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Solutions Manual to Advanced Engineering Mathematics with MATLAB 5th Edition by Dean G. Duffy PDF | Comprehensive Step-by-Step Solutions and MATLAB Applications | Covers Differential Equations, Linear Algebra, Fourier and Laplace Transforms, Complex Varia

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The Solutions Manual to Advanced Engineering Mathematics with MATLAB (5th Edition) by Dean G. Duffy provides fully worked-out solutions to all exercises and MATLAB-based problems in the main textbook. It covers advanced topics such as differential equations, vector calculus, transform methods, and matrix computations. Designed for engineering and applied science students, this manual is widely used in top programs at MIT, Stanford, and Georgia Tech for mathematical modeling and simulation courses.

Meer zien Lees minder
Instelling
Structural Dynamics Concepts And Applications
Vak
Structural Dynamics Concepts and Applications

Voorbeeld van de inhoud

All Chapters Covered




SOLUTIONS

,Table of Contents
Chapter 1: First-Order Ordinary Differential
Equations 1 Chapter 2: Higher-Order Ordinary
Differential Equations Chapter 3: Linear Algebra
Chapter 4: Vector Calculus
Chapter 5: Fourier Series
Chapter 6: The Fourier
Transform
Chapter 7: The Laplace
Transform Chapter 8: The Wave
Equation Chapter 9: The Heat
Equation Chapter 10: Laplace’s
Equation
Chapter 11: The Sturm-Liouville
Problem Chapter 12: Special Functions
Appendix A: Derivation of the Laplacian in Polar Coordinates
Appendix B: Derivation of the Laplacian in Spherical Polar
Coordinates




@LECTJULIESOLUTIONSSTUVIA

, Solution Manual
Section 1.1

1. first-order, linear 2. first-order, nonlinear
3. first-order, nonlinear 4. third-order, linear
5. second-order, linear 6. first-order, nonlinear
7. third-order, nonlinear 8. second-order, linear
9. second-order, nonlinear 10. first-order, nonlinear
11. first-order, nonlinear 12. second-order, nonlinear
13. first-order, nonlinear 14. third-order, linear
15. second-order, nonlinear 16. third-order, nonlinear

Section 1.2

1. Because the differential equation can be rewritten e−y dy = xdx,
integra- tion immediately gives —e−y = 1 x2 — C, or y = — ln(C —
2
x2/2).

2. Separating variables, we have that dx/(1 + x2) = dy/(1 + y2).

Integrating this equation, we find that tan−1(x) tan−1—
(y) = tan(C),
or (x y)/(1+xy) = C.

3. Because the differential equation can be rewritten ln(x)dx/x = y dy,
inte- gration immediately2
gives 1 ln2(x)
2
+ C = 1 y2, or y2(x) — ln2(x)
= 2C.

4. Because the differential equation can be rewritten y2 dy = (x +
x3) dx, integration immediately gives y 3(x)/3 = x 2/2 + x4/4 + C.

5. Because the differential equation can be rewritten y dy/(2+y2) = xdx/(1+
x2), integration immediately gives 1 ln(2 + y2) = 1 ln(1 + x2) + 1 ln(C), or
2 2 2
2 + y2(x) = C(1 + x2).

6. Because the differential equation can be rewritten dy/y1/3 = x1/3
dx, integration immediately gives 3 y 2/3 = 3 x4/3 + 3 C, or y(x) = 1 x 4/3
3/2 2 4 2 2
+C .

1

,2 Advanced Engineering Mathematics with MATLAB

7. Because the differential equation can be rewritten e−y dy = ex dx,
integra- tion immediately gives —e−y = ex — C, or y(x) = — ln(C —
ex).

8. Because the differential equation can be rewritten dy/(y2 + 1) =
(x3 + 5) dx, integration immediately gives tan−1 (y) = 1 x4 + 5x +
C, or y(x) =
4
tan 41 x 4 + 5x + C .

9. Because the differential equation can be rewritten y2 dy/(b — ay3) = dt,
integration immediately gives ln[b — ay 3] yy0 = —3at, or (ay 3 — b)/(ay03 — b) =
e−3at.

10. Because the differential equation can be written du/u = dx/x2,
integra- tion immediately gives u = Ce−1/x or y(x) = x + Ce−1/x.

11. From the hydrostatic equation and ideal gas law, dp/p
— = g
dz/(RT ). Substituting for T (z),
dp g
=— dz.
p R(T0 — Γz)
Integrating from 0 to
z,

p(z) g T0 — p(z) T0 — Γz g/(RΓ)
ln = , = .
p0 l Γz p0 T0
n T0 o
RΓ r


12. For 0 < z < H, we simply use the previous problem. At z =
H, the pressure is
T0 — ΓH g/(RΓ)
p(H) = p0 .
T0
Then we follow the example in the text for an isothermal atmosphere for
z ≥ H.

13. Separating variables, we find that
dV dV R dV dt
2
= — =— .
V + RV /S V S(1 + RV/S) RC

Integration yields

V t
ln =— + ln(C).
1 + RV/S RC
Upon applying the initial conditions,

V0 RV0/S
V (t) = e−t/(RC) + e−t/(RC)V (t).
1 + RV0/S 1 + RV0/S




@LECTJULIESOLUTIONSSTUVIA

,Worked Solutions 3

Solving for V (t), we obtain

SV0 e−t/(RC)
V (t) = .
S + RV0 1 — e−t/(RC)

14. From the definition of γ, we can write the differential equation
A dT
+ T 4 = γ4,
B dt
or
B dT 1 dT dT
A dt = —
T 4 — γ4 =2γ2 T 2 + γ2 —T 2 — γ2
1 2γ dT dT dT
= — + .
3 2 2
4γ T + γ T — γ T + γ
The final answer follows from direction integration.

15. Separating the variables yields
dN d[ln(K/N )]
= b dt, or = —b dt.
N ln(K/N ) ln(K/N )

Integration leads
to
ln [ln(K/N )] — ln {ln[K/N (0)]} =
—bt

or
ln {ln(K/N )/ ln[K/N (0)]} = —

or
bt ln(K/N ) = ln[K/N (0)]e−bt

or
ln[N/N (0)] = ln[K/N (0)] 1 —
or
e−bt
}
N (t) = N (0) exp ln[K/N (0)] 1 — e−bt .

16. Separating the variables yields
dI β dI
— = —α dz.
I α 1 + βI/α

Integration leads to

I(z) 1 + βI(0)/α
ln = —αz,
1 + βI(z)/α I(0)

,4 Advanced Engineering Mathematics with MATLAB

or
I(z) I(0) αI(0)e−αz
= e−αz , or I(z) .
1 + βI(z)/α 1 + βI(0)/α = α + βI(0) [1 — e−αz ]


17. Separating the variables yields

d[X]
= k dt
([A]0 — [X]) ([B]0 — [X]) ([C]0 — [X])
d[X]
([A]0 — [B]0) ([A]0 — [C]0) ([A]0 — [X])
d[X]
+
([B]0 — [A]0) ([B]0 — [C]0) ([B]0 —
[X])
d[X] = k dt
+
([C]0 — [A]0) ([C]0 — [B]0) ([C]0 —
[X])
Integration yields

1 [A]0
ln
([A]0 — [B]0) ([A]0 — [C]0) [A]0 — [X]
1 [B]0
+ ln
([B]0 — [A]0) ([B]0 — [C]0) [B]0 — [X]
1 = kt.
+ ln
[C]0
([C]0 — [A]0) ([C]0 — [B]0) [C]0 — [X]


18. Separation of variables yields
d[X]
= (k1 + k2) dt.
α — [X]
Integrating both
sides,

ln(α — [X]) — ln(α — [X]0 ) = —(k1 + k2)t.

Because [X]0 = 0,
h i
α — [X] = αe−(k1+k2)t, or [X] = α 1 — e−(k 1+k 2)t .


Section 1.3

1. Because M (x, y) =— y and N (x, y) = x + y, we have that M (tx, ty) =
— ty = tM (x, y), and N (tx, ty) = tx + ty = tN (x, y). Therefore, the
differen- tial equation is homogeneous.




@LECTJULIESOLUTIONSSTUVIA

,Worked Solutions 5

Let y = ux. Substituting into the differential equation, (ux + x)(u dx +
xdu) = uxdx, or —u2xdx = (1 + u)x2 du, or

dx 1 1
— = + du.
x u u2
Integrating this last equation,
1 x
— ln |x| = ln(u) — — C, or ln |y| — = C.
u y

2. Because M (x, y) = —y x and N (x, y) = x + y, we have that M
(tx,— ty) = ty tx = tM (x, y), and N (tx, ty) = tx + ty = tN (x, y).
Therefore, the differential equation is homogeneous.
Let y = ux. Substituting into the differential equation,
— (u 1)xdx
+(u + 1)x(u dx + xdu) = 0, or
dx u+1
(u2 + 2u — 1) dx = —(u + 1)xdu, or — = du.
x u2 + 2u — 1
Integrating this last
equation,

y2 y
— ln |x| = 12 ln |u2 +2u—1|+C, or x
2
2
+ 2 — 1 = y2 +2xy —x 2 = C.
x x

3. Because M (x, y) = x2 + y2 and N (x, y) = 2xy, we have that M (tx,
ty) = t2x2 + t2y2 = t2(x2 + y2) = t2 M (x, y), and N (tx, ty) = 2t2xy = t2N
(x, y). Therefore, the differential equation is homogeneous.
Let y = ux. Substituting into the differential

equation, 2x(ux)(u dx + xdu) + (x2 +

x2u2) dx = 0

or
dx 2u
2xu du + (1 + 3u2) dx = 0, or =— du.
x 1 + 3u2
Integrating this last equation,
1
ln |x| = —
3
ln(1 + 3u2) + ln(C1).

Inverting the logarithms,

|x|(1 + 3y2/x2)1/3 = C1, or |x|(x2 + 3y2) = C.

4. Because M (x, y) = y(y — x) and N (x, y) = x(x + y), we have
that M (tx, ty) =—ty(ty tx) = t2 M (x, y), and N (tx, ty) = tx(tx + ty) =
t2N (x, y). Therefore, the differential equation is homogeneous.

, 6 Advanced Engineering Mathematics with MATLAB

Let y = ux. Substituting into the differential equation,

x2u(u — 1) dx + x2(u + 1)(u dx + xdu) = 0
or
dx u+1
2u2 dx + (u + 1)xdu = 0, or 2 =— du.
x u2
Integrating this last equation,

1 x
ln |x|2 = — ln |u| + + C, or ln |ux2 | = C — , or ln
u2 y y
x
|xy| = C — .


5. Because M (x, y) = y + 2 xy and N (x, y) = —x, we have that M (tx,

ty) = ty 2+ 2 t xy = ty √ + 2t xy = tM (x, y), and N (tx, ty) = tx =

tN (x, y). Therefore, the differential equation is homogeneous.
Let y = ux. Substituting into the differential equation,
√ du dx
x(u dx + xdu) = (xu + u ) dx, √ = .
2x o 2 u x
r

Integrating this last equation,

u1/2 = ln |x| + C, or y = x (ln |x| + C) 2 .

6. Because M (x, y) = x 2 + y 2 — y and N (x, y) = x, we have that M (tx, ty)
√ √
= t2x2 + t2y2 — ty = t x2 + y2 — y = tM (x, y), and N (tx, ty) = tx =
tN (x, y). Therefore, the differential equation is
homogeneous. Let y = ux. Substituting into the
differential equation,

x2 + x2u2 — ux dx + x(xdu + u dx) = 0,

or
dx du
x√ 1 + u2 dx + x2 du = 0, or = —√ .
x 1 + u2
Integrating this last equation,

— ln(x) = — ln u + 1 + u2 — ln(C).

Inverting the logarithms,
√ √
ux + u2x2 + x2 = C, or y + x2 + y2 = C.

7. Because M (x, y) = sec(y/x) + y/x and N (x, y) —= 1, we have that
M (tx, ty) = sec[(ty)/(tx)] + (ty)/(tx) = sec(y/x) + y/x = M (x, y), and




@LECTJULIESOLUTIONSSTUVIA

,Worked Solutions 7

N (tx, ty) =— 1 = N (x, y). Therefore, the differential equation is
homoge- neous.
Let y = ux. Substituting into the differential equation,

dx
u dx + xdu = [sec(u) + u] dx, or cos(u) du = .
x
Integrating and substituting for u, the final answer is

sin(y/x) — ln |x| = C.

8. Because M (x, y) = ey/x + y/x and N (x, y)—= 1, we have that M (tx,
ty) = e(ty)/(tx) + (ty)/(tx) = ey/x + y/x = M (x, y), and N (tx,
— ty) = 1 =
N (x, y). Therefore, the differential equation is homogeneous.
Let y = ux. Substituting into the differential equation,
dx
u dx + xdu = (eu + u) dx, or e−u du = .
x
Integrating and substituting for u, the final answer is

y(x) = —x ln (C — ln |x|) .


Section 1.4

1. Since M (x, y) = y2 — x2, and N (x, y) = 2xy,
∂M ∂N
= 2y = .
∂y ∂x

The exactness criteria is satisfied.
Now, since
∂u
= y2— x2,
∂x
then u(x, y) = xy 2 —3 1 x3 + f (y). To find f (y), we use
∂u
= 2xy + f ′(y) = 2xy.
∂y

Therefore, f ′(y) = 0, and u(x, y) = xy2 3— 1 x3 = C.

2. Since M (x, y) = y — x, and N (x, y) = x + y,
∂M ∂N
=1= .
∂y ∂x

, 8 Advanced Engineering Mathematics with MATLAB

The exactness criteria is satisfied.
Now, since
∂u
= y — x,
∂x
then u(x, y) = xy — 12x2 + f (y). To find f (y), we use
∂u
= x + f ′(y) = x + y.
∂y
Therefore, f ′(y) = y, and u(x, y) = xy2 + 1 y22 — 1 x2 = C.
3. Since M (x, y) = y2 — 1, and N (x, y) = 2xy — sin(y),
∂M ∂N
= 2y = .
∂y ∂x
The exactness criteria is
satisfied.
Now, since
∂u
= y2 — 1,
∂x
then u(x, y) = xy2 — x + f (y). To find f (y), we use
∂u
= 2xy + f ′(y) = 2xy— sin(y).
∂y
Therefore, f ′(y) = — sin(y), and u(x, y) = xy2 — x + cos(y) = C.
4. Since M (x, y) = sin(y) — 2xy + x2, and N (x, y) = x cos(y) — x2,
∂M ∂N
= cos(y) — 2x = .
∂y ∂x
The exactness criteria is satisfied.
Now, since
∂u
= sin(y)— 2xy + x2,
∂x
then u(x, y) = x sin(y) — x 2y 3+ 1 x 3 + f (y). To find f (y), we use
∂u
= x cos(y)
— x + f (y) = x cos(y)
2 ′
—x .
2
∂y
Therefore, f ′(y) = 0, and u(x, y) = x sin(y) — x 2y + 1 x3 = C.
3

5. Since M (x, y) = —y/x2, and N (x, y) = 1/x + 1/y,
∂M 1 ∂N
=— 2 = .
∂y x ∂x




@LECTJULIESOLUTIONSSTUVIA

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Structural Dynamics Concepts and Applications

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