒ y2 = 1− 1
8=7
8⇒ y = ±
r7
8.
Therefore, the critical points areµ1√2, 0
¶,
µ− 1√
2, 0
¶,
Ã1
4,
r7
8
!,
Ã1
4,−r7
8
!We have
f
µ1√2, 0
¶=
1√2, f
µ− 1√
2, 0
¶= − 1√
2, f
Ã1
4,±r7
8
!=9
8
Therefore, the minimum value of f (x, y) subject to 2x2+y2 = 1 is -−1/√2, the maximum valueis 9/8.
5. The critical point of f in the interior of D is (0, 0), and f (0, 0) = 0. In order to find thecritical point of f subject to x2 + y2 = 4, we set g (x, y) = x2 + y2, and apply the technique ofthe technique of Lagrange multipliers. We have
∇f (x, y) = (2x, 4y) and ∇g (x, y) = (2x, 2y) .Therefore,
∇f (x, y) = λ∇g (x, y)⇔ 2x = 2λx and 4y = 2λy.
Thus, we need to solve the following system of equations:
2x = 2λx ⇔ (λ− 1)x = 04y = 2λy ⇔ (λ− 2) y = 0
x2 + y2 = 4
12.9. ABSOLUTE EXTREMA AND LAGRANGE MULTIPLIERS 67
If λ = 1 then y = 0 and x = ±2. Thus, (2, 0) and (−2, 0) are a critical points.If x = 0 then y = ±2. Thus, (0, 2) and (0,−2) are critical point. We have
f (±2, 0) = 4, f (0,±2) = 8.Therefore, the minimum value of f in D is 0, and its maximum value in D is 8.
6. The critical point of f in the interior of D is (0, 0), and f (0, 0) = 0. In order to find thecritical point of f subject to x2 + 2y2 = 1, we set g (x, y) = x2 + 2y2, and apply the techniqueof the technique of Lagrange multipliers. We have
∇f (x, y) = (y, x) and ∇g (x, y) = (2x, 4y) .Therefore,
∇f (x, y) = λ∇g (x, y)⇔ y = 2λx and x = 4λy.
Thus, we need to solve the following system of equations:
y = 2λx
x = 4λy
x2 + 2y2 = 1
We cannot have λ = 0: In that case x = 0 and y = 0, so that the constraint equation is notsatisfied.
We have
x = 4λy = 4λ (2λx) = 8λ2x,
so that ¡8λ2 − 1¢x = 0.
We cannot have x = 0. Therefore,
8λ2 − 1 = 0⇒ λ = ± 1√8.
Therefore
y = 2λx = ± 2√8x = ± 1√
2x.
Thus,
x2 + 2
µ1
2x2¶= 1⇒ 2x2 = 1⇒ x = ± 1√
2.
Therefore,
y = ±12.
Thus, the critical points on x2 + 2y2 = 1 areµ1√2,1
2
¶.
µ1√2,−12
¶,
µ− 1√
2,1
2
¶,
µ− 1√
2,−12
¶We have
f
µ1√2,1
2
¶=
√2
4, f
µ1√2,−12
¶= −√2
4
f
µ− 1√
2,1
2
¶= −
√2
4, f
µ− 1√
2,−12
¶=
√2
4
Therefore, the maximum value of f in D is −√2/4 and its maximum value in D is√2/4.
68 CHAPTER 12. FUNCTIONS OF SEVERAL VARIABLES
Chapter 13
Multiple Integrals
13.1 Double Integrals Over Rectangles
1. We have Z x=3
x=0
¡x2 + 3xy2
¢dx =
1
3x3 + 3
x2
2y2¯x=3x=0
= 9 +27
2y2
Therefore, Z y=2
y=1
µZ x=3
x=0
¡x2 + 3xy2
¢dx
¶dy =
Z y=2
y=1
µ9 +
27
2y2¶dy
= 9y +9
2y3¯21
=81
2
2. We have Z y=π/3
y=π/4
x sin (y) dy = −x cos (y)|y=π/3y=π/4
= −x cos³π3
´+ x cos
³π4
´=
Ã−12+
√2
2
!x =
x
2
³√2− 1
´Therefore,
Z x=1
x=0
ÃZ y=π/3
y=π/4
x sin (y) dy
!dx =
Z x=1
x=0
x
2
³√2− 1
´dx
=
√2− 14
x2
¯¯1
0
=
√2− 14
3. We have Z x=3
x==1
exyydx = exy|31 = e3y − ey.
69
70 CHAPTER 13. MULTIPLE INTEGRALS
Therefore, Z y=4
y=2
µZ x=3
x==1
exyydx
¶dy =
Z y=4
y=2
¡e3y − ey¢ dy
=1
3e3y − ey
¯42
=1
3e12 − e4 − 1
3e6 + e2
4. We set u = 1 + y2 so that du = 2ydy. Thus,Z y=3
y=1
xyp1 + y2dy = x
Z y=3
y=1
yp1 + y2dy
=x
2
Zu=10u=2 u
1/2du
=x
2
Ã2
3u3/2
¯102
!=x
3
³103/2 − 23/2
´.
Z x=2
x=0
µZ y=3
y=1
xyp1 + y2dy
¶dx =
Z x=2
x=0
x
3
³103/2 − 23/2
´dx
=103/2 − 23/2
6x2¯20
=2¡103/2 − 23/2¢
3
5. Z ZD
xy2
x2 + 1dA =
Z x=1
x=0
µZ y=2
y=−2
xy2
x2 + 1dy
¶dx
=
Z x=1
x=0
x
x2 + 1
µZ y=2
y=−2y2dy
¶dx
=
µZ x=1
x=0
x
x2 + 1dx
¶µZ y=2
y=−2y2dy
¶=
Ã1
2ln¡x2 + 1
¢¯10
!Ã1
3y3¯2−2
!
=1
2ln (2)
µ16
3
¶=8
3ln (2)
6. Z ZD
xyex2ydA =
Z y=2
y=1
µZ 1
x=0
xyex2ydx
¶dy
=
Z y=2
y=1
Ã1
2ex
2y
¯x=1x=0
!dy
=1
2
Z y=2
y=1
(ey − 1) dy
=1
2
³ey − y|21
´=1
2
¡e2 − 1− e¢
13.1. DOUBLE INTEGRALS OVER RECTANGLES 71
7. Z ZD
x2
1 + y2dA =
Z y=1
y=0
µZ x=1
x=0
x2
1 + y2dx
¶dy
=
Z y=1
y=0
1
1 + y2
Ãx3
3
¯10
!dy
=1
3
³arctan (y)|10
´=1
3arctan (1) =
π
12.
8.Z ZD
y cos (x+ y) dA =
Z y=π/2
y=0
y
ÃZ x=π/3
x=0
cos (x+ y) dx
!dy
=
Z y=π/2
y=0
y³sin (x+ y)|x=π/3x=0
´dy
=
Z y=π/2
y=0
y³sin³π3+ y
´− sin (y)
´dy
=
Z y=π/2
y=0
y sin³π3+ y
´dy −
Z y=π/2
y=0
y sin (y) dy
=
Z u=5π/6
u=π/3
³u− π
3
´sin (u) du−
Z y=π/2
y=0
y sin (y) dy
=π
3cos (u)
¯u=5π/6u=π/3
+
Z y=5π/6
y=π/3
y sin (y) dy −Z y=π/2
y=0
y sin (y) dy
=π
3cos
µ5π
6
¶− π
3cos³π3
´+
Z y=5π/6
y=π/3
y sin (y) dy −Z y=π/2
y=0
y sin (y) dy
= −π√3
6− π
6+
Z y=5π/6
y=π/3
y sin (y) dy −Z y=π/2
y=0
y sin (y) dy
We set u = y and dv = sin (y) dy so that
du = dy and v = − cos (y) .
Therefore Zy sin (y) dy =
Zudv = uv −
Zvdu
= −y cos (y) +Zcos (y) dy
= −y cos (y) + sin (y)
Thus, Z y=5π/6
y=π/3
y sin (y) dy = −y cos (y) + sin (y)|5π/6π/3
= −5π6cos
µ5π
6
¶+ sin
µ5π
6
¶+
π
3cos³π3
´− sin
³π3
´=
1
6π +
5
12
√3π − 1
2
√3 +
1
2,
72 CHAPTER 13. MULTIPLE INTEGRALS
Z y=π/2
y=0
y sin (y) dy = −y cos (y) + sin (y)|π/20 = 1
Therefore,Z ZD
y cos (x+ y) dA = −π√3
6− π
6+
Z y=5π/6
y=π/3
y sin (y) dy −Z y=π/2
y=0
y sin (y) dy
= −π√3
6− π
6+1
6π +
5
12
√3π − 1
2
√3 +
1
2− 1
=1
4
√3π − 1
2
√3− 1
2
13.2 Double Integrals Over Non-Rectangular Regions
1. We have Z √y0
xy2dx = y2Z √y0
xdx = y2
Ãx2
2
¯√y0
!
= y2³y2
´=y3
2.
Therefore, Z y=4
y=0
Z x=√y
x=0
xy2dxdy =
Z 4
0
y3
2dy =
y4
8
¯40
=44
8= 32
2. We have Z cos(θ)
0
esin(θ)dr = esin(θ)Z cos(θ)
0
dr = esin(θ) cos (θ) .
Therefore, Z θ=π/2
θ=0
Z r=cos(θ)
r=0
esin(θ)drdθ =
Z π/2
0
esin(θ) cos (θ) dθ.
We set u = sin (θ) so that du = cos (θ) dθ. Thus,Z π/2
0
esin(θ) cos (θ) dθ =
Z sin(π/2)
sin(0)
eudu =
Z 1
0
eudu
= eu|10 = e− 1.
3.
2
4
x
y
We have y = x2 and y = 2x if
x2 − 2x = 0⇔ x (x− 2) = 0⇔ x = 0 or x = 2.
13.2. DOUBLE INTEGRALS OVER NON-RECTANGULAR REGIONS 73
Thus, the graphs intersect at (0, 0) and (2, 4).Z ZD
4x3ydA =
Z x=2
x=0
Z y=2x
y=x24x3ydydx.
We have Z y=2x
y=x24x3ydy = 4x3
Z y=2x
y=x2ydy
= 4x3
Ã1
2y2¯2xx2
!= 2x3
¡4x2 − x4¢ .
Therefore, Z x=2
x=0
Z y=2x
y=x24x3ydydx =
Z 2
0
2x3¡4x2 − x4¢ dx
=
Z 2
0
¡8x5 − 2x7¢ dx
= 8
µx6
6
¶− 2
µx8
8
¶¯20
=4
3
¡26¢− 1
4
¡28¢=64
3
4.
4
16
x
y
We have Z ZD
y√xdA =
Z x=4
x=0
Z y=x2
y=0
y√xdydx,
and Z y=x2
y=0
y√xdy =
√x
Z y=x2
y=0
ydy
=√x
Ãy2
2
¯x20
!=
√x
2
¡x4¢=1
2x9/2.
Therefore, Z x=4
x=0
Z y=x2
y=0
y√xdydx =
Z 4
0
1
2x9/2dx
=1
2
µx11/2
11/2
¶¯40
=411/2
11=211
11.
74 CHAPTER 13. MULTIPLE INTEGRALS
5.
1
1
x
y
Z ZD
y2exydA =
Z y=1
y=0
Z x=y
x=0
y2exydxdy.
We have Z x=y
x=0
y2exydx = y
Z x=y
x=0
yexydx.
We set u = xy so that du = ydx. Therefore,Z x=y
x=0
yexydx =
Z y2
0
eudu = ey2 − 1.
Thus, Z y=1
y=0
Z x=y
x=0
y2exydxdy =
Z 1
0
y³ey
2 − 1´dy =
Z 1
0
yey2
dy −Z 1
0
ydy
=
Z 1
0
yey2
dy − 12
We set u = y2 so that du = 2ydy. Therefore,Z 1
0
yey2
dy =1
2
Z 1
0
eudu =1
2(e− 1) .
Thus, Z y=1
y=0
Z x=y
x=0
y2exydxdy =1
2(e− 1)− 1
2=1
2e− 1.
6.
x
y
Z ZD
y2 sin¡x2¢dA =
Z x=√π
x=0
Z y=x1/3
y=−x1/3y2 sin
¡x2¢dydx.
13.2. DOUBLE INTEGRALS OVER NON-RECTANGULAR REGIONS 75
We have Z y=x1/3
y=−x1/3y2 sin
¡x2¢dy = sin
¡x2¢ Z y=x1/3
y=−x1/3y2dy
= sin¡x2¢⎛⎝ y3
3
¯x1/3−x1/3
⎞⎠= sin
¡x2¢µ23x
¶=2
3x sin
¡x2¢.
Thus, Z x=√π
x=0
Z y=x1/3
y=−x1/3y2 sin
¡x2¢dydx =
Z x=√π
x=0
2
3x sin
¡x2¢dx.
We set u = x2 so that du = 2xdx. Therefore,Z x=√π
x=0
2
3x sin
¡x2¢dx =
1
3
Z u=π
u=0
sin (u) du
=1
3(− cos (x)|π0 ) =
2
3
7.
y
-2
01
2
0
1
x
-1
0
2z
4
6
-1 0 1
1
x
y
Let R be the region in the xy-plane that is between y = x2 and y = 1. The volume of D isZ ZR
¡x2 + y2 + 1
¢dA =
Z x=1
x=−1
Z y=1
y=x2
¡x2 + y2 + 1
¢dydx
=
Z x=1
x=−1
Ãx2y +
y3
3+ y
¯y=1y=x2
!dx
=
Z x=1
x=−1
µx2 +
1
3+ 1− x4 − x
6
3− x2
¶dx
=
Z x=1
x=−1
µ4
3− x4 − x
6
3
¶dx
=4
3x− x
5
5− x
7
21
¯1−1=38
35+38
35=76
35
76 CHAPTER 13. MULTIPLE INTEGRALS
8.
1.0
0.5
1.0
0.5
y x0.0 0.0
-2
z 0
2
Let R be the square [0, 1]× [0, 1] in the xy-plane. The volume of D is
Z ZR
(ex + ey) dA =
Z x=1
x=0
Z y=1
y=0
(ex + ey) dydx
=
Z x=1
x=0
³exy + ey|y=1y=0
´dx
=
Z x=1
x=0
(ex + e− 1) dx
= ex + (e− 1)x|10 = e+ (e− 1)− 1 = 2e− 2.
9.
02
1
6
z
4
x
2
00
3
y
21
2
3
x
y
13.2. DOUBLE INTEGRALS OVER NON-RECTANGULAR REGIONS 77
Let R be the shaded triangle. The volume of D isZ ZR
(6− 3x− 2y) dA =
Z x=2
x=0
Z y=3−3x/2
y=0
(6− 3x− 2y) dydx
=
Z x=2
x=0
³6y − 3xy − y2 ¯3−3x/2
0
´dx
=
Z x=2
x=0
Ã6
µ3− 3x
2
¶− 3x
µ3− 3x
2
¶−µ3− 3x
2
¶2!dx
=
Z x=2
x=0
µ9
4(x− 2)2
¶dx
=
Z u=0
u=−2
9
4u2du =
9
12u3¯0−2=9
12
¡23¢= 6
10.
a)
3
1
x
y
b) Z y=1
y=0
Z 3
x=3y
ex2
dxdy =
Z x=3
x=0
Z y=x/3
y=0
ex2
dydx
=
Z x=3
x=0
ex2
ÃZ y=x/3
y=0
dy
!dx
=
Z x=3
x=0
x
3ex
2
dx.
We set u = x2 so that du = 2xdx. Thus,Z x=3
x=0
x
3ex
2
dx =1
6
Z 9
u=0
eudu =1
6
¡e9 − 1¢ .
11.
a)
78 CHAPTER 13. MULTIPLE INTEGRALS
b) Z y=√π/2
y=0
Z x=√π/2
x=y
cos¡x2¢dxdy =
Z x=√π/2
x=0
Z y=x
y=0
cos¡x2¢dydx
=
Z x=√π/2
x=0
cos¡x2¢µZ y=x
y=0
dy
¶dx
=
Z x=√π/2
x=0
cos¡x2¢xdx.
We set u = x2 so that du = 2xdx. Thus,Z x=√π/2
x=0
cos¡x2¢xdx =
1
2
Z π/4
0
cos (u) du
=1
2
³sin (u)|π/40
´=1
2
³sin³π4
´− sin (0)
´=
√2
4
12.
b)Z y=1
y=0
Z π/2
x=arcsin(y)
cos (x)p1 + cos2 (x)dxdy =
Z x=π/2
x=0
Z y=sin(x)
y=0
cos (x)p1 + cos2 (x)dydx
=
Z x=π/2
x=0
cos (x)p1 + cos2 (x)
ÃZ y=sin(x)
y=0
dy
!dx
=
Z x=π/2
x=0
cos (x)p1 + cos2 (x) sin (x) dx
We set u = cos (x) so that du = − sin (x) dx. Thus,Z x=π/2
x=0
cos (x)p1 + cos2 (x) sin (x) dx = −
Z u=0
u=1
up1 + u2du
=
Z u=1
u=0
up1 + u2du.
If we set v = 1 + u2 then dv = 2udu. Thus,Z u=1
u=0
up1 + u2du =
1
2
Z v=2
v=1
v1/2dv
=1
2
µ2
3v3/2
¶¯21
=1
3
³√8− 1
´.
13.3. DOUBLE INTEGRALS IN POLAR COORDINATES: 79
13.3 Double Integrals in Polar Coordinates:
1.
a)
4x
4
y
b) Z ZD
xydA =
Z θ=π/2
θ=0
Z r=4
r=0
r cos (θ) r sin (θ) rdrdθ
=
Z θ=π/2
θ=0
cos (θ) sin (θ)
µZ r=4
r=0
r3dr
¶dθ
=
Z θ=π/2
θ=0
cos (θ) sin (θ)
Ãr4
4
¯r=4r=0
!dθ
= 64
Z θ=π/2
θ=0
cos (θ) sin (θ) dθ.
We set u = sin (θ) so that du = cos (θ) dθ. Thus,
64
Z θ=π/2
θ=0
cos (θ) sin (θ) dθ = 64
Z 1
0
udu = 64
Ãu2
2
¯10
!= 32.
2.
a)
-2 2
2
b) Z ZD
sin¡x2 + y2
¢dA =
Z θ=π
θ=0
Z 2
r=0
sin¡r2¢rdrdθ
=
ÃZ θ=π
θ=0
dθ
!µZ 2
r=0
sin¡r2¢rdr
¶= π
Z 2
r=0
sin¡r2¢rdr.
80 CHAPTER 13. MULTIPLE INTEGRALS
We set u = r2 so that du = 2rdr. Thus,
π
Z 2
r=0
sin¡r2¢rdr =
π
2
Z 4
u=0
sin (u) du =π
2
³− cos (u)|40
´=
π
2(1− cos (4)) .
3.
a)
3
-3
3
x
y
b) Z ZD
p9− x2 − y2dA =
Z θ=π/2
θ=−π/2
Z 3
r=0
p9− r2rdrdθ
=
ÃZ θ=π/2
θ=−π/2dθ
!µZ 3
r=0
p9− r2rdr
¶= π
Z 3
r=0
p9− r2rdr.
We set u = 9− r2 so that du = −2rdr. Thus,
π
Z r=3
r=0
p9− r2rdr = −π
2
Z 0
9
√udu
=π
2
Ã2
3u3/2
¯90
!= π
µ1
3
¶(27) = 9π.
4.
a)
-2 -1 1 2
1
2
x
y
b) Z ZD
e−x2−y2dA =
Z θ=π
θ=0
Z r=2
r=1
e−r2
rdrdθ
= π
Z r=2
r=1
e−r2
rdr
= π
Ã−12e−r
2
¯21
!=
π
2
¡e−1 − e−4¢
5.
13.3. DOUBLE INTEGRALS IN POLAR COORDINATES: 81
a)
1 2
1
2
x
y
b) Z ZD
arctan³yx
´dA =
Z θ=π/4
θ=0
Z r=2
r=1
θrdrdθ
=
ÃZ θ=π/4
θ=0
θdθ
!µZ r=2
r=1
rdr
¶
=
Ãθ2
2
¯π/40
!Ãr2
2
¯21
!=1
4
µπ2
16
¶(3) =
3π2
64.
6.
a)
-0.5 0.5
-0.5
0.5
x
y
b) We have
r = sin (2θ) = 0 and 0 < θ ≤ π
2if 2θ = π ⇔ θ =
π
2.
The area inside one loop isZ θ=π/2
θ=0
Z sin(2θ)
r=0
rdrdθ =
Z θ=π/2
θ=0
Ã1
2r2¯sin(2θ)r=0
!dθ
=1
2
Z θ=π/2
θ=0
sin2 (2θ) dθ
=1
4
Z π/2
0
(1− cos (4θ)) dθ
=1
4
Ãθ − 1
4sin (4θ)
¯π/20
!=
1
4
³π2
´=
π
8.
7.
a)
82 CHAPTER 13. MULTIPLE INTEGRALS
1 2 3
-1
1
x
y
b) We have
1 + cos (θ) = 3 cos (θ) if 2 cos (θ) = 1⇔ cos (θ) =1
2.
The only such angle between 0 and π/2 is π/3. By symmetry, the area of D is
2
ÃZ π/2
θ=π/3
Z r=1+cos(θ)
r=3 cos(θ)
rdrdθ +
Z θ=π
θ=π/2
Z r=1+cos(θ)
r=0
rdrdθ
!.
We haveZ π/2
θ=π/3
Z r=1+cos(θ)
r=3cos(θ)
rdrdθ =
Z π/2
θ=π/3
Ãr2
2
¯1+cos(θ)3 cos(θ)
!dθ
=1
2
Z π/2
θ=π/3
¡1 + 2 cos (θ)− 8 cos2 (θ)¢ dθ
=1
2
Z π/2
θ=π/3
µ1 + 2 cos (θ)− 8
µ1 + cos (2θ)
2
¶¶dθ
= −32θ + sin (θ)− sin (2θ)
¯π//2π/3
=
µ−3π4+ 1
¶−Ãπ
2+
√3
2−√3
2
!= −π
4+ 1,
and Z θ=π
θ=π/2
Z r=1+cos(θ)
r=0
rdrdθ =
Z θ=π
θ=π/2
Ã1
2r2¯1+cos(θ)0
!dθ
=1
2
Z θ=π
θ=π/2
(1 + cos (θ))2 dθ
=1
2
Z θ=π
θ=π/2
¡1 + 2 cos (θ) + cos2 (θ)
¢dθ
=1
2
Z θ=π
θ=π/2
µ1 + 2 cos (θ) +
1 + cos (2θ)
2
¶dθ
=1
2
Ã3
2θ + 2 sin (θ) +
1
4sin (2θ)
¯ππ/2
!
=1
2
µ3π
2− 3π4− 2¶=3π
8− 1.
13.3. DOUBLE INTEGRALS IN POLAR COORDINATES: 83
Therefore, the area of D is
2
ÃZ π/2
θ=π/3
Z r=1+cos(θ)
r=3 cos(θ)
rdrdθ +
Z θ=π
θ=π/2
Z r=1+cos(θ)
r=0
rdrdθ
!= 2
µ−π4+ 1 +
3π
8− 1¶
= 2³π8
´=
π
4.
8. The volume of D is Z ZR
px2 + y2dA,
where R is the disk that is inside the circle x2+y2 = 4, so that R is the disk of radius 2 centeredat the origin. Using polar coordinates,Z Z
R
px2 + y2dA =
Z θ=2π
θ=0
Z r=2
r=0
(r) rdrdθ
=
Z θ=2π
θ=0
Z r=2
r=0
r2drdθ
=
ÃZ θ=2π
θ=0
dθ
!µZ r=2
r=0
r2dr
¶
= 2π
Ãr3
3
¯20
!= 2π
µ8
3
¶=16π
3.
9. By symmetry, the volume of D is
2
Z ZR
p16− x2 − y2dA,
where R is the annular region between the circles x2 + y2 = 4 and x2 + y2 = 16. Thus,
2
Z ZR
p16− x2 − y2dA = 2
Z θ=2π
θ=0
Z r=4
r=2
p16− r2rdrdθ
= 2
ÃZ θ=2π
θ=0
dθ
!µZ r=4
r=2
p16− r2rdr
¶= 4π
Z r=4
r=2
p16− r2rdr.
We set u = 16− r2 so that du = −2rdr. Therefore,
4π
Z r=4
r=2
p16− r2rdr = −2π
Z u=0
u=12
u1/2du
= −2πÃ2
3u3/2
¯012
!=4π
3123/2.
10.
a)
-3
3
x
y
84 CHAPTER 13. MULTIPLE INTEGRALS
b) Z 3
−3
Z √9−x20
sin¡x2 + y2
¢dydx =
Z θ=π
θ=0
Z r=3
r=0
sin¡r2¢rdrdθ
=
ÃZ θ=π
θ=0
dθ
!µZ r=3
r=0
sin¡r2¢rdr
¶= π
Z r=3
r=0
sin¡r2¢rdr.
We set u = r2 so that du = 2rdr. Thus,
π
Z r=3
r=0
sin¡r2¢rdr =
π
2
Z 9
u=0
sin (u) du =π
2
³− cos (u)|90
´=
π
2(− cos (9) + 1)
11.
a) We have
x =p2− y2 ⇒ x2 + y2 = 2.
This is the equation of a circle of radius√2 centered at the origin. If y = 1 then x =
√2. The
polar coordinates of (1, 1) are r =√2 and θ = π/4
b) We have θ = π/4 on the line y = x. Thus,
Z y=1
y=0
Z x=√2−y2
x=y
xdxdy =
Z θ=π/4
θ=0
Z √2r=0
r cos (θ) rdrdθ
=
ÃZ θ=π/4
θ=0
cos (θ) dθ
!ÃZ √2r=0
r2dr
!
=³sin (θ)|π/40
´Ã 13r3¯√20
!
=
√2¡√2¢3
6=4
6=2
3.
13.4 Applications of Double Integrals
1. The mass of the plate is
13.4. APPLICATIONS OF DOUBLE INTEGRALS 85
m (D) =
Z ZD
ρ (x, y) dA =
Z x=4
x=0
Z y=2
y=0
(1 + x+ y) dydx
=
Z 4
0
(2x+ 4) dx = 32
The moment of the plate with respect to the y-axis is
My (D) =
Z ZD
xρ (x, y) dxdy =
Z x=4
x=0
Z y=2
y=0
x (1 + x+ y) dydx
=
Z 4
0
2x (x+ 2) dx =224
3
The moment of the plate with respect to the x-axis is
Mx (D) =
Z ZD
yρ (x, y) dxdy =
Z 4
0
Z 2
0
y (1 + x+ y) dydx
=
Z 4
0
µ2x+
14
3
¶dx =
104
3
Therefore, the x-coordinate of the center of mass is
x =My (D)
m (D)=
224
332
=7
3∼= 2.33
The y-coordinate of the center of mass is
y =Mx (D)
m (D)=
104
332
=13
12∼= 1. 083
2. The mass of the plate is
m (D) =
Z ZD
ρ (x, y) dA =
Z ZD
³81−
px2 + y2
´dA.
We transform to polar coordinates:Z ZD
³81−
px2 + y2
´dA =
Z θ=π
θ=0
Z r=3
r=0
(81− r) rdrdθ
= 2π
Z 3
r=0
¡81r − r2¢ dr = 711π
The moment of the plate with respect to the y-axis is
My (D) =
Z ZD
xρ (x, y) dA =
Z ZD
x³81−
px2 + y2
´dA.
We transform to polar coordinates:Z ZD
x³81−
px2 + y2
´dA =
Z θ=π
θ=0
Z r=3
r=0
r cos (θ) (81− r) rdrdθ
=
ÃZ θ=π
θ=0
cos (θ) dθ
!µZ r=3
r=0
¡81r2 − r3¢ dr¶
= (0)
µ2835
4
¶= 0.
86 CHAPTER 13. MULTIPLE INTEGRALS
The moment of the plate with respect to the x-axis is
Mx (D) =
Z ZD
yρ (x, y) =
Z ZD
y³81−
px2 + y2
´dA.
We transform to polar coordinates:Z ZD
y³81−
px2 + y2
´dA =
Z θ=π
θ=0
Z r=3
r=0
r sin (θ) (81− r) rdrdθ
=
ÃZ θ=π
θ=0
sin (θ) dθ
!µZ r=3
r=0
¡81r2 − r3¢ dr¶
= (2)
µ2835
4
¶=2835
2.
Therefore, the x-coordinate of the center of mass is
x =My (D)
m (D)= 0.
The y-coordinate of the center of mass is
y =Mx (D)
m (D)=
2835
2711π
=315
158π∼= 0.634.
3. The moment of inertia of the plate about the x-axis is
Ix =
Z ZD
y2ρ (x, y) dxdy =
Z ZD
y2ρ0dxdy = ρ0
Z ZD
y2dxdy.
We transform to polar coordinates:
ρ0
Z ZD
y2dxdy = ρ0
Z θ=2π
θ=0
Z r=r0
r=0
r2 sin2 (θ) rdrdθ
= ρ0
ÃZ θ=2π
θ=0
sin2 (θ) dθ
!µZ r=r0
r=0
r3dr
¶= ρ0 (π)
µ1
4r40
¶=
π
4ρ0r
40
The moment of inertia of the plate about the y-axis is
Iy =
Z ZD
x2ρ (x, y) dxdy =
Z ZD
x2ρ0dxdy = ρ0
Z ZD
x2dxdy.
We transform to polar coordinates:
ρ0
Z ZD
x2dxdy = ρ0
Z θ=2π
θ=0
Z r=r0
r=0
r2 cos2 (θ) rdrdθ
= ρ0
ÃZ θ=2π
θ=0
cos2 (θ) dθ
!µZ r=r0
r=0
r3dr
¶= ρ0 (π)
µ1
4r40
¶=
π
4ρ0r
40.
13.4. APPLICATIONS OF DOUBLE INTEGRALS 87
The moment of inertia of the plate about the origin is
I0 = Ix + Iy =π
4ρ0r
40 +
π
4ρ0r
40 =
π
2ρ0r
40.
4. The moment of inertia of the plate about the x-axis is
Ix =
Z ZD
y2ρ (x, y) dxdy =
Z ZD
y2³81−
px2 + y2
´dxdy.
We transform to polar coordinates:
Z ZD
y2³4−
px2 + y2
´dxdy =
Z θ=π
θ=0
Z r=3
r=0
r2 sin2 (θ) (4− r) rdrdθ
=
ÃZ θ=π
θ=0
sin2 (θ) dθ
!µZ r=3
r=0
¡4r3 − r4¢ dr¶
=
µ1
2π
¶µ162
5
¶= 16.2π
The moment of inertia of the plate about the y-axis is
Iy =
Z ZD
x2ρ (x, y) dxdy =
Z ZD
x2³81−
px2 + y2
´dxdy
We transform to polar coordinates:
Z ZD
x2³81−
px2 + y2
´dxdy =
Z θ=π
θ=0
Z r=3
r=0
r2 cos2 (θ) (4− r) rdrdθ
=
ÃZ θ=π
θ=0
cos2 (θ) dθ
!µZ r=3
r=0
¡4r3 − r4¢ dr¶
=
µ1
2π
¶µ162
5
¶= 16.2π
The moment of inertia of the plate about the origin is
I0 = Ix + Iy = 16.2π + 16.2π = 32.4π
5. Since X and Y are independent, their joint density function is
f (x, y) = f1 (x) f2 (y) =
½112e−−x/6e−y/2 if x ≥ 0 and y ≥ 0,0 otherwise.
Therefore, the probability that X + Y < 8 isZ ZD
1
12e−x/6e−y/2dxdy,
88 CHAPTER 13. MULTIPLE INTEGRALS
where D is the triangular region in the first quadrant below the line x+ y = 8. We have
Z ZD
1
12e−−x/6e−y/2dxdy =
Z x=8
x=0
Z 8−x
y=0
1
12e−−x/6e−y/2ydx
=1
12
Z x=8
x=0
e−x/6µZ 8−x
y=0
e−y/2dy¶dx
=1
12
Z x=8
x=0
e−x/6³2− 2ex/2−4
´dx
=1
12
Z x=8
x=0
³2e−x/6 − 2ex/3−4
´dx
=1
12
³6e−4 − 18e−4/3 + 12
´=
1
2e−4 − 3
2e−4/3 + 1 ∼= 0.613 762.
6. The density functions of X and Y are
f1 (x) =1
0.2√2πe−(x−3)
2/0.08 and f2 (y) =1
0.1√2πe−(y−5)
2/0.02,
respectively. Therefore,
P (2.5 < X < 3.5 and 4.5 < Y < 5.5)
=
Z y=5.5
y=4.5
Z x=3.5
x=2.5
f1 (x) f2 (y) dxdy
=
µZ y=5.5
y=4.5
f2 (y) dy
¶µZ x=3.5
x=2.5
f1 (x) dx
¶=
µZ y=5.5
y=4.5
1
0.1√2πe−(y−5)
2/0.02dy
¶µZ x=3.5
x=2.5
1
0.2√2πe−(x−3)
2/0.08dx
¶∼= (0.999 999 ) (0.987 581 ) ∼= 0.987 58.
13.5 Triple Integrals
1. The surfaces intersect when
x2 + y2 = 18− x2 − y2 ⇔ x2 + y2 = 9.
This is a circle of radius 3 centered at the origin. The volume in question is
Z ZR
ÃZ z=18−x2−y2
z=x2+y2dz
!dxdy
13.5. TRIPLE INTEGRALS 89
where R is the disk that is enclosed by the circle x2 + y2 = 9. Let’s use polar coordinates:
Z ZR
ÃZ z=18−x2−y2
z=x2+y2dz
!dxdy =
Z θ−2π
θ=0
Z r=3
r=0
ÃZ z=18−r2
z=r2dz
!rdrdθ
=
Z θ−2π
θ=0
Z r=3
r=0
¡18− 2r2¢ rdrdθ
= 2π
Z r=3
r=0
¡18r − 2r3¢ dr
= 2π
Ã9r2 − 1
2r4¯30
!
= 2π
µ81
2
¶= .81π.
2. The volume in question is
Z ZR
µZ z=1−x−y
z=−10dz
¶dxdy,
where R is the disk that is enclosed by the circle of radius 2 centered at the origin. Let’s use
polar coordinates:
Z ZR
µZ z=1−x−y
z=−10dz
¶dxdy =
Z θ=2π
θ=0
Z r−2
r−0
ÃZ z=1−r(cos(θ)+sin(θ))
z=−10dz
!rdrdθ
=
Z θ=2π
θ=0
Z r−2
r−0
¡11r − r2 cos (θ)− r2 sin (θ)¢ drdθ
=
Z θ=2π
θ=0
Ã11
2r2 − 1
3r3 cos (θ)− 1
3r3 sin (θ)
¯r=2r=0
!dθ
=
Z θ=2π
θ=0
µ22− 8
3cos (θ)− 8
3sin (θ)
¶dθ
= 22θ − 83sin (θ) +
8
3cos (θ)
¯2π0
= 44π.
3.
Z Z ZD
x2dxdydz =
Z z=1
z=0
Z y=1
y=0
Z x=1
x=0
x2dxdydz
=
Z z=1
z=0
Z y=1
y=0
Ã1
3x3¯10
!dydz
=1
3
Z z=1
z=0
Z y=1
y=0
dydz =1
3.
90 CHAPTER 13. MULTIPLE INTEGRALS
4.
Z Z ZD
e−xyydxdydz =Z z=1
z=0
Z y=1
y=0
Z x=1
x=0
e−xyydxdydz
=
Z z=1
z=0
Z y=1
y=0
³−e−xy ¯x=1
x=0
´dydz
=
Z z=1
z=0
Z y=1
y=0
¡−e−y + 1¢ dydz=
Z z=1
z=0
³e−y + y
¯y=1y=0
´dz
=
Z z=1
z=0
¡e−1 + 1− 1¢ dz = 1
e.
5.
Z Z ZD
zex+ydxdydz =
Z z=2
z=0
Z y=1
y=0
Z x=1
x=0
zex+ydxdydz
=
Z z=2
z=0
Z y=1
y=0
zeyµZ x=1
x=0
exdx
¶dydz
=
Z z=2
z=0
Z y=1
y=0
zey (e− 1) dydz
= (e− 1)Z z=2
z=0
Z y=1
y=0
zeydydz
= (e− 1)Z z=2
z=0
z
Z y=1
y=0
eydydz
= (e− 1)Z z=2
z=0
z (e− 1) dz
= (e− 1)2Ã1
2z2¯z=2z=0
!= 2 (e− 1)2 .
Remark: One can also note that
Z z=2
z=0
Z y=1
y=0
Z x=1
x=0
zex+ydxdydz =
Z z=2
z=0
Z y=1
y=0
Z x=1
x=0
zexeydxdydz
=
µZ z=2
z=0
zdz
¶µZ y=1
y=0
eydy
¶µZ 1
x=0
ex¶dx
at the beginning.
13.5. TRIPLE INTEGRALS 91
6. Z Z ZD
x2 cos (z) dxdydz =
Z z=π/2
z=0
µZ 1
y=0
µZ x=1−y
x=0
x2 cos (z) dx
¶dy
¶dz
=
Z z=π/2
z=0
cos (z)
ÃZ y=1
y=0
Ã1
3x3¯1−yx=0
!dy
!
=
Z z=π/2
z=0
cos (z)
µZ y=1
y=0
1
3(1− y)3 dy
¶dz
=
Z z=π/2
z=0
cos (z)
µ1
12
¶dz
=1
12
³sin (z)|π/20
´=1
12.
7. Z Z ZD
zdxdydz =
Z z=1
z=0
z
µZ ZR
dxdy
¶dz =
1
2
Z ZR
dxdy,
where
R = (x, y) : x2 + y2 ≤ 1, x ≥ 0 and y ≥ 0.Therefore, Z Z
R
dxdy =
Z θ=π/2
θ=0
Z 1
r=0
rdrdθ =π
2
Ã1
2r2¯10
!=
π
4
(merely the area of the part of the unit disk in the first quadrant).
Thus, Z Z ZD
zdxdydz =1
2
Z ZR
dxdy =π
8.
8. Part of the boundary of the tetrahedron is the plane that passes trough the points (1, 0, 0) , (0, 1, 0) , (0, 0, 1).That plane is the graph of an equation of the form is
ax+ by + cz = d.
You can confirm that a = b = c = d = 1, so that the equation is
x+ y + z = 1,
so that z = 1− x− y = 1− y − x. The projection of that plane onto the xy-plane is the linex+ y = 1.
Thus, Z Z ZD
x2dxdydz =
Z ZR
µZ z=1−x−y
z=0
x2dz
¶dxdy,
where R is the triangular region bounded by the x and y axes and the line x+ y = 1, as in thepicture:
1
1
x
y
92 CHAPTER 13. MULTIPLE INTEGRALS
Therefore,
Z ZR
µZ z=1−x−y
z=0
x2dz
¶dxdy =
Z x=1
x=0
Z 1−x
y=0
x2µZ z=1−x−y
z=0
dz
¶dydx
=
Z x=1
x=0
Z 1−x
y=0
x2 (1− x− y) dydx
=
Z x=1
x=0
Z 1−x
y=0
¡x2 − x3 − x2y¢ dydx
=
Z x=1
x=0
Ãx2y − x3y − 1
2x2y2
¯1−x0
!dx
=
Z x=1
x=0
µ1
2x4 − x3 + 1
2x2¶dx
=1
10x5 − 1
4x4 +
1
6x3¯10
=1
60
9.
Z Z ZD
xydxdxydz =
Z ZR
µZ z=x+y
z=0
xydz
¶dxdy,
where R is the region in the xy-plane that is bounded by y = x2 and x = y2.
13.5. TRIPLE INTEGRALS 93
Thus,
Z ZR
µZ z=x+y
z=0
xydz
¶dxdy =
Z ZR
xy
µZ z=x+y
z=0
dz
¶dxdy
=
Z ZR
xy (x+ y) dxdy
=
Z ZR
¡x2y + xy2
¢dxdy
=
Z x=1
x=0
Z y=√x
y=x2
¡x2y + xy2
¢dydx
=
Z x=1
x=0
Ãx2y2
2+xy3
3
¯y=√xy=x2
!dx
=
Z x=1
x=0
µx3
2+x5/2
3− x
6
2− x
7
3
¶dx
=x4
8+2
21x7/2 − x
7
14− x
8
24
¯10
=1
8+2
21− 1
14− 1
24=3
28
10.
Z Z ZD
x2dydxdz =
Z ZR
x2µZ z=5−y
z=1
dz
¶dxdy,
where R is the region inside the circle x2 + y2 = 9. Thus,
Z ZR
x2µZ z=5−y
z=1
dz
¶dxdy =
Z ZR
x2 (4− y) dxdy
=
Z θ=2π
θ=0
Z 3
r=0
r3 cos2 (θ) (4− r sin (θ)) drdθ
=
Z θ=2π
θ=0
cos2 (θ)
Ãr4 − r
5
5sin (θ)
¯3r=0
!dθ
=
Z θ=2π
θ=0
cos2 (θ)
µ81− 243
5sin (θ)
¶dθ
=
Z θ=2π
θ=0
µ81 cos2 (θ)− 243
5cos2 (θ) sin (θ)
¶dθ
=81
2
Z θ=2π
θ=0
(1 + cos (2θ)) dθ − 2435
Z 2π
0
cos2 (θ) sin (θ) dθ
=81
2
Ãθ +
1
2sin (2θ)
¯2π0
!+243
5
Ãcos3 (θ)
3
¯2π0
!= 81π
94 CHAPTER 13. MULTIPLE INTEGRALS
13.6 Triple Integrals in Cylindrical and Spherical Coordi-
nates
1.
x = 2 cos³π4
´= 2
Ã√2
2
!=√2,
y = 2 sin³π4
´= 2
Ã√2
2
!=√2,
z = 1.
2.
x = 4cos³π6
´= 4
Ã√3
2
!= 2√3,
y = 4 sin³π6
´= 4
µ1
2
¶= 2,
z = 2.
3.
x = 3 cos
µ2π
3
¶= 3
µ−12
¶= −3
2,
y = 3 sin
µ2π
3
¶= 3
Ã√3
2
!=3√3
2,
z = 4.
4.
x = 2cos³−π6
´= 2
Ã√3
2
!=√3,
y = 2 sin³−π6
´= 2
µ−12
¶= −1,
z = 4.
5.
r =√1 + 1 =
√2,
θ = arccos
µ− 1√
2
¶= π − π
4=3π
4,
z = 4.
6.
r =√4 + 12 =
√16 = 4,
θ = − arccosµ2
4
¶= − arccos
µ1
2
¶= −π
3,
z = −1
13.6. TRIPLE INTEGRALS IN CYLINDRICAL AND SPHERICAL COORDINATES 95
7.
r =√1 + 1 =
√2
θ = − arccosµ1√2
¶= −π
4,
z = 2
8.
r =√1 + 3 =
√4 = 2,
θ = arccos
µ1
2
¶=
π
3,
z = 2
9. We have
x2 + y2 = 16⇔ r2 = 16⇒ r = 4.
5-5
0z
5
5
y
0
x0
-5-5
Thus, Z Z ZD
px2 + y2dxdydz =
Z ZR
µZ z=4
z=−5
px2 + y2dz
¶dxdy,
where R is the disk of radius 4 centered at the origin in the xy-plane. Thus,Z ZR
µZ z=4
z=−5
px2 + y2dz
¶dxdy =
Z ZR
px2 + y2
µZ z=4
z=−5dz
¶dxdy
= 9
Z ZR
px2 + y2dxdy
= 9
Z θ=2π
θ=0
Z r−4
r=0
r2drdθ
= 9 (2π)
Ãr3
3
¯40
!= 9 (2π)
µ64
3
¶= 384π
10. We have
z = 1− x2 − y2 = z = 1− r2,and
z = 0⇒ 1− r2 = 0⇒ r = 1.
Thus, the intersection of the paraboloid with the xy-plane is the unit circle.
00
1
z
1
x y1 0
96 CHAPTER 13. MULTIPLE INTEGRALS
Therefore, Z Z ZD
¡x3 + xy2
¢dxdydz =
Z ZR
ÃZ 1−x2−y2
z=0
¡x3 + xy2
¢dz
!dxdy,
where R is the part of the unit disk in the first quadrant. Thus,Z ZR
ÃZ 1−x2−y2
z=0
¡x3 + xy2
¢dz
!dxdy
=
Z θ=π/2
θ=0
Z r=1
r=0
ÃZ 1−r2
z=0
¡r3 cos3 (θ) + r3 cos (θ) sin2 (θ)
¢dz
!rdrdθ
We have
r3 cos3 (θ) + r3 cos (θ) sin2 (θ) = r3 cos (θ)¡cos2 (θ) + sin2 (θ)
¢= r3 cos (θ) .
Therefore, Z θ=π/2
θ=0
Z r=1
r=0
ÃZ 1−r2
z=0
¡r3 cos3 (θ) + r3 cos (θ) sin2 (θ)
¢dz
!rdrdθ
=
Z θ=π/2
θ=0
Z r=1
r=0
ÃZ 1−r2
z=0
r4 cos (θ) dz
!drdθ
=
Z θ=π/2
θ=0
Z r=1
r=0
r4 cos (θ)
ÃZ 1−r2
z=0
dz
!drdθ
=
Z θ=π/2
θ=0
Z r=1
r=0
r4 cos (θ)¡1− r2¢ drdθ
=
ÃZ θ=π/2
θ=0
cos (θ) dθ
!µZ r=1
r=0
¡r4 − r6¢ dr¶
=³sin (θ)|π/20
´Ã 15r5 − 1
7r7¯1r=0
!
= (1)
µ2
35
¶=2
35.
11.
0
1
2
z
6
y
0
2
x
-2 0-2
We have Z Z ZD
ezdxdydz =
Z ZR
ÃZ z=1+x2+y2
z=0
ezdz
!dxdy,
13.6. TRIPLE INTEGRALS IN CYLINDRICAL AND SPHERICAL COORDINATES 97
where R is the disk that is bounded by the circle x2 + y2 = 5 in the xy-plane. This is the circleof radius
√5 centered at the origin. Thus,Z θ=2π
θ=0
Z r=√5
r=0
ÃZ z=1+r2
z=0
ezdz
!rdrdθ =
Z θ=2π
θ=0
Z r=√5
r=0
³ez|1+r20
´rdrdθ
=
Z θ=2π
θ=0
Z r=√5
r=0
³e1+r
2 − 1´rdrdθ
= 2π
Z r=√5
r=0
³e1+r
2
r − r´dr.
We set u = 1 + r2 so that du = 2rdr. Therefore,Ze1+r
2
rdr =1
2
Zeudu =
1
2eu =
1
2e1+r
2
.
Thus,
2π
Z r=√5
r=0
³e1+r
2
r − r´dr = 2π
Ã1
2e1+r
2 − 12r2¯√50
!= π
¡e6 − 5− e¢
12. In cylindrical coordinates,
x2 + y2 = 1⇔ r2 = 1⇔ r = 1,
and
z =p4x2 + 4y2 ⇔ z = 2
px2 + y2 ⇔ z = 2r.
01
z
2
1
y
0
x0
-1 -1
We have Z Z ZD
x2dxdydz =
Z ZR
µZ z=2r
z=0
r2 cos2 (θ) dz
¶dxdy
=
Z θ=2π
θ=0
Z r=1
r=0
µZ z=2r
z=0
r2 cos2 (θ) dz
¶rdrdθ
=
Z θ=2π
θ=0
Z r=1
r=0
r3 cos2 (θ)
µZ z=2r
z=0
dz
¶drdθ
=
Z θ=2π
θ=0
Z r=1
r=0
2r4 cos2 (θ) drdθ
=
ÃZ θ=2π
θ=0
cos2 (θ) dθ
!µZ r=1
r=0
2r4dr
¶
=
ÃZ θ=2π
θ=0
1 + cos (2θ)
2dθ
!Ã2
5r5¯r=1r=0
!
=2
5
Ãθ
2+1
4sin (2θ)
¯θ=2πθ=0
!=2
5π.
98 CHAPTER 13. MULTIPLE INTEGRALS
13.
2
2
0
-1
-2
1
z
2
1
0
y -1
-2
1
x0
-1-2
The volume of the region is Z ZR
ÃZ z=√4−x2−y2
z=−√4−x2−y2
dz
!dxdy,
where R is the disk in the xy-plane that is bounded by the circle x2 + y2 = 1. Thus,Z ZR
ÃZ z=√4−x2−y2
z=−√4−x2−y2
dz
!dxdy =
Z θ=2π
θ=0
Z r=1
r=0
ÃZ z=√4−r2
z=−√4−r2dz
!rdrdθ
=
Z θ=2π
θ=0
Z r=1
r=0
³2p4− r2
´rdrdθ
= 4π
Z r=1
r=0
p4− r2rdr.
We set u = 4− r2 so that du = −2rdr. Therefore,
4π
Z r=1
r=0
p4− r2rdr = −2π
Z u=3
u=4
u1/2du
= −2πÃ2
3u3/2
¯34
!=
4π
3
³8− 33/2
´14.
x = ρ sin (φ) cos (θ) = 1 sin (0) cos (0) = 0,
y = ρ sin (φ) sin (θ) = 1 sin (0) sin (0) = 0,
z = ρ cos (φ) = 1 cos (0) = 1.
Thus, the point is (0, 0, 1) in Cartesian coordinates.
15.
x = ρ sin (φ) cos (θ) = 2 sin³π4
´cos³π3
´= 2
Ã√2
2
!µ1
2
¶=
√2
2,
y = ρ sin (φ) sin (θ) = 2 sin³π4
´sin³π3
´= 2
Ã√2
2
!Ã√3
2
!=
√6
2,
z = ρ cos (φ) = 2 cos³π4
´= 2
Ã√2
2
!=√2.
13.6. TRIPLE INTEGRALS IN CYLINDRICAL AND SPHERICAL COORDINATES 99
Thus, the point is Ã√2
2,
√6
2,√2
!in Cartesian coordinates.
16.
x = ρ sin (φ) cos (θ) = 5 sin³π2
´cos (π) = 5 (1) (−1) = −5,
y = ρ sin (φ) sin (θ) = 5 sin³π2
´sin (π) = 5 (1) (0) = 0,
z = ρ cos (φ) = 5 cos³π2
´= 5 (0) = 0.
Thus, the point is (−5, 0, 0) in Cartesian coordinates.17.
x = ρ sin (φ) cos (θ) = 4 sin³π3
´cos
µ3π
4
¶= 4
Ã√3
2
!Ã−√2
2
!= −√6,
y = ρ sin (φ) sin (θ) = 4 sin³π3
´sin
µ3π
4
¶= 4
Ã√3
2
!Ã√2
2
!=√6,
z = ρ cos (φ) = 4 cos³π3
´= 4
µ1
2
¶= 2.
Thus, the point is¡−√6,√6, 2¢ in Cartesian coordinates.
18.
ρ =√1 + 3 + 12 =
√16 = 4,
φ = arccos
µz
ρ
¶= arccos
Ã2√3
4
!= arccos
Ã√3
2
!=
π
6,
θ = arccos
Ãxp
x2 + y2
!= arccos
µ1√1 + 3
¶= arccos
µ1
2
¶=
π
3
(since y =√3 > 0).
Thus, the point is ³4,π
3,π
6
´in spherical coordinates.
19.
ρ =√0 + 1 + 1 =
√2,
φ = arccos
µz
ρ
¶= arccos
µ− 1√
2
¶= π − π
4=3π
4,
θ = − arccosÃ
xpx2 + y2
!= − arccos (0) = −π
2
(since y = −1 < 0).Thus, the point is µ√
2,−π2,3π
4
¶
100 CHAPTER 13. MULTIPLE INTEGRALS
in spherical coordinates.
20.
ρ =√0 + 3 + 1 =
√4 = 2,
φ = arccos
µz
ρ
¶= arccos
µ1
2
¶=
π
3,
θ = arccos
Ã0p
x2 + y2
!= arccos (0) =
π
2
(since y = 1 > 0).
Thus, the point is ³2,π
2,π
3
´in spherical coordinates.
21.
ρ =√1 + 1 + 6 =
√8 = 2
√2,
φ = arccos
µz
ρ
¶= arccos
à √6
2√2
!= arccos
Ã√3
2
!=
π
6,
θ = arccos
Ãxp
x2 + y2
!= arccos
µ− 1√
1 + 1
¶= arccos
µ− 1√
2
¶=3π
4
(since y = 1 > 0).
Thus, the point is µ2√2,3π
4,π
6
¶
in spherical coordinates.
22.
1
x0
0
y
2
2
-2-2
0
z
2
3
Since ρ = 3 on the sphere x2 + y2 + z2 = 9, and 0 ≤ φ < π/2 above the xy-plane,
13.6. TRIPLE INTEGRALS IN CYLINDRICAL AND SPHERICAL COORDINATES 101
Z Z ZD
¡9− x2 − y2¢ dxdydz
=
Z θ=2π
θ=0
Z π/2
φ=0
Z ρ=3
ρ=0
¡9− ρ2 sin2 (φ) cos2 (θ)− ρ2 sin2 (φ) sin2 (θ)
¢ρ2 sin (φ) dρdφdθ
=
Z θ=2π
θ=0
Z π/2
φ=0
Z ρ=3
ρ=0
¡9− ρ2 sin2 (φ)
¢ρ2 sin (φ) dρdφdθ
=
Z θ=2π
θ=0
Z π/2
φ=0
Ã3ρ3 − 1
5ρ5 sin2 (φ)
¯ρ=3ρ=0
!sin (φ) dφdθ
=
Z θ=2π
θ=0
Z π/2
φ=0
µ81− 243
5sin2 (φ)
¶sin (φ) dφdθ
= 81
Z θ=2π
θ=0
Z π/2
φ=0
sin (φ) dφdθ − 2435
Z θ=2π
θ=0
Z π/2
φ=0
sin3 (φ) dφdθ
We have
81
Z θ=2π
θ=0
Z π/2
φ=0
sin (φ) dφdθ = 81
Z θ=2π
θ=0
³− cos (φ)|π/20
´dθ
= 81
Z θ=2π
θ=0
dθ = 81 (2π) = 162π
We also have Zsin3 (φ) dφ =
Zsin2 (φ) sin (φ) dφ =
Z ¡1− cos2 (φ)¢ sin (φ) dφ.
If we set u = cos (φ) then du = − sin (φ) dφ so thatZ ¡1− cos2 (φ)¢ sin (φ) dφ = −
Z ¡1− u2¢ du
= −u+ 13u3 = − cos (φ) + 1
3cos3 (φ) .
Thus, Z π/2
φ=0
sin3 (φ) dφ = − cos (φ) + 13cos3 (φ)
¯π/20
= 1− 13=2
3.
Therefore,Z Z ZD
¡9− x2 − y2¢ dxdydz = 81
Z θ=2π
θ=0
Z π/2
φ=0
sin (φ) dφdθ − 2435
Z θ=2π
θ=0
Z π/2
φ=0
sin3 (φ) dφdθ
= 162π − 2435
Z θ=2π
θ=0
µ2
3
¶dθ
= 162π − 1625(2π) =
486
5π
23.
102 CHAPTER 13. MULTIPLE INTEGRALS
2
y
1
0
00
x
1
2
z 1
2
Z Z ZD
zdxdydz =
Z θ=π/2
θ=0
Z φ=π/2
φ=0
Z ρ=2
ρ=1
ρ cos (φ) ρ2 sin (φ) dρdφdθ
=
Z θ=π/2
θ=0
Z φ=π/2
φ=0
Z ρ=2
ρ=1
ρ3 cos (φ) sin (φ) dρdφdθ
=
ÃZ θ=π/2
θ=0
dθ
!ÃZ φ=π/2
φ=0
cos (φ) sin (φ) dφ
!µZ ρ=2
ρ=1
ρ3dρ
¶
=³π2
´Ã 12sin2 (φ)
¯π/20
!Ã1
4ρ4¯21
!
=³π2
´µ12
¶µ24
4− 14
¶=15
16π
24.
3
2x
z
2
1
1
00
0
1 y
2
3
3
Z Z ZD
e√x2+y2+z2dxdydz =
Z θ=π/2
θ=0
Z φ=π/2
φ=0
Z ρ=3
ρ=0
eρρ2 sin (φ) dρdφdθ
=
ÃZ θ=π/2
θ=0
dθ
!ÃZ φ=π/2
φ=0
sin (φ) dφ
!µZ ρ=3
ρ=0
eρρ2dρ
¶=
³π2
´³− cos (φ)|π/20
´Z ρ=3
ρ=0
eρρ2dρ
=π
2
Z ρ=3
ρ=0
eρρ2dρ.
In order to evaluate the last integral, let’s apply integration by parts by setting u = ρ2 anddv = eρdρ. Thus,
du = 2ρdρ and v =
Zeρdρ = eρ.
13.6. TRIPLE INTEGRALS IN CYLINDRICAL AND SPHERICAL COORDINATES 103
Therefore, Zρ2eρdρ =
Zudv = uv −
Zvdu
= ρ2eρ − 2Zeρρdρ.
Now we apply integration by parts by setting u = ρ and dv = eρ. Therefore,Zρeρdρ =
Zudv = uv −
Zvdu
= ρeρ −Zeρdρ = ρeρ − eρ.
Thus, Zρ2eρdρ = ρ2eρ − 2
Zeρρdρ = ρ2eρ − 2 (ρeρ − eρ)
= ρ2eρ − 2ρeρ + 2eρ.
Therefore,
π
2
Z ρ=3
ρ=0
eρρ2dρ =π
2
³ρ2eρ − 2ρeρ + 2eρ¯ρ=3
ρ=0
´=
π
2
¡5e3 − 2¢ = π
2
¡5e3 − 2¢
25.
2
0z
-2
-4-4
-2
x
0
2
4 02
y
4
4
The spheres have radius 3 and 4, respectively, and y > 0 in the region. Therefore,Z Z ZD
x2dxdydz =
Z θ=π
θ=0
Z φ=π
φ=0
Z ρ=4
ρ=3
ρ2 sin2 (φ) cos2 (θ) ρ2 sin3 (θ) dρdφdθ
=
ÃZ θ=π
θ=0
cos2 (θ) dθ
!ÃZ φ=π
φ=0
sin3 (φ) dφ
!µZ ρ=4
ρ=3
ρ4dρ
¶
=
µ1
2θ +
1
4sin (2θ)
¯π0
¶ÃZ φ=π
φ=0
sin3 (φ) dφ
!Ã1
5ρ5¯43
!
=³π2
´ÃZ φ=π
φ=0
sin3 (φ) dφ
!µ781
5
¶.
We have Zsin3 (φ) dφ =
Zsin2 (φ) sin (φ) dφ =
Z ¡1− cos2 (φ)¢ sin (φ) dφ.
104 CHAPTER 13. MULTIPLE INTEGRALS
We set u = cos (φ):Z ¡1− cos2 (φ)¢ sin (φ) dφ = −
Z ¡1− u2¢ du
= −u+ 13u3 = − cos (φ) + 1
3cos3 (φ) .
Therefore, Z φ=π
φ=0
sin3 (φ) dφ = − cos (φ) + 13cos3 (φ)
¯π0
= 1− 13+ 1− 1
3=4
3
Thus, ³π2
´ÃZ φ=π
φ=0
sin3 (φ) dφ
!µ781
5
¶=³π2
´µ43
¶µ781
5
¶=1562
15π
26.
0
2
4
z
y
0
42
x0-2-4
Z Z ZD
x2zdxdydz =
Z θ=2π
θ=0
Z φ=π/3
φ=0
Z ρ=4
ρ=2
ρ2 sin2 (φ) cos2 (θ) ρ cos (φ) ρ2 sin (φ) dρdφdθ
=
Z θ=2π
θ=0
Z φ=π/3
φ=0
Z ρ=4
ρ=2
ρ5 sin3 (φ) cos (φ) cos2 (θ) dρdφdθ
=
ÃZ θ=2π
θ=0
cos2 (θ) dθ
!ÃZ φ=π/3
φ=0
sin3 (φ) cos (φ) dφ
!µZ ρ=4
ρ=2
ρ5dρ
¶
=
Ã1
2θ +
1
4sin (2θ)
¯2π0
!Ã1
4sin4 (θ)
¯π/30
!Ã1
5ρ5¯42
!
= (π)
⎛⎝14
Ã√3
2
!4⎞⎠µ15
¡45 − 25¢¶ = 279
10π
27.
0
2
4
4
z
2
y
0
-2 42
x0
-4 -2-4
13.6. TRIPLE INTEGRALS IN CYLINDRICAL AND SPHERICAL COORDINATES 105
Z Z ZD
dxdydz =
Z θ=2π
θ=0
Z φ=π/3
φ=π/6
Z ρ=3
ρ=0
ρ2 sin (φ) dρdφdθ
=
ÃZ θ=2π
θ=0
dθ
!ÃZ φ=π/3
φ=π/6
sin (φ) dφ
!µZ ρ=3
ρ=0
ρ2dρ
¶
= (2π)³− cos (φ)|π/3π/6
´Ã 13ρ3¯30
!
= (2π)
Ã−12+
√3
2
!µ1
3
¡33¢¶= 9
³√3− 1
´π.
28.
0
2
4
z
y
0
4
x
20-2-4
Z Z ZD
zdxdydz =
Z θ=2π
θ=0
Z φ=π/3
φ=0
Z ρ=4 cos(φ)
ρ=0
ρ cos (φ) ρ2 sin (φ) dρdφdθ
=
Z θ=2π
θ=0
Z φ=π/3
φ=0
cos (φ) sin (φ)
ÃZ ρ=4 cos(φ)
ρ=0
ρ3dρ
!dφdθ
= 2π
Z φ=π/3
φ=0
cos (φ) sin (φ)
Ãρ4
4
¯4 cos(φ)0
!dφ
= 2π
Z φ=π/3
φ=0
cos (φ) sin (φ)¡64 cos4 (θ)
¢dφ
= 128π
Z φ=π/3
φ=0
cos5 (φ) sin (φ) dφ
= 128π
Ã−16cos6 (φ)
¯π/30
!
=128π
6
Ã1−
µ1
2
¶6!= 21π
29.
022
1z
2
xy
00
-2-2
106 CHAPTER 13. MULTIPLE INTEGRALS
The sphere is the graph of ρ = 2. We have
z =px2 + y2 ⇒ ρ cos (φ) =
qρ2 sin2 (φ) cos2 (θ) + ρ2 sin2 (φ) sin2 (θ)
⇒ ρ cos (φ) = ρ sin (φ)⇒ cos (φ) = sin (φ) ,
so that the cone is the graph of φ = π/4. Therefore,Z Z Zdxdydz =
Z θ=2π
θ=0
Z φ=π/2
φ=π/4
Z ρ=2
ρ=0
ρ2 sin (φ) dφdθ
=
ÃZ θ=2π
θ=0
dθ
!ÃZ φ=π/2
φ=π/4
sin (φ) dφ
!µZ ρ=2
ρ=0
ρ2dρ
¶
= (2π)³− cos (θ)|π/2π/4
´Ã 13ρ3¯20
!
= 2π
Ã√2
2
!µ8
3
¶=8√2
3π
Chapter 14
Vector Analysis
14.1 Vector Fields, Divergence and Curl
1.
a)
∇ · F (x, y, z) = ∂
∂x(xyz)− ∂
∂z
¡x2y
¢= yz
b)
∇×F (x, y, z) =
¯¯ i j k
∂x ∂y ∂zxyz 0 −x2y
¯¯
=
¯∂y ∂z0 −x2y
¯i−
¯∂x ∂zxyz −x2y
¯j+
¯∂x ∂yxyz 0
¯k
=
µ∂
∂y
¡−x2y¢¶ i−µ ∂
∂x
¡−x2y¢− ∂
∂z(xyz)
¶j+
µ− ∂
∂y(xyz)
¶k
= −x2i− (−2xy − xy) i− xzk = −x2i+ 3xyi− xzk2.
a)
∇ · F (x, y, z) =∂
∂x
¡e−xxy2
¢+
∂
∂y
¡e−xx2y
¢=
¡−e−xxy2 + e−xy2¢+ e−xx2 = e−x ¡−xy2 + y2 + x2¢b)
∇×F (x, y, z) =
¯¯ i j k
∂x ∂y ∂ze−xxy2 e−xx2y 0
¯¯
=
¯∂y ∂z
e−xx2y 0
¯i−
¯∂x ∂z
e−xxy2 0
¯j+
¯∂x ∂y
e−xxy2 e−xx2y
¯k
=∂
∂x
¡e−xx2y
¢− ∂
∂y
¡e−xxy2
¢= −e−xx2y + 2xe−xy − 2ye−xx = −e−xx2y
3.
107
108 CHAPTER 14. VECTOR ANALYSIS
a)
∇ · F (x, y, z) = ∂
∂ycos (xz)− ∂
∂zsin (xy) = 0.
b)
∇×F (x, y, z) =
¯¯ i j k
∂x ∂y ∂z0 cos (xz) − sin (xy)
¯¯
=
¯∂y ∂z
cos (xz) − sin (xy)¯i−
¯∂x ∂z0 − sin (xy)
¯j+
¯∂x ∂y0 cos (xz)
¯k
=
µ− ∂
∂ysin (xy)− ∂
∂zcos (xz)
¶i+
∂
∂xsin (xy) j+
∂
∂xcos (xz)k
= (−x cos (xy) + x sin (xz)) i+ y cos (xy) j− z sin (xz)k
4.
a)
∇ · F (x, y, z) =∂
∂xarctan
³yx
´+
∂
∂yarctan
µx
y
¶
=
⎛⎜⎝ 1
1 +³yx
´2⎞⎟⎠³− y
x2
´+
⎛⎜⎜⎜⎝ 1
1 +
µx
y
¶2⎞⎟⎟⎟⎠µ− xy2
¶
=
µx2
x2 + y2
¶³− yx2
´+
µy2
x2 + y2
¶µ− xy2
¶= − y
x2 + y2− x
x2 + y2= − x+ y
x2 + y2
b)
∇×F (x, y, z)
=
¯¯ i j k
∂x ∂y ∂zarctan (y/x) arctan (x/y) 0
¯¯
=
¯∂y ∂z
arctan (x/y) 0
¯i−
¯∂x ∂z
arctan (y/x) 0
¯i+
¯∂x ∂y
arctan (y/x) arctan (x/y)
¯k
=
µ∂
∂xarctan
µx
y
¶− ∂
∂yarctan
³yx
´¶k
=
⎛⎜⎜⎜⎝⎛⎜⎜⎜⎝ 1
1 +
µx
y
¶2⎞⎟⎟⎟⎠µ1
y
¶+
⎛⎜⎝ 1
1 +³yx
´2⎞⎟⎠µ 1
x
¶⎞⎟⎟⎟⎠k=
µµy2
x2 + y2
¶µ1
y
¶+
µx2
x2 + y2
¶µ1
x
¶¶k
=
µx+ y
x2 + y2
¶k
5.
14.2. LINE INTEGRALS 109
a)
∇ · F (x, y, z) = ∂
∂x(2xy) +
∂
∂y
¡x2 + 2yz
¢+
∂
∂zy2 = 2y + 2z
b)
∇×F (x, y, z) =
¯¯ i j k
∂x ∂y ∂z2xy x2 + 2yz y2
¯¯
=
¯∂y ∂z
x2 + 2yz y2
¯i−
¯∂x ∂z2xy y2
¯j+
¯∂x ∂y2xy x2 + 2yz
¯k
= (2y − 2y) i− (0) j+ (2x− 2x)k = 06.
a)
∇ · F (x, y, z) =∂
∂xln (x) +
∂
∂yln (xy) +
∂
∂zln (xyz)
=1
x+1
y+1
z
b)
×F (x, y, z) =
¯¯ i j k
∂x ∂y ∂zln (x) ln (xy) ln (xyz)
¯¯
=
¯∂y ∂z
ln (xy) ln (xyz)
¯i−
¯∂x ∂zln (x) ln (xyz)
¯j+
¯∂x ∂yln (x) ln (xy)
¯k
=1
yi− 1
xj+
1
xk
14.2 Line Integrals
1. We have σ0 (t) =¡3t2, 1
¢so that
ds = ||σ0 (t)|| dt =p9t4 + 1dt
Therefore, ZC
y3ds =
Z 2
0
t3p9t4 + 1dt.
We set u = 9t4 + 1 so that du = 36t3dt. Thus,Z 2
0
t3p9t4 + 1dt =
1
36
Z 145
1
u1/2du
=1
36
Ã2
3u3/2
¯1451
!=1
54
³1453/2 − 1
´2. We have
σ0 (t) = (−2 sin (t) , 2 cos (t))so that
ds = ||σ0 (t)|| dt =q4 sin2 (t) + 4 cos2 (t) = 2dt.
110 CHAPTER 14. VECTOR ANALYSIS
Therefore, ZC
xy2ds =
Z π/2
−π/2(2 cos (t)) (2 sin (t))
2(2) dt = 16
Z π/2
−π/2sin2 (t) cos (t) dt.
We set u = sin (t) so that du = cos (t) dt. Thus,
16
Z π/2
−π/2sin2 (t) cos (t) dt = 16
Z 1
−1u2du
= 16
Ã1
3u3¯1−1
!=16
3(1 + 1) =
32
3
3. We can paramterize C by
σ (t) = (2, 1) + t (4− 2, 5− 1) = (2, 1) + t (2, 4) = (2 + 2t, 1 + 4t) ,where 0 ≤ t ≤ 1. Thus,
σ0 (t) = (2, 4)⇒ ||σ0 (t)|| = √4 + 16 =√20 = 2
√5
Therefore, ZC
xeyds =
Z 1
0
(2 + 2t) e1+4tdt = 2e
Z 1
0
e4tdt+ 2e
Z 1
0
te4tdt.
We have
2e
Z 1
0
e4tdt = 2e
Ã1
4e4t¯10
!=e
2
¡e4 − 1¢ = e5
2− e2
We evaluate the other integral by setting u = t and dv = e4tdt. Thus
du = dt and v =1
4e4t.
Therefore, Zte4tdt =
Zudv = uv −
Zvdu
= t
µ1
4e4t¶− 14
Ze4tdt
=t
4e4t − 1
16e4t.
Thus,
2e
Z 1
0
te4tdt = 2e
Ãt
4e4t − 1
16e4t¯10
!
= 2e
µ1
4e4 − 1
16e4 +
1
16
¶=1
8e+
3
8e5
Therefore, ZC
xeyds = 2e
Z 1
0
e4tdt+ 2e
Z 1
0
te4tdt
=e5
2− e2+1
8e+
3
8e5 =
7
8e5 − 3
8e
14.2. LINE INTEGRALS 111
4. We can parametrize C by
σ (θ) = (4, 3) + 2 (cos (θ) , sin (θ))
= (4 + 2 cos (θ) , 3 + 2 sin (θ)) , 0 ≤ θ ≤ π.
Thus,
σ0 (θ) = 2 (− sin θ) , cos (θ) ,so that
ds = ||σ0 (θ)|| = 2.Therefore, Z
C
y − 3(x− 4)2 + (y − 3)2 ds =
Z π
0
2 sin (θ)
4 cos2 (θ) + 4 sin2 (θ)(2) dθ
=
Z π
0
sin (θ) dθ = − cos (θ)|π0 = 2.
5. We can parametrize C by
σ (t) = (2, 3, 4) + t (1, 2, 3) = (2 + t, 3 + 2t, 4 + 3t) , 0 ≤ t ≤ 1.Thus,
ds = ||σ0 (t)|| dt = ||(1, 2, 3)|| dt =√14dt.
Therefore, ZC
(x− 2) e(y−3)(z−4)ds =Z 1
0
te(2t)(3t)√14dt =
√14
Z 1
0
te6t2
dt
=√14
Ã1
12e6t
2
¯10
!
=
√14
12
¡e6 − 1¢ .
6. We can parametrize C by
σ (t) = (1, 2) + t (3− 1, 4− 2) = (1, 2) + t (2, 2) = (1 + 2t, 2 + 2t) ,where 0 ≤ t ≤ 1. Thus,
σ0 (t) = 2i+ 2j,
and
F (σ (t)) = F (1 + 2t, 2 + 2t) = (1 + 2t)2 i+ (2 + 2t)2 j
Therefore,
F (σ (t)) · σ0 (t) =³(1 + 2t)2 i+ (2 + 2t)2 j
´· (2i+ 2j)
= 2 (1 + 2t)2+ 2 (2 + 2t)
2
= 16t2 + 24t+ 10.
Thus, ZC
F·d σ =Z 1
0
F (σ (t)) · σ0 (t) dt =
Z 1
0
¡16t2 + 24t+ 10
¢dt
=16
3t3 + 12t2 + 10t
¯10
=16
3+ 12 + 10 =
82
3
112 CHAPTER 14. VECTOR ANALYSIS
7. We can parametrize C by
σ (θ) = (cos (θ) , sin (θ)) ,π
2≤ θ ≤ π.
Thus,
σ0 (θ) = − sin (θ) i+ cos (θ) jand
F (σ (θ)) = F (cos (θ) , sin (θ)) = sin (θ) i− cos (θ) jTherefore,
F (σ (θ)) · σ0 (θ) = (sin (θ) i− cos (θ) j) · (− sin (θ) i+ cos (θ) j)= − sin2 (θ)− cos2 (θ) = −1.
Thus ZC
F·dσ =
Z π
π/2
F (σ (θ)) · σ0 (θ) dθ
=
Z π
π/2
(−1) dθ = −³π − π
2
´= −π
2.
8. We have
σ0 (t) =1
ti+ 3t2j
and
F (σ (t)) = F¡ln (t) , t3
¢= ln
¡t3¢i− eln(t)j = 3 ln (t) i− tj
Therefore,
F (σ (t)) · σ0 (t) = (3 ln (t) i− tj) ·µ1
ti+ 3t2j
¶= 3
ln (t)
t− 3t3
Thus, ZC
F·d σ =Z e
1
F (σ (t)) · σ0 (t) dt =
Z e
1
µ3ln (t)
t− 3t3
¶dt
= 3ln2 (t)
2− 34t4¯e1
=3
2− 34e4 +
3
4=9
4− 34e4
9. We have
σ0 (t) = − sin (t) i+ j+ kand
F (σ (t)) = F (cos (t) , t, t) = cos (t) i+ sin (t) j+ cos (t)k
Therefore,
F (σ (t)) · σ0 (t) = (cos (t) i+ sin (t) j+ cos (t)k) · (− sin (t) i+ j+ k)= − cos (t) sin (t) + sin (t) + cos (t)
14.2. LINE INTEGRALS 113
Thus ZC
F·dσ =
Z π/2
π/4
F (σ (t)) · σ0 (t) dt
=
Z π/2
π/4
(− cos (t) sin (t) + sin (t) + cos (t)) dt
= −12sin2 (t)− cos (t) + sin (t)
¯π/2π/4
= −12+ 1 +
1
2
µ1√2
¶2+
√2
2−√2
2=3
4
10. We have ZC
F·d σ =ZC1+C2
F·d σ =ZC1
F·dσ +ZC2
F·dσ.
We can parametrize C1 byσ1 (x) = (x, 0) , 0 ≤ x ≤ 2
and C2 byσ2 (t) = (2, 0) + t (3− 2, 2− 0) = (2, 0) + t (1, 2) = (2 + t, 2t) ,
where 0 ≤ t ≤ 1.On C1,
σ01 (x) = i
and
F (σ1 (x)) = xj
Thus, ZC1
F·d σ =Z 2
0
F (σ1 (x)) · σ01 (x) dx =Z 2
0
(xj) · idx = 0
On C2,σ02 (t) = i+ 2j
and
F (σ2 (t)) = F (2 + t, 2t) = (2 + t) 2ti+ (2 + t− 2t) j=
¡4t+ 2t2
¢i+ (2− t) j
Thus, ZC2
F·d σ =Z 1
0
F (σ2 (t)) · σ02 (t) dt =
Z 1
0
¡¡4t+ 2t2
¢i+ (2− t) j¢ · (i+ 2j) dt
=
Z 1
0
¡4t+ 2t2 + 4− 2t¢ dt
=
Z 1
0
¡2t+ 2t2 + 4
¢dt
= t2 +2
3t3 + 4t
¯10
=17
3
Therefore, ZC
F·d σ =ZC1
F·dσ +ZC2
F·dσ = 0 + 173=17
3.
114 CHAPTER 14. VECTOR ANALYSIS
11. We have ZC
F ·Tds = −ZC2
F ·Tds,
where C2is the part of the circle of radius 2 centered at the origin traversed from (0, 2) to (−2, 0).We can parametrize C2 by
σ (θ) = (2 cos (θ) , 2 sin (θ)) ,π
2≤ θ ≤ π.
Thus,
σ0 (θ) = −2 sin (θ) i+ 2 cos (θ) j,so that ||σ0 (θ)|| = 2,
T (θ) =σ0 (θ)||σ0 (θ)|| = − sin (θ) i+ cos (θ) j
and
ds = ||σ0 (θ)|| dθ =q4 sin2 (θ) + 4 cos2 (θ)dθ = 2dθ.
We have
F (σ (θ)) = −2 (2 cos (θ)) (2 sin (θ)) i+ (2 sin (θ) + 1) j= −8 cos (θ) sin (θ) i+ (2 sin (θ) + 1) j
Thus,
(F ·T) (θ) = (−8 cos (θ) sin (θ) i+ (2 sin (θ) + 1) j) · (− sin (θ) i+ cos (θ) j)= 8 cos (θ) sin2 (θ) + 2 sin (θ) cos (θ) + cos (θ) .
Therefore,
−ZC2
F ·Tds = −Z π
θ=π/2
¡8 cos (θ) sin2 (θ) + 2 sin (θ) cos (θ) + cos (θ)
¢2dθ
= −Z π
θ=π/2
¡16 cos (θ) sin2 (θ) + 4 sin (θ) cos (θ) + 2 cos (θ)
¢dθ
= −Ã16
3sin3 (θ) + 2 sin2 (θ) + 2 sin (θ)
¯ππ/2
!=
16
3+ 2 + 2 =
28
3
12. We can parametrize C by
σ (t) = (1, 2, 3) + t (−1− 1,−2− 2,−3− 3)= (1, 2, 3)− t (2, 4, 6) = (1− 2t, 2− 4t, 3− 6t) ,
where 0 ≤ t ≤ 1.Thus,
σ0 (t) = −2i− 4j− 6kso that
||σ0 (t)|| = √4 + 16 + 36 = 2√14
Thus,
T (t) =σ0 (t)||σ0 (t)|| =
1
2√14(−2i− 4j− 6k)
14.2. LINE INTEGRALS 115
and
ds = ||σ0 (t)|| dt = 2√14dt.
We have
F (σ (t)) = F (1− 2t, 2− 4t, 3− 6t)= e1−2t+2−4ti+ (1− 2t) (3− 6t) j+ (2− 4t)k= e3−6ti+
¡12t2 − 12t+ 3¢ j+ (2− 4t)k
Therefore,
F (σ (t)) ·T (t)=
¡e3−6ti+
¡12t2 − 12t+ 3¢ j+ (2− 4t)k¢ ·µ 1
2√14(−2i− 4j− 6k)
¶=
1
2√14
¡−2e3−6t − 4 ¡12t2 − 12t+ 3¢− 6 (2− 4t)¢=
1
2√14
¡−2e3−6t − 48t2 + 72t− 24¢Thus, Z
C
F ·Tds =
Z 1
0
F (σ (t)) ·T (t) ds
=
Z 1
0
1
2√14
¡−2e3−6t − 48t2 + 72t− 24¢ 2√14dt=
Z 1
0
¡−2e3−6t − 48t2 + 72t− 24¢ dt=
1
3e3e−6t − 16t3 + 36t2 − 24t
¯10
=1
3e3e−6 − 16 + 36− 24− 1
3e3 =
1
3e−3 − 1
3e3 − 4
13.
a) ZC
F·d σ =ZC
−xydx+ 1
x2 + 1dy.
b) ZC
−xydx+ 1
x2 + 1dy =
Z −1−4
µ−xydx
dt+
1
x2 + 1
dy
dt
¶dt
=
Z −1−4
µ−t ¡t2¢ d
dt(t) +
1
t2 + 1
d
dt
¡t2¢¶dt
=
Z −1−4
µ−t3 + 2t
t2 + 1
¶dt
= −14t4 + ln
¡t2 + 1
¢¯−1−4
= −14+ ln (2) + 43 − ln (17) = ln
µ2
17
¶+255
4
14.
116 CHAPTER 14. VECTOR ANALYSIS
a) ZC
F·d σ =ZC
ydx− xdy
b) We can parametrize C by
σ (θ) = (cos (θ) , sin (θ)) , −π2≤ θ ≤ π
2.
Thus, ZC
ydx− xdy =
Z π/2
−π/2
µy (θ)
dx
dθ− x (θ) dy
dθ
¶dθ
=
Z π/2
−π/2(sin (θ) (− sin (θ))− cos (θ) cos (θ)) dθ
= −Z π/2
π/2
¡sin2 (θ) + cos2 (θ)
¢dθ
= −Z π/2
π/2
dθ = −³θ|π/2−π/2
´= −π
15. We can parametrize C by
σ (θ) = (cos (θ) , sin (θ)) , 0 ≤ θ ≤ π
2.
Thus, ZC
3x2dx− 2y3dy =
Z π/2
0
¡3 cos2 (θ) (− sin (θ))− 2 sin3 (θ) cos (θ)¢ dθ
= −Z π/2
0
¡3 cos2 (θ) sin (θ) + 2 sin3 (θ) cos (θ)
¢dθ
= −Ã− cos3 (θ) + 1
2sin4 (θ)
¯π/20
!
= −µ1
2+ 1
¶= −3
2
16. The equation of the ellipse can be written as
x2
4+ y2 = 1.
This suggests that we set
σ (θ) = (2 cos (θ) , sin (θ)) .
Indeed(2 cos (θ))2
4+ sin2 (θ) = cos2 (θ) + sin2 (θ) = 1.
Thus, −C is parametrized by
σ (θ) = (2 cos (θ) , sin (θ)) , 0 ≤ θ ≤ π
2
(since C is from (0, 1) to (2, 0).
14.2. LINE INTEGRALS 117
Therefore, ZC
exdx+ eydy = −Z π/2
0
³e2 cos(θ) (−2 sin (θ)) + esin(θ) cos (θ)
´dθ
=
Z π/2
0
e2 cos(θ)2 sin (θ) dθ −Z π/2
0
esin(θ) cos (θ) dθ
=
µ−e2 cos(θ)
¯π/20
¶−µesin(θ)
¯π/20
¶=
¡−1 + e2¢− (e− 1) = e2 − e17. We can parametrize C by
σ (x) =¡x, x2
¢, 0 ≤ x ≤ 2.
Thus, ZC
− sin (x) dx+ cos (x) dy =
Z π
0
(− sin (x) + cos (x) (2x)) dx
= −Z π
0
sin (x) dx+ 2
Z π
0
x cos (x) dx
= cos (x)|π0 + 2Z π
0
x cos (x) dx
= −2 + 2Z π
0
x cos (x) dx
In order to evaluate the last integral, we set u = x and dv = cos (x) dx. Thus,
du = dx and v =
Zcos (x) dx = sin (x) .
Therefore, Z π
0
x cos (x) dx = x sin (x)|π0 −Z π
0
sin (x) dx = cos (x)|π0 = −2.
Thus, ZC
− sin (x) dx+ cos (x) dy = −2 + 2Z π
0
x cos (x) dx
= −2 + 2 (−2) = −6.
18. We can parametrize C by
σ (t) = t (2, 3, 4) = (2t, 3t, 4t) , 0 ≤ t ≤ 1.
Thus, ZC
x3dx+ y2dy + zdz =
Z 1
0
³(2t)
3(2) + (3t)
2(3) + (4t) (4)
´dt
=
Z 1
0
¡16t3 + 27t2 + 16t
¢dt
= 4t4 + 9t3 + 8t2¯10= 4 + 9 + 8 = 21.
118 CHAPTER 14. VECTOR ANALYSIS
14.3 Line Integrals of Conservative Vector Fields
1.
a)∂
∂y(2x− 3y) = −3 and ∂
∂x(−3x+ 4y − 8) = −3.
Since the above partial derivatives are equal F may be conservative.
b) We need to have
∂f
∂x(x, y) = 2x− 3y,
∂f
∂y(x, y) = −3x+ 4y − 8
From the first equation,
f (x, y) =
Z(2x− 3y) dx = x2 − 3yx+ g (y) .
Therefore,
−3x+ 4y − 8 = ∂f
∂y(x, y) = −3x+ dg (y)
dy
Thus,dg (y)
dy= 4y − 8⇒ g (y) =
Z(4y − 8) dy = 2y2 − 8y +K,
where K is an arbitrary constant.
Therefore,
f (x, y) = x2 − 3yx+ g (y) = x2 − 3yx+ 2y2 − 8y +Kis a potential for F (you can check that ∇f = F).2.
a) We have∂
∂y(ex cos (y)) = −ex sin (y)
and∂
∂x(ex sin (y)) = ex sin (y) .
We have
−ex sin (y) = ex sin (y)⇔ sin (y) = 0⇔ y = nπ, n = 0,±1,±2, . . .Since the necessary conditions for the existence of a potential function are satisfied only at
isolated points, F is not conservative.
3.
a) We have∂
∂y(ex sin (y)) = ex cos (y)
and∂
∂x(ex cos (y)) = ex cos (y) .
Since the abve partial derivatives are equal everywhere, F may be conservative.
14.3. LINE INTEGRALS OF CONSERVATIVE VECTOR FIELDS 119
b) We need to have
∂f
∂x(x, y) = ex sin (y) ,
∂f
∂y(x, y) = ex cos (y) .
From the first equation,
f (x, y) =
Zex sin (y) dx = ex sin (y) + g (y)
⇒ex cos (y) =
∂f
∂y(x, y) = ex cos (y) +
dg (y)
dy⇒
dg (y)
dy= 0⇒ g (y) = K,
where K is an arbitrary constant. Thus,
f (x, y) = ex sin (y) +K
is a is a potential for F (confirm).
4.
a)
∇×F (x, y, z) =
¯¯ i j k
∂x ∂y ∂z− cos (z) e−x−y − cos (z) e−x−y − sin (z) e−x−y
¯¯
=
¯∂y ∂z
− cos (z) e−x−y − sin (z) e−x−y¯i
−¯
∂x ∂z− cos (z) e−x−y − sin (z) e−x−y
¯j
+
¯∂x ∂y
− cos (z) e−x−y − cos (z) e−x−y¯k
=¡−∂y sin (z) e−x−y + ∂z cos (z) e
−x−y¢ i− ¡−∂x sin (z) e−x−y + ∂z cos (z) e
−x−y¢ j+¡−∂x cos (z) e−x−y + ∂y cos (z) e
−x−y¢k=
¡sin (z) e−x−y − sin (z) e−x−y¢ i− ¡sin (z) e−x−y − sin (z) e−x−y¢ j+¡cos (z) e−x−y − cos (z) e−x−y¢k
= 0
Thus, F may be conservative.
b) We need to have
∂f
∂x(x, y, z) = − cos (z) e−x−y,
∂f
∂y(x, y, z) = − cos (z) e−x−y,
∂f
∂z(x, y, z) = − sin (z) e−x−y.
120 CHAPTER 14. VECTOR ANALYSIS
From the first equation,
f (x, y, z) = −Zcos (z) e−x−ydx = − cos (z) e−y
Ze−xdx
= cos (z) e−ye−x + g (y, z)= cos (z) e−x−y + g (y, z) .
From the second equation,
− cos (z) e−x−y = ∂f
∂y(x, y, z) = − cos (z) e−x−y + ∂g
∂y(y, z)
⇒∂g
∂y(y, z) = 0
⇒g (y, z) = h (z) .
Therefore,
f (x, y, z) = cos (z) e−x−y + h (z) .
From the third equuation,
− sin (z) e−x−y = ∂f
∂z(x, y, z) = − sin (z) e−x−y + dh (z)
dz
⇒dh (z)
dz= 0⇒ h (z) = K,
where K is an arbitrary constant. Thus,
f (x, y, z) = cos (z) e−x−y
is a is a potential for F (confirm).
5.
a) We need to have∂f
∂x(x, y) = xy2 and
∂f
∂y(x, y) = x2y.
From the first equation,
f (x, y) =
Zxy2dx =
1
2x2y2 + g (y) .
Therefore,∂f
∂y(x, y) = x2y +
dg (y)
dy.
From the second equation,
x2y =∂f
∂y(x, y) = x2y +
dg (y)
dy
⇒dg (y)
dy= 0⇒ g (y) = K,
where K is an arbitrary constant. We can set K = 0. Thus,
f (x, y) =1
2x2y2
14.3. LINE INTEGRALS OF CONSERVATIVE VECTOR FIELDS 121
is a potential for F (confirm by differentiation).
b) ZC
F · dσ = f (2, 1)− f (0, 1) = 2− 0 = 2.
6.
a) We need to have∂f
∂x(x, y) = yexy − 1 and ∂f
∂y(x, y) = xexy
From the first equation,
f (x, y) =
Z(yexy − 1) dx = exy − x+ g (y)
Therefore,∂f
∂y(x, y) = xexy +
dg (y)
dy
From the second equation,
xexy =∂f
∂y(x, y) = xexy +
dg (y)
dy
⇒dg (y)
dy= 0⇒ g (y) = K.
We can set K = 0. Thus,f (x, y) = exy − x
is a potential for F.
b) ZC
F · dσ = f (4, ln (2))− f (0, 1)
=³e4 ln(2) − 4
´− 1 = 24 − 5 = 11
7.
a) We need to have
∂f
∂x(x, y, z) = yz,
∂f
∂y(x, y, z) = xz,
∂f
∂z(x, y, z) = xy + 2z.
From the first equation,
f (x, y, z) =
Zyzdx = xyz + g (y, z) .
Thus,∂f
∂y(x, y, z) = xz +
∂g
∂y(y, z) .
From the second equation,
xz =∂f
∂y(x, y, z) = xz +
∂g
∂y(y, z)
⇒∂g
∂y(y, z) = 0⇒ g (y, z) = h (z) .
122 CHAPTER 14. VECTOR ANALYSIS
Thus,
f (x, y, z) = xyz + h (z) .
Therefore,∂f
∂z(x, y, z) = xy +
dh (z)
dz.
From the third equation,
xy + 2z =∂f
∂z(x, y, z) = xy +
dh (z)
dz
⇒dh (z)
dz= 2z ⇒ h (z) = z2 +K.
Thus, we can set
f (x, y, z) = xyz + z2.
b) ZC
F · dσ = f (4, 6, 3)− f (1, 0,−2)=
¡(4) (6) (3) + 32
¢− (4) = 778. We have
df =∂f
∂x(x, y) dx+
∂f
∂y(x, y) dy =
y
x2 + y2dx− x
x2 + y2dy
⇔∂f
∂x(x, y) =
y
x2 + y2and
∂f
∂y(x, y) = − x
x2 + y2.
From the first equation,
f (x, y) =
Zy
x2 + y2dx =
Z1
(x/y)2 + 1
µ1
y
¶dx
We set u = x/y so that du = dx/y. Thus,
f (x, y) =
Z1
(x/y)2 + 1
µ1
y
¶dx =
Z1
u2 + 1du
= arctan (u) + g (y) = arctan (x/y) + g (y) .
Therefore,∂f
∂y(x, y) =
1
1 +x2
y2
µ− xy2
¶+dg (y)
dy= − x
x2 + y2+dg (y)
dy.
From the second equation,
− x
x2 + y2=
∂f
∂y(x, y) = − x
x2 + y2+dg (y)
dy
⇒dg (y)
dy= 0⇒ g (y) = K.
We can set K = 0 and set
f (x, y) = arctan
µx
y
¶.
14.3. LINE INTEGRALS OF CONSERVATIVE VECTOR FIELDS 123
Since we have y > 0 on C and C joins (0, 1) to (1, 1) we haveZC
y
x2 + y2dx− x
x2 + y2dy =
ZC
d arctan
µx
y
¶= arctan (1)− arctan (0) = π
4.
9. We have
df =∂f
∂x(x, y) dx+
∂f
∂y(x, y) dy =
y2
1 + x2dx+ 2y arctan (x) dy
⇔∂f
∂x(x, y) =
y2
1 + x2and
∂f
∂y(x, y) = 2y arctan (x) .
From the first equation,
f (x, y) =
Zy2
1 + x2dx = y2 arctan (x) + g (y) .
Therefore,∂f
∂y(x, y) = 2y arctan (x) +
dg (y)
dy.
From the second equation,
2y arctan (x) =∂f
∂y(x, y) = 2y arctan (x) +
dg (y)
dy
⇒dg (y)
dy= 0⇒ g (y) = K.
Thus, we can set K = 0 andf (x, y) = y2 arctan (x) .
Therefore, ZC
y2
1 + x2dx+ 2y arctan (x) dy =
ZC
df
= f (1, 2)− f (0, 0)= 4 arctan (1) = 4
³π4
´= π.
10. We have
df =∂f
∂xdx+
∂f
∂ydy +
∂f
∂z= y2 cos (z) dx+ 2xy cos (z) dy − xy2 sin (z) dz
⇔∂f
∂x= y2 cos (z) ,
∂f
∂y= 2xy cos (z) ,
∂f
∂z= −xy2 sin (z)
From the first equuation,
f (x, y, z) =
Zy2 cos (z) dx = xy2 cos (z) + g (y, z) .
Therefore,∂f
∂y(x, y, z) = 2xy cos (z) +
∂g (y, z)
∂y.
124 CHAPTER 14. VECTOR ANALYSIS
From the second equation,
2xy cos (z) =∂f
∂y(x, y, z) = 2xy cos (z) +
∂g (y, z)
∂y
⇒∂g (y, z)
∂y= 0⇒ g (y, z) = h (z) .
Thus,
f (x, y, z) = xy2 cos (z) + h (z) .
Therefore,∂f
∂z(x, y, z) = −xy2 sin (z) + dh (z)
dz.
From the third equation,
−xy2 sin (z) = −xy2 sin (z) + dh (z)dz
⇒ dh (z)
dz= 0.
Therefore, we can set h (z) = 0 and
f (x, y, z) = xy2 cos (z)
Then ZC
y2 cos (z) dx+ 2xy cos (z) dy − xy2 sin (z) dz =
ZC
df
= f (1, 1,π)− f (0, 0, 0)= cos (π) = −1.
14.4 Parametrized Surfaces and Tangent Planes
1.
a) We have
∂Φ
∂u(u, v) = −3 sin (u) j+ 3 cos (u)k,
∂Φ
∂v(u, v) = i
Therefore,
∂Φ
∂u
³π6, 1´= −3 sin
³π6
´j+ 3 cos
³π6
´k = −3
2j+
3√3
2k,
and∂Φ
∂v
³π6, 1´= i.
Thus,
N³π6, 1´
=∂Φ
∂u
³π6, 1´× ∂Φ
∂v
³π6, 1´
=
Ã−32j+
3√3
2k
!× i
=
¯¯ i j k
0 −32 3√3
21 0 0
¯¯
=
¯−32 3
√32
0 0
¯i−
¯0 3
√32
1 0
¯j+
¯0 −321 0
¯k =
3√3
2j+
3
2k
14.4. PARAMETRIZED SURFACES AND TANGENT PLANES 125
b) We have
P0 = Φ³π6, 1´=³1, 3 cos
³π6
´, 3 sin
³π6
´´=
Ã1,3√3
2,3
2
!.
Therefore, the required tangent plane is the set of points P = (x, y, z) such that
N³π6, 1´·−−→P0P = 0
⇔ Ã3√3
2j+
3
2k
!·Ã(x− 1) i+
Ãy − 3
√3
2
!j+
µz − 3
2
¶k
!= 0
⇔3√3
2
Ãy − 3
√3
2
!+3
2
µz − 3
2
¶= 0
2.
a) We have∂Φ
∂u(u, v) = 2ui+ cos (v) j+ sin (v)k
and∂Φ
∂v(u, v) = −u sin (v) j+ u cos (v)k.
Therefore,
∂Φ
∂u
³3,π
3
´= 6i+
1
2j+
√3
2k
and
∂Φ
∂v
³3,π
3
´= −3
Ã√3
2
!j+ 3
µ1
2
¶k = −3
√3
2j+
3
2k
Thus,
N³3,π
3
´=
∂Φ
∂u
³3,π
3
´× ∂Φ
∂v
³3,π
3
´=
Ã6i+
1
2j+
√3
2k
!×Ã−3√3
2j+
3
2k
!
=
¯¯ i j k
6 12
√32
0 −3√32
32
¯¯
=
¯¯ 1
2
√32
−3√32
32
¯¯ i−
¯6
√32
0 32
¯j+
¯6 1
2
0 −3√3
2
¯k
= 3i−9j− 9√3k.
b) We have
P0 = Φ³3,π
3
´=³9, 3 cos
³π3
´, 3 sin
³π3
´´=
Ã9,3
2,3√3
2
!Therefore, the required tangent plane is the set of points P = (x, y, z) such that
N³3,π
3
´·−−→P0P = 0
126 CHAPTER 14. VECTOR ANALYSIS
⇐⇒ ³3i−9j− 9
√3k´·Ã(x− 9) i+
µy − 3
2
¶j+
Ãz − 3
√3
2
!k
!= 0
⇐⇒3 (x− 8)− 9
µy − 3
2
¶− 9√3
Ãz − 3
√3
2
!= 0.
3.
a) We have∂Φ
∂r(r, θ) = 3 cos (θ) i+ 2rj+ 2 sin (θ)k
and∂Φ
∂θ(r, θ) = −3r sin (θ) i+ 2r cos (θ)k.
Therefore,
∂Φ
∂r
³2,π
4
´=3√2
2i+ 4j+
√2k
and∂Φ
∂θ
³2,π
4
´= −3
√2i+ 2
√2k.
Thus,
N³2,π
4
´=
∂Φ
∂r
³2,π
4
´× ∂Φ
∂θ
³2,π
4
´=
Ã3√2
2i+ 4j+
√2k
!׳−3√2i+ 2
√2k´
=
¯¯ i j k3√22 4
√2
−3 0 2√2
¯¯
=
¯4√2
0 2√2
¯i−
¯¯ 3√22
√2
−3 2√2
¯¯ j+
¯3√2
2 4−3 0
¯k
= 8√2i−
³3√2 + 6
´j+ 12k
b) We have
Φ³2,π
4
´=³3√2, 4, 2
√2´
Therefore, he required tangent plane is the set of points (x, y, z) such that³8√2i−
³3√2 + 6
´j+ 12k
´·³³x− 3
√2´i+ (y − 4) j+
³z − 2
√2´k´= 0
⇔8√2³x− 3
√2´−³3√2 + 6
´(y − 4) + 12
³z − 2
√2´= 0.
4.
a) We have∂Φ
∂u(u, v) = sinh (u) cos (v) i+ cosh (u) j+ sinh (u) sin (v)k
and∂Φ
∂v(u, v) = − cosh (u) sin (v) i+ cosh (u) cos (v)k.
14.4. PARAMETRIZED SURFACES AND TANGENT PLANES 127
Therefore,∂Φ
∂u
³1,π
2
´= cosh (1) j+ sinh (1)k
and∂Φ
∂v
³1,π
2
´= − cosh (1) i.
Thus,
N³1,π
2
´=
∂Φ
∂u
³1,π
2
´× ∂Φ
∂v
³1,π
2
´= (cosh (1) j+ sinh (1)k)× (− cosh (1) i)
=
¯¯ i j k
0 cosh (1) sinh (1)− cosh (1) 0 0
¯¯
=
¯cosh (1) sinh (1)0 0
¯i−
¯0 sinh (1)
− cosh (1) 0
¯j+
¯0 cosh (1)
− cosh (1) 0
¯k
= − sinh (1) cosh (1) j+cosh2 (1)k.b) We have
P0 = Φ³1,π
2
´= (0, sinh (1) , cosh (1)) .
Therefore, he required tangent plane is the set of points (x, y, z) such that¡− sinh (1) cosh (1) j+cosh2 (1)k¢ · (xi+ (y − sinh (1)) j+ (z − cosh (1))k) = 0⇔
− sinh (1) cosh (1) (y − sinh (1)) + cosh2 (1) (z − cosh (1)) = 0.5.
a) We have
∂Φ
∂ρ(ρ, θ) =
1
2cos (θ) i+
1
2sin (θ) j+
√3
2k
and∂Φ
∂θ(ρ, θ) = −1
2ρ sin (θ) i+
1
2ρ cos (θ) j.
Therefore,
∂Φ
∂ρ
³2,π
3
´=1
4i+
√3
4j+
√3
2k
and∂Φ
∂θ
³2,π
3
´= −√3
2i+1
2j
Thus,
N³2,π
3
´=
Ã1
4i+
√3
4j+
√3
2k
!×Ã−√3
2i+1
2j
!
=
¯¯ i j k
14
√34
√32
−√32
12 0
¯¯
=
¯ √34
√32
12 0
¯i−
¯¯ 1
4
√32
−√32 0
¯¯ j+
¯¯ 1
4
√34
−√32
12
¯¯k
= −√3
4i−34j+
1
2k
128 CHAPTER 14. VECTOR ANALYSIS
b) We have
Φ³2,π
3
´=
Ã1
2,
√3
2,√3
!Therefore, he required tangent plane is the set of points (x, y, z) such thatÃ
−√3
4i−34j+
1
2k
!·Ãµ
x− 12
¶i+
Ãy −√3
2
!j+
³z −√3´k
!= 0
⇐⇒−√3
4
µx− 1
2
¶− 34
Ãy −√3
2
!+1
2
³z −√3´= 0.
6. We have∂Φ
∂φ(φ, θ) = 2 cos (φ) cos (θ) i+ cos (φ) sin (θ) j− 1
3sin (φ)k
and∂Φ
∂θ(φ, θ) = −2 sin (φ) sin (θ) i+ sin (φ) cos (θ) j
Therefore,
∂Φ
∂φ
³π4,π
2
´=
√2
2j− 1
3k
and∂Φ
∂θ
³π4,π
2
´= −√2i
Thus,
N³π4,π
2
´=
Ã√2
2j− 1
3k
!׳−√2i´
=
¯¯ i j k
0√22 − 13
−√2 0 0
¯¯
=
¯ √22 −130 0
¯i−
¯0 −13−√2 0
¯j+
¯¯ 0
√22
−√2 0
¯¯k
=
√2
3j+ k
b) We have
Φ³π4,π
2
´=
Ã0,
√2
2, 0
!Therefore, he required tangent plane is the set of points (x, y, z) such thatÃ√
2
3j+ k
!·Ãxi+
Ãy −√2
2
!j+ zk
!= 0
⇐⇒ √2
3
Ãy −√2
2
!+ z = 0
7.
14.4. PARAMETRIZED SURFACES AND TANGENT PLANES 129
a) We have∂Ω
∂x(x, θ) = i+ ex sin (θ) j+ ex cos (θ)k
and∂Ω
∂θ(x, θ) = ex cos (θ) j− ex sin (θ)k.
Therefore,
∂Ω
∂x
³1,π
6
´= i+
1
2ej+
√3
2ek
and∂Ω
∂θ
³1,π
6
´=
√3
2ej− 1
2ek
Thus,
N³1,π
6
´=
Ãi+
1
2ej+
√3
2ek
!×Ã√
3
2ej− 1
2ek
!
=
¯¯ i j k
1 12e
√32 e
0√32 e −12e
¯¯
=
¯¯ 1
2e√32 e√
32 e −12e
¯¯ i−
¯1
√32 e
0 −12e¯j+
¯1 1
2e
0√32 e
¯k
= −e2i+ 12ej+
√3
2k
b) We have
Ω³1,π
6
´=
Ã1,1
2e,
√3
2e
!.
Therefore, he required tangent plane is the set of points (x, y, z) such thatÃ−e2i+ 1
2ej+
√3
2k
!·Ã(x− 1) i+
µy − 1
2e
¶j+
Ãz −√3
2e
!k
!= 0
⇐⇒−e2 (x− 1) + 1
2e
µy − 1
2e
¶+
√3
2
Ãz −√3
2e
!= 0.
8.
a) We have∂Ω
∂x(x, θ) = cos (θ) i+ sin (θ) j+ exk
and∂Ω
∂θ(x, θ) = −x sin (θ) i+ x cos (θ) j.
Therefore,∂Ω
∂x
³1,π
2
´= j+ ek
and∂Ω
∂θ
³1,π
2
´= −i
130 CHAPTER 14. VECTOR ANALYSIS
Thus,
N³1,π
2
´= (j+ ek)× (−i)
=
¯¯ i j k
0 1 e−1 0 0
¯¯
=
¯1 e0 0
¯i−
¯0 e−1 0
¯j+
¯0 1−1 0
¯k
= ej+ k
b) We have
Ω³1,π
2
´= (0, 1, e) .
Therefore, he required tangent plane is the set of points (x, y, z) such that
(ej+ k) · (xi+ (y − 1) j+ (z − e)k) = 0
⇐⇒e (y − 1) + (z − e) = 0
14.5 Surface Integrals
1 (a cylinder)
Φ (u, v) = (v, 3 cos (u) , 3 sin (u)) , −4 ≤ v ≤ 4, 0 ≤ u ≤ 2π.
\We have∂Φ
∂u(u, v) = −3 sin (u) j+ 3 cos (u)k,
∂Φ
∂v(u, v) = i
Therefore,
N (u, v) =∂Φ
∂u(u, v)× ∂Φ
∂v(u, v)
= (−3 sin (u) j+ 3cos (u)k)× i
=
¯¯ i j k
0 −3 sin (u) 3 cos (u)1 0 0
¯¯
=
¯ −3 sin (u) 3 cos (u)0 0
¯i−
¯0 3 cos (u)1 0
¯j+
¯0 −3 sin (u)1 0
¯k
= −3 cos (u) j+ 3 sin (u)k
Thus,
||N (u, v)|| =q9 cos2 (u) + 9 sin2 (u) = 3.
Therefore the area of the surface isZ 2π
u=0
Z 4
v=−43dvdu = 3 (8) (2π) = 48π.
14.5. SURFACE INTEGRALS 131
2 (a paraboloid)
Φ (u, v) =¡u2, u cos (v) , u sin (v)
¢, 0 ≤ u ≤ 3, 0 ≤ v ≤ 2π.
We have∂Φ
∂u(u, v) = 2ui+ cos (v) j+ sin (v)k
and∂Φ
∂v(u, v) = −u sin (v) j+ u cos (v)k.
Therefore,
N (u, v) =∂Φ
∂u(u, v)× ∂Φ
∂v(u, v)
= (2ui+ cos (v) j+ sin (v)k)× (−u sin (v) j+ u cos (v)k)
=
¯¯ i j k
2u cos (v) sin (v)0 −u sin (v) u cos (v)
¯¯
=
¯cos (v) sin (v)−u sin (v) u cos (v)
¯i−
¯2u sin (v)0 u cos (v)
¯j+
¯2u cos (v)0 −u sin (v)
¯k
=¡u cos2 (v) + u sin2 (v)
¢i−2u2 cos (v) j− 2u2 sin (v)k
= ui−2u2 cos (v) j− 2u2 sin (v)k.
Thus,
||N (u, v)|| =qu2 + 4u4 cos2 (v) + 4u4 sin2 (v) =
pu2 + 4u4
Therefore, the area of the surface isZ 3
u=0
Z 2π
v=0
pu2 + 4u4dudv =
Z 3
u=0
Z 2π
v=0
up1 + 4u2dudv
= 2π
Z 3
u=0
up1 + 4u2du.
We set w = 1 + 4u2 so that dw = 8udu. Thus,
2π
Z 3
u=0
up1 + 4u2du =
π
4
Z w=37
w=1
w1/2dw
=π
4
Ã2
3w3/2
¯371
!=
π
6
³373/2 − 1
´.
3 (a cone)
Φ (ρ, θ) =
Ã1
2ρ cos (θ) ,
1
2ρ sin (θ) ,
√3
2ρ
!where 0 ≤ ρ ≤ 4 and 0 ≤ θ ≤ 2π.We have
∂Φ
∂ρ(ρ, θ) =
1
2cos (θ) i+
1
2sin (θ) j+
√3
2k
and∂Φ
∂θ(ρ, θ) = −1
2ρ sin (θ) i+
1
2ρ cos (θ) j.
132 CHAPTER 14. VECTOR ANALYSIS
Therefore,
N (ρ, θ) =
Ã1
2cos (θ) i+
1
2sin (θ) j+
√3
2k
!×µ−12ρ sin (θ) i+
1
2ρ cos (θ) j
¶
=
¯¯ i j k
12 cos (θ)
12 sin (θ)
√32−12ρ sin (θ) 1
2ρ cos (θ) 0
¯¯
=
¯12 sin (θ)
√32
12ρ cos (θ) 0
¯i−
¯12 cos (θ)
√32−12ρ sin (θ) 0
¯j+
¯12 cos (θ)
12 sin (θ)−12ρ sin (θ) 12ρ cos (θ)
¯k
= −√3
4ρ cos (θ) i+
√3
4ρ sin (θ) j+
µ1
4ρ sin2 (θ) +
1
4ρ cos2 (θ)
¶k
= −√3
4ρ cos (θ) i+
√3
4ρ sin (θ) j+
1
4ρk.
Thus,
||N (ρ, θ)|| =r3
16ρ2 cos2 (θ) +
3
16ρ2 sin2 (θ) +
1
16ρ2 =
1
4
p4ρ2 =
1
2ρ.
Therefore, the area of the surface isZ θ=2π
θ=0
Z ρ=4
ρ=0
1
2ρdρdθ = 2π
µZ ρ=4
ρ=0
1
2ρdρ
¶= 2π
Ã1
4ρ2¯40
!= 8π.
4 (an ellipsoid)
Φ (φ, θ) =
µ2 sin (φ) cos (θ) , sin (φ) sin (θ) ,
1
3cos (φ)
¶,
where 0 ≤ φ ≤ π and 0 ≤ θ ≤ 2π.We have
∂Φ
∂φ(φ, θ) = 2 cos (φ) cos (θ) i+ cos (φ) sin (θ) j− 1
3sin (φ)k
and∂Φ
∂θ(φ, θ) = −2 sin (φ) sin (θ) i+ sin (φ) cos (θ) j
Therefore,
N (φ, θ) =
µ2 cos (φ) cos (θ) i+ cos (φ) sin (θ) j− 1
3sin (φ)k
¶× (−2 sin (φ) sin (θ) i+ sin (φ) cos (θ) j)
=
¯¯ i j k
2 cos (φ) cos (θ) cos (φ) sin (θ) −13 sin (φ)−2 sin (φ) sin (θ) sin (φ) cos (θ) j 0
¯¯
=
¯cos (φ) sin (θ) −13 sin (φ)sin (φ) cos (θ) j 0
¯i−
¯2 cos (φ) cos (θ) −13 sin (φ)−2 sin (φ) sin (θ) 0
¯j
+
¯2 cos (φ) cos (θ) cos (φ) sin (θ)−2 sin (φ) sin (θ) sin (φ) cos (θ) j
¯k
=1
3sin2 (φ) cos (θ) i− 2
3sin2 (φ) sin (θ) j+
¡2 sin (φ) cos (φ) cos2 (θ) + 2 sin (φ) cos (φ) sin2 (θ)
¢k
=1
3sin2 (φ) cos (θ) i− 2
3sin2 (φ) sin (θ) j+2 sin (φ) cos (φ)k.
14.5. SURFACE INTEGRALS 133
Thus,
||N (φ, θ)|| =
r1
9sin4 (φ) cos2 (θ) +
4
9sin4 (φ) sin2 (θ) + 4 sin2 (φ) cos2 φ
=
ssin4 (φ)
µ1
9cos2 (θ) +
4
9sin2 (θ)
¶+ 4 sin2 (φ) cos2 φ
= sin (φ)
ssin2 (φ)
µ1
9cos2 (θ) +
4
9sin2 (θ)
¶+ 4cos2 (φ)
Therefore, the area of the surface is
Z θ=2π
θ=0
Z φ=π
φ=0
sin (φ)
ssin2 (φ)
µ1
9cos2 (θ) +
4
9sin2 (θ)
¶+ 4 cos2 (φ)dφdθ
5 (a surface of revolution)
Ω (x, θ) = (x, ex sin (θ) , ex cos (θ)) ,
where 0 ≤ x ≤ 2, 0 ≤ θ ≤ 2π.We have
∂Ω
∂x(x, θ) = i+ ex sin (θ) j+ ex cos (θ)k
and∂Ω
∂θ(x, θ) = ex cos (θ) j− ex sin (θ)k.
Therefore,
N (x, θ) = (i+ ex sin (θ) j+ ex cos (θ)k)× (ex cos (θ) j− ex sin (θ)k)
=
¯¯ i j k
1 ex sin (θ) ex cos (θ)0 ex cos (θ) −ex sin (θ)
¯¯
=
¯ex sin (θ) ex cos (θ)ex cos (θ) −ex sin (θ)
¯i−
¯1 ex cos (θ)0 −ex sin (θ)
¯j+
¯1 ex sin (θ)0 ex cos (θ)
¯k
=¡−e2x sin2 (θ)− e2x cos2 (θ)¢ i+ ex sin (θ) j+ ex cos (θ)k
= −e2xi+ ex sin (θ) j+ ex cos (θ)k
Thus,
||N (x, θ)|| =qe4x + e2x sin2 (θ) + e2x cos2 (θ) =
pe4x + e2x = ex
pe2x + 1.
Therefore, the area of the surface isZ θ=2π
θ=0
Z x=2
x=0
expe2x + 1dxdθ = 2π
Z x=2
x=0
expe2x + 1dx
We have Zexpe2x + 1dx =
1
2expe2x + 1 +
1
2arcsinh (ex)
134 CHAPTER 14. VECTOR ANALYSIS
(you can set u = ex so that the integrand takes the form√1 + u2du: Then set u = sinh (v)).
Therefore,
2π
Z x=2
x=0
expe2x + 1dx = 2π
Ã1
2expe2x + 1 +
1
2arcsinh (ex)
¯20
!
= 2π
µ1
2e2p(e4 + 1) +
1
2arcsinh
¡e2¢− 1
2
√2− 1
2arcsinh (1)
¶6. The radius of the sphere is 3. As in the lecture notes,
N (φ, θ) = 9 sin (φ) (sin (φ) cos (θ) i+ sin (φ) sin (θ) j+ cos (φ)k)
and
||N (φ, θ)|| = 9 sin (φ) .Therefore,Z Z
S
¡x2 + y2
¢dS =
Z π
θ−0
Z π
φ=0
¡9 sin2 (φ) cos2 (θ) + 9 sin2 (φ) sin2 (θ)
¢ ||N (φ, θ)|| dφdθ
=
Z π
θ−0
Z π
φ=0
9 sin2 (φ)¡cos2 (θ) + sin2 (θ)
¢9 sin (φ) dφdθ
= 81
Z π
θ−0
Z π
φ=0
sin3 (φ) dφdθ
= 81π
Z π
φ=0
sin3 (φ) dφ
Now, Zsin3 (φ) dφ =
Zsin2 (φ) sin (φ) dφ =
Z ¡1− cos2 (φ)¢ sin (φ) dφ.
We set u = cos (φ) so that du = − sin (φ) dφ. Thus,Z ¡1− cos2 (φ)¢ sin (φ) = −Z ¡
1− u2¢ du = −u+ 13u3 = − cos (φ) + 1
3cos3 (φ) .
Therefore, Z ZS
¡x2 + y2
¢dS = 81π
Z π
φ=0
sin3 (φ) dφ
= 81π
Ã− cos (φ) + 1
3cos3 (φ)
¯φ=πφ=0
!
= 81π
µ1− 1
3+ 1− 1
3
¶= 81π
µ4
3
¶= 108π.
7. We have
N (u, v) =
¯¯ i j k
0 −2 sin (u) 2 cos (u)1 0 0
¯¯
=
¯ −2 sin (u) 2 cos (u)0 0
¯i−
¯0 2 cos (u)1 0
¯j+
¯0 −2 sin (u)1 0
¯k
= 2 cos (u) j+ 2 sin (u)k.
14.5. SURFACE INTEGRALS 135
Therefore,
||N (u, v)|| =q4 cos2 (u) + 4 sin2 (u) = 2.
Thus,
Z ZS
y2dS =
Z v=4
v=−4
Z u=π
u=0
cos2 (u) 2dudv = 16
Z u=π
u=0
cos2 (u) du
= 16
Z u=π
u=0
1 + cos (2u)
2du
= 8π + 8
Z π
0
cos (2u) du
= 8π + 8
µ1
2sin (2u)
¯π0
¶= 8π
8. We have
N (r, θ) =
¯¯ i j k
cos (θ) sin (θ) 0−r sin (θ) r cos (θ) 1
¯¯
=
¯sin (θ) 0r cos (θ) 1
¯i−
¯cos (θ) 0−r sin (θ) 1
¯j+
¯cos (θ) sin (θ)−r sin (θ) r cos (θ)
¯k
= sin (θ) i− cos (θ) j+ ¡r cos2 (θ) + r sin2 (θ)¢k= sin (θ) i− cos (θ) j+rk.
Thus,
||N (r, θ)|| =qsin2 (θ) + cos2 (θ) + r2 =
p1 + r2.
Therefore,
Z ZS
px2 + y2dS =
Z θ=2π
θ=0
Z r=4
r=0
qr2 cos2 (θ) + r2 sin2 (θ) ||N (r, θ)|| drdθ
=
Z θ=2π
θ=0
Z r=4
r=0
rp1 + r2dr
= 2π
Z r=4
r=0
rp1 + r2dr.
We set u = 1 + r2 so that du = 2rdr. Thus,
2π
Z r=4
r=0
rp1 + r2dr =
2π
2
Z u=17
u=1
u1/2du = π
Ã2
3u3/2
¯171
!=2π
3
³173/2 − 1
´.
9. S is the part of the graph of x = g (y, z) = 1 − y −z over the triangular region D in the
136 CHAPTER 14. VECTOR ANALYSIS
yz-plane that is bounded by the axes and the line z + y = 1. We haveZ ZS
xdS =
Z ZD
(1− y − z)√1 + 1 + 1dzdy
=√3
Z y=1
y=0
Z z=1−y
z=0
(1− y − z) dzdy
=√3
Z y=1
y=0
Ãz − yz − 1
2z2¯1−y0
dy
!
=√3
Z y=1
y=0
µ(1− y)− y (1− y)− 1
2(1− y)2
¶dy
=√3
Z y=1
y=0
µ1
2(y − 1)2
¶dy =
1
6
√3
10. The surface S is the graph of
z =p1− x2 − y2
over the region D that is the part of the unit circle x2 + y2 = 1 in the first quadrant. Thus,
Z ZS
z2dS =
Z ZD
¡1− x2 − y2¢
s1 +
µ∂z
∂x
¶2+
µ∂z
∂y
¶2dxdy
=
Z ZD
¡1− x2 − y2¢
vuut1 +Ã− xp1− x2 − y2
!2+
Ã− yp
1− x2 − y2
!2dxdy
=
Z ZD
¡1− x2 − y2¢s1 + x2 + y2
1− x2 + y2 dxdy
=
Z ZD
p1− x2 − y2dxdy.
In polar coordinates,Z ZD
p1− x2 − y2dxdy =
Z θ=π/2
θ=0
Z r=1
r=0
p1− r2rdrdθ
=π
2
µ1
3
¶=
π
6
(via the substitution u = 1− r2).11. Let D be the rectangle [0,π]× [−2, 2] in the uv-plane. We have
N (u, v) =
¯¯ i j k
− sin (u) 0 cos (u)0 1 0
¯¯
=
¯0 cos (u)1 0
¯i−
¯ − sin (u) cos (u)0 0
¯j+
¯ − sin (u) 00 1
¯k
= − cos (u) i− sin (u)k.
(Note that N is multiplied by −1 if we interchange the order of u and v).
14.5. SURFACE INTEGRALS 137
Therefore,Z ZS
(xi+ zk) · dS =
Z ZD
(cos (u) i+ sin (u)k) ·N (u, v) dudv
=
Z ZD
(cos (u) i+ sin (u)k) · (− cos (u) i− sin (u)k) dudv
=
Z ZD
¡− cos2 (u)− sin2 (u)¢ dudv= −
Z ZD
dudv = −4π.
12. Let D be the rectangle [0, 3]× [0, 4] in the yz-plane. We have
N (y, z) =
¯¯ i j k
0 1 00 1 1
¯¯ = i.
(Note that N is multiplied by −1 if we interchange the order of y and z).Therefore, Z Z
S
(yi+ xj+ zk) · dS =
Z ZD
(yi+ 2j+ zk) ·N (y, z) dydz
=
Z ZD
(yi+ 2j+ zk) · idydz
=
Z ZD
ydydz
=
Z z=4
z=0
Z y=3
y=0
ydydz
= 4
Ã1
2y2¯30
!= 18.
13. As in the lecture notes, we have
N (φ, θ) = 9 sin (φ) (sin (φ) cos (θ) i+ sin (φ) sin (θ) j+ cos (φ)k) = 3 sin (φ)Φ (φ, θ) ,
Therefore, ZS
xi+ yj+ zk
(x2 + y2 + z2)· dS =
Z π
θ=0
Z π
φ=0
Φ (φ, θ)
9·N (φ, θ) dφdθ
=
Z π
θ=0
Z π
φ=0
Φ (φ, θ)
9· 3 sin (φ)Φ (φ, θ) dφdθ
=
Z π
θ=0
Z π
φ=0
1
3sin (φ)Φ (φ, θ) ·Φ (φ, θ) dφdθ
=
Z π
θ=0
Z π
φ=0
1
3sin (φ) ||Φ (φ, θ)||2 dφdθ
=
Z 2π
θ=0
Z π
φ=0
1
3sin (φ) (9) dφdθ
= 3 (2π)
Z π
φ=0
sin (φ) dφ
= 6π (2) = 12π
138 CHAPTER 14. VECTOR ANALYSIS
14. We have
1− 12x− 1
2y = 0⇔ x+ y = 2.
Therefore, the projection of S onto the xy-plane is the triangular region D that is bounded by
the coordinate axes and the line x+ y = 2. Thus,Z ZS
(xi− zk) ·dS =
Z ZD
µxi−
µ1− 1
2x− 1
2y
¶k
¶·µ−∂z∂xi− ∂z
∂yj+ k
¶dxdy
=
Z ZD
µxi−
µ1− 1
2x− 1
2y
¶k
¶·µ1
2i+
1
2j+ k
¶dxdy
=
Z ZD
µ1
2x−
µ1− 1
2x− 1
2y
¶¶dxdy
=
Z ZD
µx+
1
2y − 1
¶dxdy
=
Z x=2
x=0
Z y=2−x
y=0
µx+
1
2y − 1
¶dydx
=
Z x=2
x=0
Ãxy +
1
4y2 − y
¯y=2−xy=0
!dx
=
Z x=2
x=0
µx (2− x) + 1
4(2− x)2 − (2− x)
¶dx
=
Z x=2
x=0
µ−34x2 + 2x− 1
¶dx = 0
15. The projection of S onto the xy-plane is the disk D of radius 2 centered at the origin. We
have
N (x, y) = −∂z∂xi− ∂z
∂yj+ k
=xp
4− x2 − y2 i+yp
4− x2 − y2 j+ k.
Thus, Z ZS
(xi+yj+ zk) · dS
=
Z ZD
³xi+yj+
p4− x2 − y2k
´·N (x, y) dxdy
=
Z ZD
³xi+yj+
p4− x2 − y2k
´·Ã
xp4− x2 − y2 i+
yp4− x2 − y2 j+ k
!dxdy
=
Z ZD
Ãx2p
4− x2 − y2 +y2p
4− x2 − y2 +p4− x2 − y2
!dxdy
=
Z ZD
Ãx2 + y2 + 4− x2 − y2p
4− x2 − y2
!dxdy
= 4
Z ZD
1p4− x2 − y2 dxdy.
14.5. SURFACE INTEGRALS 139
We transform to polar coordinates:
4
Z ZD
1p4− x2 − y2 dxdy = 4
Z 2π
θ=0
Z 2
r=0
r√4− r2 drdθ
= 8π
Z 2
r=0
r√4− r2 dr
= 16π
(via the substitution u = 4− r2).16. The projection of S onto the xy-plane is the unit disk D. We haveZ Z
S
(yj+ k) · dS =
Z ZD
(yj+ k) ·N (x, y) dxdy
=
Z ZD
(yj+ k) · (2xi+ 2yj+ k) dxdy
=
Z ZD
¡2y2 + 1
¢dxdy
=
Z θ=2π
θ=0
Z r=1
r=0
¡2r2 sin2 (θ) + 1
¢rdrdθ
=
Z θ=2π
θ=0
Z r=1
r=0
2r3 sin2 (θ) drdθ +
Z θ=2π
θ=0
Z r=1
r=0
rdrdθ
=
µZ r=1
r=0
2r3dr
¶ÃZ θ=2π
θ=0
sin2 (θ) dθ
!+ 2π
µ1
2
¶=
µ1
2
¶(π) + π =
1
2π
(you can make use of the identity sin2 (θ) = (1− cos (θ)) /2).17. We haveZ Z
S
(yzi+ xzj+ xyk) · dS =Z Z
S1
(yzi+ xzj+ xyk) · dS+Z Z
S2
(yzi+ xzj+ xyk) · dS.
We will evaluate the integrals separately.
As in Problem 10, on S1,
N (x, y) = −∂z∂xi− ∂z
∂yj+ k =
xp4− x2 − y2 i+
yp4− x2 − y2 j+ k,
and D is the disk of radius 2 centered at the origin. We haveZ ZS1
(yzi+ xzj+ xyk) · dS
=
Z ZD
³yp4− x2 − y2i+ x
p4− x2 − y2j+ xyk
´·Ã
xp4− x2 − y2 i+
yp4− x2 − y2 j+ k
!
=
Z ZD
3xydxdy
=
Z θ=2π
θ=0
Z 2
r=0
3 (r cos (θ)) (r sin (θ)) rdrdθ
= 3
µZ r=2
r=0
r3dr
¶µZ 2π
0
cos (θ) sin (θ) dθ
¶= 3 (4) (0) = 0.
140 CHAPTER 14. VECTOR ANALYSIS
The outward unit normal to S2 is -k. Therefore,Z ZS2
(yzi+ xzj+ xyk) · dS =
Z ZD
(yzi+ xzj+ xyk) · kdxdy
=
Z ZD
xydxdy = 0
Thus, Z ZS
(yzi+ xzj+ xyk) · dS = 0.
14.6 Green’s Theorem
1.
a) Let D be the disk that is bounded by the circle x2 + y2 = 4. ThenZC
y3dx− x3dy =
Z ZD
µ∂
∂x
¡−x3¢− ∂
∂y
¡y3¢¶dxdy
=
Z ZD
¡−3x2 − 3y2¢ dxdy= −3
Z ZD
¡x2 + y2
¢dxdy.
b) We transform the double integral to polar coordinates:
−3Z Z
D
¡x2 + y2
¢dxdy = −3
Z 2π
θ=0
Z 2
r=0
r2rdrdθ
= −6πÃ1
4r4¯20
!= −24π
2.
a) Let D be the triangular region with vertices (0, 0) , (2, 0) and (2, 4). ThenZC
xy2dx+ 2x2ydy =
Z ZD
µ∂
∂x
¡2x2y
¢− ∂
∂y
¡xy2
¢¶=
Z ZD
(4xy − 2xy) dxdy
=
Z ZD
2xydxdy
b) Since the equation of the line that joins (0, 0) to (2, 4) is y = 2x,Z ZD
2xydxdy =
Z x=2
x=0
µZ 2x
y=0
2xydy
¶dx =
Z x=2
x=0
³xy2
¯y=2xy=0
´dx
=
Z x=2
x=0
4x3dx = x4¯20= 16.
3.
14.6. GREEN’S THEOREM 141
a) Let D be the rectangular region with vertices (0, 0) , (5, 0) , (5,π) and (0,π). ThenZC
cos (y) dx+ x2 sin (y) dy =
Z ZD
µ∂
∂x
¡x2 sin (y)
¢− ∂
∂ycos (y)
¶dxdy
=
Z ZD
(2x sin (y) + sin (y)) dxdy
=
Z ZD
(2x+ 1) sin (y) dxdy.
b) Z ZD
(2x+ 1) sin (y) dxdy =
Z x=5
x=0
Z y=π
y=0
(2x+ 1) sin (y) dydx
=
µZ x=5
x=0
(2x+ 1) dx
¶µZ y=π
y=0
sin (y) dy
¶=
³x2 + x
¯50
´(− cos (y)|π0 )
= 30 (2) = 60.
4.
a) Let D be annular region bounded by the circles x2 + y2 = 1 an x2 + y2 = 4. ThenZC
xe−2xdx+¡x4 + 2x2y2
¢dy =
Z ZD
µ∂
∂x
¡x4 + 2x2y2
¢− ∂
∂y
µZC
xe−2x¶¶
dxdy
=
Z ZD
¡4x3 + 4xy2
¢dxdy = 4
Z ZD
x¡x2 + y2
¢dxdy
b) Let’s transform the double integral to polar coordinates:
4
Z ZD
x¡x2 + y2
¢dxdy = 4
Z θ=2π
θ=0
Z r=2
r=1
r4 cos (θ) drdθ
= 4
ÃZ θ=2π
θ=0
cos (θ) dθ
!µZ r=2
r=1
r4dr
¶
= 4³sin (θ)|2π0
´Ã 15r5¯21
!
= 4 (0)
µ25 − 15
¶= 0.
5.
a) Let D be the triangular region with vertices (0, 0) , (2, 6) and (2, 0). Note that C is the
negatively oriented boundary of D. Thus,ZC
F · dσ =
ZC
y2 cos (x) dx+¡x2 + 2y sin (x)
¢dy
= −Z Z
D
µ∂
∂x
¡x2 + 2y sin (x)
¢− ∂
∂y
¡y2 cos (x)
¢dxdy
¶= −
Z ZD
(2x+ 2y cos (x)− 2y cos (x)) dxdy
= −Z Z
D
2xdxdy
142 CHAPTER 14. VECTOR ANALYSIS
b) Since the line that joins (0, 0) to (2, 6) is y = 3x,
−Z Z
D
2xdxdy = −Z x=2
x=0
Z 3x
y=0
2xdydx
= −Z x=2
x=0
2x
µZ y=3x
y=0
dy
¶dx
= −Z x=2
x=0
2x (3x) dx
= −6Z 2
0
x2dx = −6Ãx3
3
¯20
!= −16.
6.
a) Let D be the disk bounded by the circle x2 + y2 = 25. ThenZC
F · dσ =
Z ¡ex + x2y
¢dx+
¡ey − xy2¢ dy
=
Z ZD
µ∂
∂x
¡ey − xy2¢− ∂
∂y
¡ex + x2y
¢¶dxdy
=
Z ZD
¡−y2 − x2¢ dxdy = −Z ZD
¡x2 + y2
¢dxdy
b) We transform the double integral to polar coordinates:
−Z Z
D
¡x2 + y2
¢dxdy = −
Z 2π
θ=0
Z 5
r=0
r3drdθ
= −µZ 2π
θ=0
dθ
¶µZ 5
r=0
r3dr
¶= −2π
µ54
4
¶= −625
2π
7. Let C2 be the positively oriented circle of radius a centered at the origin, and let D be the
region between C1 and C2. By Greens theorem,ZC1
F · dσ −ZC2
F · dσ =
Z ZD
µ∂
∂x
µy
x2 + y2
¶− ∂
∂y
µx
x2 + y2
¶¶dxdy
=
Z ZD
Ã− 2xy
(x2 + y2)2 +
2xy
(x2 + y2)2
!dxdy = 0.
Thus, ZC1
F · dσ =ZC2
F · dσ.
We can parametrize the circle C2 by
σ (θ) = (cos (θ) , sin (θ)) , 0 ≤ θ ≤ 2π.Therefore,
dσ
dθ= − sin (θ) i+ cos (θ) j
and
F (σ (θ)) = F (cos (θ) , sin (θ)) = cos (θ) i+ sin (θ) j
14.7. STOKES’ THEOREM 143
Thus,
F · dσdθ
= (cos (θ) i+ sin (θ) j) · (− sin (θ) i+ cos (θ) j)= − cos (θ) sin (θ) + sin (θ) cos (θ) = 0
Therefore, ZC1
F · dσ =ZC2
F · dσ = 0.
8. Let D be the triangular region with vertices (0, 0) , (1, 0) and (1, 2). We have
∇ · F (x, y) = ∂
∂x
¡x2y3
¢− ∂
∂y(xy) = 2xy3 − x.
Therefore, ZC
F · nds =
Z ZD
∇ · F (x, y) dxdy
=
Z ZD
¡2xy3 − x¢ dxdy
=
Z x=1
x=0
Z y=2x
y=0
¡2xy3 − x¢ dydx
=
Z x=1
x=0
Ã1
2xy4 − xy
¯2x0
!dx
=
Z x=1
x=0
¡−2x2 + 8x5¢ dx= −2
3x3 +
4
3x6¯10
=2
3
9. Let D be the disk bounded by the circle x2 + y2 = 4. We have
∇ · F (x, y) = ∂
∂x
¡x3¢+
∂
∂y
¡y3¢= 3x2 + 3y2
Therefore, ZC
F · nds =Z Z
D
∇ · F (x, y) dxdy =Z Z
D
3¡x2 + y2
¢dxdy.
We transform the double integral to polar coordinates:Z ZD
3¡x2 + y2
¢dxdy = 3
Z θ=2π
θ=0
Z r=2
r=0
r3drdθ
= 3 (2π)
Ã1
4r4¯20
!= 24π
14.7 Stokes’ Theorem
1. Z ZM
(∇×F) · ndS =ZC
F · dσ.
144 CHAPTER 14. VECTOR ANALYSIS
We can parametrize C by
σ (θ) = (4 cos (θ) , 4 sin (θ) , 0) , 0 ≤ θ ≤ 2π.
Thus,dσ
dθ= −4 sin (θ) i+ 4cos (θ) j,
and
F (σ (θ)) = 4 sin (θ) i+ 8 cos (θ) j
Therefore
F (σ (θ)) · dσdθ
= (4 sin (θ) i+ 8cos (θ) j) · (−4 sin (θ) i+ 4 cos (θ) j)= −16 sin2 (θ) + 32 cos2 (θ)
Thus ZC
F · dσ = −16Z 2π
0
sin2 (θ) dθ + 32
Z 2π
0
cos2 (θ) dθ = −16π + 32π = 16π.
2. Z ZM
(∇×F) · ndS =ZC
F · dσ.
We can parametrize C by
σ (θ) = (cos (θ) , sin (θ) , 1) , 0 ≤ θ ≤ 2π.
Thus,dσ
dθ= − sin (θ) i+ cos (θ) j,
and
F (σ (θ)) = sin (θ) i− cos (θ) j+ kTherefore
F (σ (θ)) · dσdθ
= (sin (θ) i− cos (θ) j+ k) · (− sin (θ) i+ cos (θ) j)= − sin2 (θ)− cos2 (θ) = −1.
Thus ZC
F · dσ = −Z 2π
0
dθ = −2π.
3. ZC
F · dσ =Z Z
M
(∇×F) · ndS
We have
∇×F (x, y, z) =
¯¯ i j k
∂x ∂y ∂zz x3 y2
¯¯
=
¯∂y ∂zx3 y2
¯i−
¯∂x ∂zz y2
¯j+
¯∂x ∂yz x3
¯k
= 2yi− j+ 3x2k
14.7. STOKES’ THEOREM 145
We also have n = k. ThusZM
(∇×F) · ndS =
Z ZM
¡2yi− j+ 3x2k¢ · kdS
=
Z ZM
3x2dS.
M can be parametrized by
Φ (x, y) = (x, y, 4) , (x, y) ∈ D,where D is the circle of radius 3 centered at the origin in the xy-plane. ThereforeZ Z
M
3x2dS =
Z ZD
3x2dxdy =
Z θ=2π
θ=0
Z r=3
r=0
3r2 cos2 (θ) rdrdθ
=
ÃZ θ=2π
θ=0
cos2 (θ) dθ
!µZ r=3
r=0
3r3dr
¶= (π)
µ243
4
¶=243
4π
4. ZC
F · dσ =Z Z
M
(∇×F) · ndS
We have
∇×F (x, y, z) =
¯¯ i j k
∂x ∂y ∂zz −x 2y
¯¯
=
¯∂y ∂z−x 2y
¯i−
¯∂x ∂zz 2y
¯j+
¯∂x ∂yz −x
¯k
= 2i+ j− k
M can be parametrized by
Φ (x, y) = (x, y, y + 2) , (x, y) ∈ D,
where D is the circle of radius 2 centered at the origin in the xy-plane. Therefore
N = −j+ k
Thus, ZM
(∇×F) · ndS =
ZD
(∇×F) ·Ndxdy
=
Z ZD
(2i+ j− k) · (−j+ k) dxy
=
Z ZD
−2dxdy= −2 (area of the disk of radius 2 )= −2 (4π) = −8π.
146 CHAPTER 14. VECTOR ANALYSIS
14.8 Gauss’ Theorem
1. We have
∇ · F (x, y, z) =∇ · (xi+ yj+ zk) = ∂
∂x(x) +
∂
∂y(y) +
∂
∂z(z) = 3.
Therefore Z ZM
F · ndS =
Z Z ZW
∇ · FdV
=
Z Z ZW
3dV
= 3 (volume of W ) = 3
µ4
3π¡43¢¶= 44π = 256π
2. We have
∇ · F (x, y, z) =∇ · ¡z3k¢ = ∂
∂z
¡z3¢= 3z2
Therefore Z ZM
F · ndS =Z Z Z
W
∇ · FdV =Z Z Z
W
3z2dV
We transform to spherical coordinates:Z Z ZW
3z2dV = 3
Z θ=2π
θ=0
Z φ=π
φ=0
Z ρ=2
ρ=0
(ρ cos (φ))2ρ2 sin (φ) dρdφdθ
= 2
ÃZ θ=2π
θ=0
dθ
!ÃZ φ=π
φ=0
cos2 (φ) sin (φ) dφ
!µZ ρ=2
ρ=0
ρ3dρ
¶= 2 (2π)
µ2
3
¶(4) =
32
3π
3. We have
∇ · F (x, y, z) =∇ · (xi+ yj+ zk) = ∂
∂x(x) +
∂
∂y(y) +
∂
∂z(z) = 3.
Therefore Z ZM
F · ndS =
Z Z ZW
∇ · FdV
=
Z Z ZW
3dV = 3 (volume of W ) = 3¡43¢= 192
4. We have
∇ · F (x, y, z) =∇ · ¡x2i¢ = ∂
∂x
¡x2¢= 2x
Therefore Z ZM
F · ndS =Z Z Z
W
∇ · FdV =
Z Z ZW
2xdV
=
Z x=1
x=0
Z y=1
y=0
Z z=1
z=0
2xdzdydx
=
Z x=1
x=0
2xdx = 1.