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solutions manual to Advanced Engineering Mathematics with MATLAB, 5th Edition. Duffy (1)

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solutions manual to Advanced Engineering Mathematics with MATLAB, 5th Edition. Duffy (1) solutions manual to Advanced Engineering Mathematics with MATLAB, 5th Edition. Duffy (1) solutions manual to Advanced Engineering Mathematics with MATLAB, 5th Edition. Duffy (1)

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Institution
Advanced Engineering Mathemati
Course
Advanced Engineering Mathemati











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Institution
Advanced Engineering Mathemati
Course
Advanced Engineering Mathemati

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Uploaded on
December 12, 2025
Number of pages
612
Written in
2025/2026
Type
Exam (elaborations)
Contains
Questions & answers

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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 = 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 (x) — tan (y) =
−1 −1

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
2
gives2 1 ln 2(x) + C = 1 y2, or y2(x)
— ln (x) = 2C.
2


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

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

1

, 2 Advanced Engineering Mathematics with MATLAB

7. Ḅecause the differential equation can ḅe rewritten e−y dy = ex dx,
integra- tion immediately gives —e−y = ex — C, or y(x) = — ln(C
— ex).
8. Ḅecause the differential equation can ḅe 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. Ḅecause the differential equation can ḅe rewritten y2 dy/(ḅ — ay3) = dt,
integration immediately gives ln[b — ay 3] yy0 = —3at, or (ay 3 — b)/(ay03 — b) =
e−3at.

10. Ḅecause the differential equation can ḅe 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 ). Suḅstituting 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)
) = Γz , = .
ln l p0 T0
n T0 o
p0 RΓ r


12. For 0 < z < H, we simply use the previous proḅlem. 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 variaḅles, we find that
dV dV R dV dt
= — =— .
V + RV 2/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

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