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

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

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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
October 6, 2025
Number of pages
596
Written in
2025/2026
Type
Exam (elaborations)
Contains
Questions & answers

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t AllChaptersCovered
t t




SOLUTIONS

,TableofContents t t




Chapter 1: First-Order Ordinary Differential Equations 1
t t t t t t




t Chapter 2: Higher-Order Ordinary Differential Equations
t t t t t




t Chapter 3: Linear Algebra
t t t




Chapter 4: Vector Calculus
t t t




t Chapter 5: Fourier Series Chapter
t t t t




6: The Fourier Transform
t t t t




Chapter7:TheLaplaceTransform
t t t t




t Chapter 8: The Wave Equation
t t t t




t Chapter 9: The Heat Equation
t t t t




t Chapter 10: Laplace’s Equation
t t t




Chapter11:TheSturm-LiouvilleProblem
t t t t




t Chapter 12: Special Functions
t t t




Appendix A: Derivation of the Laplacian in Polar Coordinates AppendixB:
t t t t t t t t t t




DerivationoftheLaplacian in SphericalPolarCoordinates
t t t t t t t t

, Solution Manual t




Section 1.1 t




1. first-order, linear
t t 2. first-order, nonlinear
t t




3. first-order, nonlinear
t t 4. third-order, linear
t t




5. second-order, linear
t t 6. first-order, nonlinear
t t




7. third-order, nonlinear
t t 8. second-order, linear
t t




9. second-order, nonlinear
t t 10. first-order, nonlinear t t




11. first-order, nonlinear
t t 12. second-order, nonlinear t t




13. first-order, nonlinear
t t 14. third-order, linear t t




15. second-order, nonlinear
t t 16. third-order, nonlinear t t




Section 1.2 t




1. Because the differential equation can be rewritten e−ydy = xdx, integra-
t t t t t t t t t t t




tion immediately gives —e−y = 12x2 —C, or y = —ln(C —x2/2).
t t t t t t t t t t t t t t t t




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




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

1
t t = C.
t t t t t t t t t t t




3. Because the differential equation can be rewritten ln(x)dx/x = y dy, inte-
t t t t t t t t t t t




gration immediately gives2 1 ln2(x) + C = 1y2 2, or y2(x) —ln2(x) = 2C.
t t t t t t t t t t t t t t t t




4. Because the differential equation can be rewritten y2dy = (x + x3)dx,
t t t t t t t t t t t t t




integration immediately gives y3(x)/3 = x2/2 + x4/4 + C.
t t t t t t t t t t




5. Because the differential equation can be rewritten y dy/(2+y2) = xdx/(1+
t t t t t t t t t t



x2), integration immediately gives 1ln(2 +y2) = 1ln(1+x2)+ 1 ln(C), or
t t t t t t t t t t t t t t t t


2 2 2
2 + y2(x) = C(1 + x2).
t t t t t t




6. Because the differential equation can be rewritten dy/y1/3 = x1/3
t t t t t t t t t




3 2/3 3 4/3 3
t

1 4/3 3/2 t


dx, integration immediately gives
t t
2 y t t t t
4 t = x t t
2+ t t C, or y(x) =
t t t t
2x +C t
. t t




1

, 2 Advanced Engineering Mathematics with MATLAB t t t t




7. Becausethe differential equation can be rewritten e−ydy =exdx, integra- tion
t t t t t t t t t t t t t




immediately gives —e−y = ex —C, or y(x) = —ln(C —ex).
t t t t t t t t t t t t t t




8. Because the differential equation can be rewritten dy/(y2 +1) = (x3 + 5) t t t t t t t t t t t t t




dx, integration immediately gives tan−1(y) = 1x4 + 5x + C, or y(x) =
t t t t t t t t t t t t t t t

t 4 t


tan 41x4 +5x +C . t
t t t t




9. Because the differential equation can be rewritten y2 dy/(b —ay3) = dt, t t t t
t
t t t t t t t


y
integration immediately gives ln[b —ay 3] y0 = —3at, or (ay 3 —b)/(ay30 —b) =
t t t t t t tt

t
t t t
t t t t




e−3at. t




10. Because the differential equation can be written du/u = dx/x2, integra- t t t t t t t t t t




tion immediately gives u = Ce−1/x or y(x) = x + Ce−1/x.
t t t t t t t t t t t t




— g dz/(RT).
11. From the hydrostatic equation and ideal gas law, dp/p = t t t t t t t t t t t




Substituting for T (z),
t t t t


dp g
=— dz. t t


p R(T 0 —Γz) t
t




Integrating from 0 to z, t t t t




p(z) g T0 —Γz p(z) T0 —Γz g/(RΓ)
t t t t t t
t t
t t t


ln = ln =
t t


, or .
p0 RΓ T0 t p0 T0


12. For 0 < z < H, we simply use the previous problem. At z = H,
t t t t t t t t t t t t t t t




tthe pressure ist t




T0 —ΓH g/(RΓ) t

t
t t
t




p(H) = p0 . t t


T0
Then we follow the example in the text for an isothermal atmosphere for
t t t t t t t t t t t t




z ≥H.
t t




13. Separating variables, we find that t t t t




dV dV R dV dt
— =—
t



= t t t t .
V t + RV 2/S t t t V t t S(1+ RV/S) t t t RC t




Integration yields t




t t t


V t
=—
t t t


ln t t + ln(C). t


1+ RV/S t t RC

Upon applying the initial conditions,
t t t t




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

V (t) = t t t
t t
t t


1+ RV0/S t t 1+ RV0/S t t
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