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Examen

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

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Escrito en
2025/2026

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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Institución
Advanced Engineering Mathemati
Grado
Advanced Engineering Mathemati











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Institución
Advanced Engineering Mathemati
Grado
Advanced Engineering Mathemati

Información del documento

Subido en
6 de octubre de 2025
Número de páginas
596
Escrito en
2025/2026
Tipo
Examen
Contiene
Preguntas y respuestas

Temas

Vista previa del contenido

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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