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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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Institution
Engineer
Course
Engineer

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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 =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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