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solutions manual to Advanced Engineering Mathematics with MATLAB, 5th Edition. Duffy

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Enhance your understanding of applied mathematics with this comprehensive solutions manual for Advanced Engineering Mathematics with MATLAB, 5th Edition by Dean G. Duffy. This manual offers complete, step-by-step solutions to all textbook exercises, integrating analytical problem-solving with MATLAB programming for real-world engineering applications. It covers essential topics such as differential equations, linear algebra, complex analysis, vector calculus, Fourier and Laplace transforms, numerical methods, and partial differential equations. Each solution is clearly explained and supported with MATLAB code to reinforce computational techniques and mathematical concepts. Perfect for engineering, physics, and applied mathematics students, this guide is an essential resource for assignments, projects, and exam preparation.

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Advanced Engineering Mathematics
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Advanced Engineering Mathematics











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Institution
Advanced Engineering Mathematics
Course
Advanced Engineering Mathematics

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Uploaded on
October 7, 2025
Number of pages
600
Written in
2025/2026
Type
Exam (elaborations)
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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 = xdx, integra-
tion immediately gives —e−y =2 1 x2 — C, or y = — ln(C — x2/2).

2. Separating variables, we have that dx/(1 + x2) = dy/(1 + y2). Integrating
— tan− (y) = tan(C), or (x
this equation, we find that tan−1(x) — y)/(1+xy) =
1

C.

3. Because the differential equation can be rewritten ln(x)dx/x = y dy, inte-
gration immediately gives2 1 ln2(x) + C = 21 y2, or y2(x) — ln2(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) = 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,
3 2/3 1 4/3 3/2
integration immediately gives
2
y =4 3 x4/3 +2 3 C, or y(x) = 2
x +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 x4 + 5x + C .

9. Because the differential equation can be rewritten y2 dy/(b — ay3) = dt,
y
integration immediately gives ln[b — ay 3] y0 = —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(T 0 — Γz)
Integrating from 0 to z,

p(z) g T0 — Γz p(z) T0 — Γz g/(RΓ)
ln = ln , or = .
p0 RΓ T0 p0 T0


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/S
= — =— .
V + RV 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

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