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Solutions Manual for Advanced Engineering Mathematics with MATLAB (5th Edition) by Dean G. Duffy

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This comprehensive solutions manual provides step-by-step solutions to all exercises in Advanced Engineering Mathematics with MATLAB, 5th Edition by Dean G. Duffy. It covers a wide range of applied mathematics topics including differential equations, linear algebra, vector calculus, complex analysis, transforms, numerical methods, partial differential equations, and boundary value problems — all reinforced with MATLAB-based problem solving and visualization. Ideal for undergraduate and graduate engineering students, this manual helps bridge the gap between theory and application, offering clear computational examples, algorithmic techniques, and MATLAB scripts to support learning and project work. advanced engineering mathematics solutions, duffy matlab solution manual, differential equations solved, laplace transform exercises, numerical methods with matlab, linear algebra engineering problems, vector calculus answers, complex analysis with matlab, pde solution manual, matlab scripts engineering math, duffy 5th edition answers, boundary value problems solutions, applied math for engineers, engineering mathematics textbook answers, matlab examples for engineering math, duffy advanced math solutions

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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

, 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 = x dx, integra- tion
immediately gives −e −y = 1 x2 − C, or2 y = − ln(C − x2 /2).

2. Separating variables, we have that dx/(1 + x2 ) = dy/(1 + y 2 ). 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
immediately gives 1 ln2(x) + C 2= 1 y2 , or y2(x) − 2ln2(x) = 2C.

4. Because the differential equation can be rewritten y2 dy = (x + x3) dx,
integration immediately gives y3(x)/3 = x2 /2 + x4 /4 + C.

5. Because the differential equation can be rewritten y dy/(2+y2 ) = x dx/(1+ x2),
integration immediately gives 1 ln(2 + y22 ) = 1 ln(1 + x2) 2+ 1 ln(C), or 2
2 + y2(x) = C(1 + x2).

6. Because the differential equation can be rewritten dy/y1/3 = x1/3 dx, integration
3/2
immediately gives 3 y2/3 = 3 x4/3 + 3 C,2 or y(x) =4 1 4/3
x +C
2
. 2

1




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,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
4
+ C, or y(x) =
tan 14x4 + 5x + C .

9. Because the differential equation can be rewritten y2 dy/(b − ay3 ) = dt,
y
integration immediately gives ln[b − ay3 ] = −3at, or (ay3 − b)/(ay3 − b) = 0
y0
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.
= − R(T0 − Γz)
p
Integrating from 0 to z,
g/(RΓ)
p(z) p(z) T0 − Γz
ln = g ln T0 − Γz , or = .
p0 RΓ T0 p0 T0


12. For 0 < z < H, we simply use the previous problem. At z = H, the
pressure is
g/(RΓ)
p(H) = p 0 T0 − ΓH .
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
= − =− .
V + RV 2/S V S(1 + RV/S) RC

Integration yields
t
ln V = − + ln(C).
1 + RV/S RC

Upon applying the initial conditions,

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




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,Worked Solutions 3

Solving for V (t), we obtain

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


14. From the definition of γ, we can write the differential equation
A dT
+ T4 = γ4 ,
B dt
or
B dT T 4 1 dT
dT T 2
= − 2 2
dt = − − γ4 + γ2
2γ2 T −γ
A dT
1 2γ dT T 2 dT
= 3 — + .
4γ + γ 2 T −γ T +γ
The final answer follows from direction integration.

15. Separating the variables yields
dN d[ln(K/N )]
= bdt, 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)]}= −bt ln(K/N) =

or
ln[K/N(0)]e−bt ln[N/N(0)] = ln[K/N(0)]

or 1 − e−bt

or
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 1 + βI(z)/α = −αz,
I(0)




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,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 [A]0
([A]0 − [B]0) ([A]0 − [C]0) ln
− [X]
1 [B]0
+ ln
([B]0 − [A]0) ([B]0 − [C]0) [B]0 − [X]
1 [C]0 [C]0
+ ln = kt.
([C]0 − [A]0) ([C]0 − [B]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 −(k 1+k 2)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.




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,Worked Solutions 5

Let y = ux. Substituting into the differential equation, (ux + x)(u dx +
x du) = ux dx, or −u2x dx = (1 + u)x2 du, or
dx 1 1
+ du.
— = u u2
x
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)x dx +(u + 1)x(u dx + x du)
= 0, or
dx u+1
(u2 + 2u − 1) dx = −(u + 1)x du, or − = du.
x u2 + 2u − 1
Integrating this last equation,
2 y
− ln |x| = 1 ln |u2+2u−1|+C, or x2 +y2 − 1 = y2 +2xy−x2 = C.
2
x2 x

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

+ x du) + (x2 + x2 u 2) dx = 0
or
dx 2u
2xu du + (1 + 3u2) dx = 0, or =− du.
x 1 + 3u2
Integrating this last equation,

ln |x| = −31 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) = t2 N (x, y). Therefore, the differential
equation is homogeneous.




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,6 Advanced Engineering Mathematics with MATLAB

Let y = ux. Substituting into the differential equation,

x2u(u − 1) dx + x2(u + 1)(u dx + x du) = 0

or
dx u+1
2u2 dx + (u + 1)x du = 0, or 2 =− du.
x u2
Integrating this last equation,
1 x x
ln |x|2 = − ln |u| + + C, or ln |ux2| = C − , or ln |xy| = C − .
u2 y y

5. Because M(x, y) = y + 2 xy and N(x, y) = −x, we have that M(tx, ty) =
p √
ty + 2 t2 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 + x du) = (xu + 2x u ) dx, or √ = .
2 u x

Integrating this last equation,

u1/2 = ln |x| + C, or y = x (ln |x| + C)2 .
p
6. Because M(x, y) = x2 + y 2 − y and N(x, y) = x, we have that M (tx, ty)
p p
= t2 x2 + t2 y2 − 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,
p
x2 + x2 u2 − ux dx + x(x du + u dx) = 0,
or p dx du
x 1 + u2 dx + x2 du = 0, or = −√ .
x 1 + u2
Integrating this last equation,
p
− ln(x) = − ln u + 1 + u2 − ln(C).

Inverting the logarithms,
p p
ux + u2 x2 + 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




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,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 + x du = [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) = e y/x + y/x and N (x, y) = −1, we have that M (tx, ty) = e (ty)/(tx) +
(ty)/(tx) = e y/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 + x du = (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) = xy2 − 1 x3 + 3f (y). To find f(y), we use

∂u
= 2xy + f′(y) = 2xy.
∂y

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

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




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