SAMPLE FINAL EXAM SOLUTIONS

Similar documents
Math 5587 Midterm II Solutions

Analysis III Solutions - Serie 12

MATH 131P: PRACTICE FINAL SOLUTIONS DECEMBER 12, 2012

Math 201 Assignment #11

# Points Score Total 100

Partial Differential Equations for Engineering Math 312, Fall 2012

Solutions to the Sample Problems for the Final Exam UCLA Math 135, Winter 2015, Professor David Levermore

Separation of Variables

MA Chapter 10 practice

FINAL EXAM, MATH 353 SUMMER I 2015

THE METHOD OF SEPARATION OF VARIABLES

The Fourier series for a 2π-periodic function

Method of Separation of Variables

LAPLACE EQUATION. = 2 is call the Laplacian or del-square operator. In two dimensions, the expression of in rectangular and polar coordinates are

UNIVERSITY OF MANITOBA

M412 Assignment 5 Solutions

Math 2930 Worksheet Final Exam Review

Math Assignment 14

Lecture 24. Scott Pauls 5/21/07

Math 251 December 14, 2005 Final Exam. 1 18pt 2 16pt 3 12pt 4 14pt 5 12pt 6 14pt 7 14pt 8 16pt 9 20pt 10 14pt Total 150pt

Math 316/202: Solutions to Assignment 7

MATH-UA 263 Partial Differential Equations Recitation Summary

Math 4263 Homework Set 1

Math 220a - Fall 2002 Homework 6 Solutions

Wave Equation With Homogeneous Boundary Conditions

McGill University April 20, Advanced Calculus for Engineers

Review For the Final: Problem 1 Find the general solutions of the following DEs. a) x 2 y xy y 2 = 0 solution: = 0 : homogeneous equation.

The end conditions on the beam are modelled by assuming the following boundary conditions on the function u: u(0, t) = u x (0, t) = 0;

Ma 221 Final Exam Solutions 5/14/13

Strauss PDEs 2e: Section Exercise 4 Page 1 of 6

Laplace s equation in polar coordinates. Boundary value problem for disk: u = u rr + u r r. r 2

BOUNDARY PROBLEMS IN HIGHER DIMENSIONS. kt = X X = λ, and the series solutions have the form (for λ n 0):

FOURIER SERIES PART III: APPLICATIONS

Diffusion on the half-line. The Dirichlet problem

Math 251 December 14, 2005 Answer Key to Final Exam. 1 18pt 2 16pt 3 12pt 4 14pt 5 12pt 6 14pt 7 14pt 8 16pt 9 20pt 10 14pt Total 150pt

MATH 251 Final Examination August 14, 2015 FORM A. Name: Student Number: Section:

c2 2 x2. (1) t = c2 2 u, (2) 2 = 2 x x 2, (3)

21 Laplace s Equation and Harmonic Functions

Special Instructions:

1 Wave Equation on Finite Interval

Fourier and Partial Differential Equations

Math 5440 Problem Set 7 Solutions

Final: Solutions Math 118A, Fall 2013

Boundary-value Problems in Rectangular Coordinates

Chapter 10: Partial Differential Equations

MATH 251 Final Examination December 19, 2012 FORM A. Name: Student Number: Section:

Partial differential equation for temperature u(x, t) in a heat conducting insulated rod along the x-axis is given by the Heat equation:

Homework 7 Math 309 Spring 2016

Math 113 Winter 2005 Key

Suggested Solution to Assignment 6

Problem (p.613) Determine all solutions, if any, to the boundary value problem. y + 9y = 0; 0 < x < π, y(0) = 0, y (π) = 6,

SC/MATH Partial Differential Equations Fall Assignment 3 Solutions

Introduction to Sturm-Liouville Theory and the Theory of Generalized Fourier Series

MATH 124B: INTRODUCTION TO PDES AND FOURIER SERIES

Vibrating-string problem

Autumn 2015 Practice Final. Time Limit: 1 hour, 50 minutes

My signature below certifies that I have complied with the University of Pennsylvania s Code of Academic Integrity in completing this exam.

6 Non-homogeneous Heat Problems

MATH 251 Final Examination December 16, 2015 FORM A. Name: Student Number: Section:

Separation of variables in two dimensions. Overview of method: Consider linear, homogeneous equation for u(v 1, v 2 )

Spotlight on Laplace s Equation

Mathematics Qualifying Exam Study Material

Math 54: Mock Final. December 11, y y 2y = cos(x) sin(2x). The auxiliary equation for the corresponding homogeneous problem is

d Wave Equation. Rectangular membrane.

Review Sol. of More Long Answer Questions

Separation of Variables. A. Three Famous PDE s

17 Source Problems for Heat and Wave IB- VPs

MB4018 Differential equations

2.4 Eigenvalue problems

DUHAMEL S PRINCIPLE FOR THE WAVE EQUATION HEAT EQUATION WITH EXPONENTIAL GROWTH or DECAY COOLING OF A SPHERE DIFFUSION IN A DISK SUMMARY of PDEs

Partial Differential Equations

Boundary value problems for partial differential equations

Differential equations, comprehensive exam topics and sample questions

UNIVERSITY of LIMERICK OLLSCOIL LUIMNIGH

A proof for the full Fourier series on [ π, π] is given here.

UNIVERSITY of LIMERICK OLLSCOIL LUIMNIGH

TMA4120, Matematikk 4K, Fall Date Section Topic HW Textbook problems Suppl. Answers. Sept 12 Aug 31/

Separation of variables

In this chapter we study elliptical PDEs. That is, PDEs of the form. 2 u = lots,

BOUNDARY-VALUE PROBLEMS IN RECTANGULAR COORDINATES

MATH 251 Final Examination May 4, 2015 FORM A. Name: Student Number: Section:

Bessel s Equation. MATH 365 Ordinary Differential Equations. J. Robert Buchanan. Fall Department of Mathematics

Staple or bind all pages together. DO NOT dog ear pages as a method to bind.

MA 201: Differentiation and Integration of Fourier Series Applications of Fourier Series Lecture - 10

ENGI 9420 Lecture Notes 8 - PDEs Page 8.01

Final Exam May 4, 2016

DIFFERENTIAL EQUATIONS

MA 201: Method of Separation of Variables Finite Vibrating String Problem Lecture - 11 MA201(2016): PDE

Part A 5 Shorter Problems, 8 points each.

MATH 251 Final Examination May 3, 2017 FORM A. Name: Student Number: Section:

Name: ID.NO: Fall 97. PLEASE, BE NEAT AND SHOW ALL YOUR WORK; CIRCLE YOUR ANSWER. NO NOTES, BOOKS, CALCULATORS, TAPE PLAYERS, or COMPUTERS.

Sturm-Liouville Theory

1 Partial derivatives and Chain rule

Midterm 2: Sample solutions Math 118A, Fall 2013

3 Green s functions in 2 and 3D

Math 311, Partial Differential Equations, Winter 2015, Midterm

MATH 3150: PDE FOR ENGINEERS FINAL EXAM (VERSION D) 1. Consider the heat equation in a wire whose diffusivity varies over time: u k(t) 2 x 2

Partial Differential Equations

MATH 412 Fourier Series and PDE- Spring 2010 SOLUTIONS to HOMEWORK 6

LECTURE 19: SEPARATION OF VARIABLES, HEAT CONDUCTION IN A ROD

Transcription:

LAST (family) NAME: FIRST (given) NAME: ID # : MATHEMATICS 3FF3 McMaster University Final Examination Day Class Duration of Examination: 3 hours Dr. J.-P. Gabardo THIS EXAMINATION PAPER INCLUDES 22 PAGES AND 9 QUESTIONS. YOU ARE RESPONSIBLE FOR ENSURING THAT YOUR COPY OF THE PAPER IS COMPLETE. BRING ANY DISCREPANCY TO THE ATTENTION OF YOUR INVIGILATOR. Instructions: The total of marks is 1. No calculator or other aid are allowed. Pages 18 21 are for scratch or overflow work. Please indicate clearly that you are continuing your work on one of these pages if you decide to do so. There is a formula sheet on the last page. SAMPLE FINAL EXAM SOLUTIONS Continued... Page 1 of 22

Provide all details and fully justify your answer in order to receive credit. 1. (1 pts.) Use the method of characteristics the solve the first-order partial differential equation (for u = u(x, y)): u x ex 1 + e u y y =, < x <, y >, with initial condition u(x, ) = e 2x. Solution. The equation for the characteristics curves is which is a separable ODE. We have (1 + e y ) dy dx = ex dy dx = ex 1 + e y and thus (1 + e y ) dy = e x dx which yield y + e y = e x + C. The characteristics curves are thus the curves with equation e y + y + e x = C, C arbitary constant. The general solution of the PDE is this u(x, y) = F (e y + y + e x ), where F (s) is an arbitrary function of 1 variable. Using the initial condition we have u(x, ) = e 2x = F (e + + e x ) = F (1 + e x ) Letting s = 1 + e x, we have e 2x = (e x ) 2 = (s 1) 2 and thus F (s) = (s 1) 2. The solution is therefore u(x, y) = (e y + y + e x 1) 2. Continued... Page 2 of 22

2. (8 pts.) Consider the solution u(x, t) of the diffusion equation u t = u xx, < x < l, t >, u x (, t) = u x (l, t) =, t >, u(x, ) = φ(x), < x < l. Show that the function F (t) = l e u(x,t) dx is decreasing for t. Solution. We compute F (t) = d l dt = l } l e u(x,t) dx = u xx (x, t) e u(x,t) dx = [ u x (x, t) e u(x,t)] l l = u x (l, t) }} = d dt e u(x,t) } dx = l (using the PDE) e u(l,t) u x (, t) e u(,t) }} = u t (x, t) e u(x,t) dx u x (x, t) d } e u(x,t) dx (using integration by parts) dx l (u x (x, t)) 2 e u(x,t) dx }} Since F (t) for all t >, it follows that F (t)is decreasing for t. Continued... Page 3 of 22

3. Consider the eigenvalue problem X (x) + λ X(x) =, < x < 1, X() =, X(1) = X (1). (a) (4 pts.) Show that the boundary conditions for the problem above are symmetric.(you should assume that all functions involved are complex-valued.) What can you conclude about the eigenvalues and eigenfunctions of the problem above? Solution. If f(x) and g(x) both satisfy the boundary conditions, we have [ ] 1 f (x) g(x) f(x) g (x) = f(1)g(1) + f(1) g(1) =. It follows that all the eigenvalues are real = f (1)g(1) f(1) g (1) f () g() }} = f() g }} () = and that eigenfunctions associated with different eigenvalues are orthogonal to each other. (b) (4 pts.) State a simple condition that can be used to check that there are no negative eigenvalues and use it to show that this is the case for the problem above. Check directly that they are indeed no negative eigenvalues. Solution. If the boundary conditions are symmetric and we have [f(x) f (x)] 1 for any (real-valued) function f(x) satisfying the boundary conditions, then all then eigenvalues are non-negative. For the boundary conditions in part (a), we have [f(x) f (x)] 1 = f(1) f (1) f() f () = f(1) 2 }} = and thus that condition holds. By direct computation, letting λ = β 2 where β >, if X (x) β 2 X(x) =, then X(x) = C 1 sinh(βx) + C 2 cosh(βx). If X() =, then C 2 = and the condition X(1) = X (1) implies that C 1 sinh(β) = C 1 β cosh(β). If C 1, we would need tanh(β) = β which has no solution as tanh(β) > and β < for β >. Continued... Page 4 of 22

(c) (2 pts.) Is zero an eigenvalue? If so find the corresponding eigenfunction. Solution. If X(x) is a corresponding eigenfunction, then X (x) =, so X(x) = C 1 x + C 2. The condition X() = implies C 2 = and the condition X(1) = X (1) implies C 1 = C 1 or C 1 =. Thus there is non non-trivial solution and is not an eigenvalue. (d) (4 pts.) Use the graphical method to show that there are infinitely many eigenvalues λ n > and find the corresponding eigenfunctions. Solution. If λ = β 2 where β > and X (x) + β 2 X(x) =, then X(x) = C 1 sin(βx) + C 2 cos(βx). If X() =, then C 2 = and the condition X(1) = X (1) implies that C 1 sin(β) = C 1 β cos(β). If C 1, we need tan(β) = β We can see from the graph above that the previous equation has infinitely many solutions β n for n 1, where (n 1/2)π < β n < n π and thus infinitely many corresponding positive eigenvalues λ = β 2 n. and eigenfunctions X n (x) = sin(β n x). Continued... Page 5 of 22

4. Let D = (x, y), x 2 + y 2 < 1} be the unit disk centered at the origin in the x, y plane and let C = (x, y), x 2 + y 2 = 1} be the unit circle bounding D. Find the solution u(x, y) of Laplace equation u xx + u yy =, (x, y) D, which satisfies the boundary condition u(x, y) = 4 x 3, (x, y) C. (a) (8 pts.) Solve this problem by passing to polar coordinates. Note that the Laplace operator is written as 2 r + 1 2 r r + 1 2 r 2 θ 2 in polar coordinates. (Hint. cos 3 θ = 1 4 cos(3θ) + 3 4 cos(θ).) Solution. We look first for non-trivial solutions of the PDE in polar coordinates of the form u(r, θ) = R(r) Θ(θ) where Θ(θ) is 2π-periodic. We have R (r) Θ(θ) + 1 r R (r) Θ(θ) + 1 r 2 R(r) Θ (θ) = or r 2 R (r) + r R (r) R(r) = Θ (θ) Θ(θ) = λ. This leads to the eigenvalue problem for Θ(θ): Θ (θ) + λ Θ(θ) =, Θ( π) = Θ(π), Θ ( π) = Θ (π), The eigenvalues are λ n = n 2, n, with corresponding eigenfunctions Θ (θ) = 1 and,for n 1, Θ n (θ) = A n cos(nθ) + B n sin(nθ). For each n, we need to solve the DE r 2 R (r) + r R (r) n 2 R(r) = which is of Cauchy-Euler type. Letting R(r) = r β we have β (β 1) + β n 2 = or β 2 = n 2. If n =, the solution is R (r) = C + D ln r and and we need D = to ensure the continuity of the solution at r =. Thus R (r) = C. If n 1, the solution is of the form R n (r) = C n r n + D n r n. Again, to ensure the continuity of the solution at r =, we need to take D n =. We obtain thus particular solutions of the form C and (A n cos(nθ) + B n sin(nθ)) r n for n 1. By the superposition principle, the general solution has the form u(r, θ) = A 2 + (A n cos(nθ) + B n sin(nθ)) r n where A 2 = C for convenience. Continued... Page 6 of 22

If x 2 + y 2 = 1, we have x = cos θ, y = sin θ, and 4 x 3 = 4 cos 3 θ = cos(3θ) + 3 cos(θ). To satisfy the boundary condition, we thus need u(1, θ) = A 2 + (A n cos(nθ) + B n sin(nθ)) = cos(3θ) + 3 cos(θ). By inspection, we see immediately that A 1 = 3, A 3 = 1 and A n = B n = otherwise. The solution is thus u(r, θ) = cos(3θ) r 3 + 3 cos(θ) r. (b) (4 pts.) Express the solution found in part (a) in rectangular coordinates and verify that it is a solution of the Laplace equation satisfying the given boundary condition. Solution. Letting x + i y = r(cos θ + i sin θ) = r e i θ, we have r cos θ = x = Re(x + iy) and r 3 cos(3θ) = Re(r 3 e 3 i θ ) = Re((r e i θ ) 3 ) = Re((x + i y) 3 ) = Re(x 3 + 3 i x 2 y 3 x y 2 i y 3 ) = x 3 3 x y 2 In cartesian coordinates, the solution is thus given by u(x, y) = x 3 3 x y 2 + 3 x. We check that this is indeed the correct solution: u xx + u yy = 6 x 6 x = and if x 2 + y 2 = 1, we have x 3 3 x y 2 + 3 x = x 3 3 x (1 x 2 ) + 3 x = 4 x 3. Continued... Page 7 of 22

5. Consider the wave equation u tt = 4 u xx, < x < π, t >, (1) together with the boundary conditions u(, t) = u(π, t) =, t >, (2) and the initial conditions u(x, ) =, u t (x, ) = 1, < x < π. (3) (a) (4 pts.) Using the method of separation of variables, find all non-trivial solutions of the equations (1) and (2) of the form u(x, t) = X(x) T (t). Solution. Letting u(x, t) = X(x) T (t), we have using (1) X(x) T (t) = 4 X (x) T (t) or T (t) 4 T (t) = X (x) X(x) = λ. and, using (2), X() T (t) = X(π) T (t) = which implies X() = X(π) =. We obtain thus the eigenvalue problem for X(x): X (x) + λ X(x) =, X() = X(π) = The eigenvalues are λ n = n 2 for n 1 with corresponding eigenfunctions X n (x) = sin(nx). For each n, the solution of the ODE is The non-trivial solutions obtained are thus T (t) + 4 n 2 T (t) = T n (t) = A n cos(2nt) + B n sin(2nt). u n (x, t) = (A n cos(2nt) + B n sin(2nt)) sin(nx), n 1. Continued... Page 8 of 22

(b) (8 pts.) Use the superposition principle to find the general form of a solution of the PDE satisfying the given boundary conditions and compute the unique solution u(x, t) satisfying the given initial conditions (3). Solution. By the superposition principle, the general solution of (1) and (2) is of the form u(x, t) = (A n cos(2nt) + B n sin(2nt)) sin(nx), < x < π, t >. for appropriate constant A n and B n, n 1. The first condition in (3) yields u(x, ) = = A n sin(nx), < x < π, and thus that A n = for all n 1 (by uniqueness of the coefficients in a Fourier sine series). The first condition in (3) yields u t (x, ) = 1 = 2 n B n sin(nx), < x < π. It follows that 2 n B n = 2 π π sin(nx) dx = 2 π [ cos(nx) n ] π = 2 π 1 ( 1) n n and thus The solution is thus B n = 1 π 1 ( 1) n, n 1. n 2 u(x, t) = 1 π 1 ( 1) n n 2 sin(2nt) sin(nx), < x < π, t >, or u(x, t) = 2 π k= 1 sin(2(1 + 2k)t) sin((1 + 2k)x), < x < π, t >. (1 + 2k) 2 Continued... Page 9 of 22

6. (a) (5 pts.) Show that if u(x, t) is solution of the diffusion equation with variable dissipation u t k u xx + φ(t) u =, < x <, t >, u(x, ) = f(x), < x <, and g(t) is solution of the differential equation g (t) = φ(t) g(t), g() = 1, then v(x, t) = g(t) u(x, t) is solution of the diffusion equation v t k v xx =, < x <, t >, v(x, ) = f(x), < x <, Solution. We have and v t (x, t) = g (t) u(x, t) + g(t) u t (x, t) v xx (x, t) = g(t) u xx (x, t). Thus v t (x, t) k v xx (x, t) = g (t) u(x, t) + g(t) u t (x, t) k g(t) u xx (x, t) = φ(t) g(t) u(x, t) + g(t) u t (x, t) k g(t) u xx (x, t) = g(t) (φ(t) u(x, t) + u t (x, t) k u xx (x, t)) = and v(x, ) = g() u(x, ) = 1 f(x) = f(x). Continued... Page 1 of 22

(b) (5 pts.) Solve the diffusion equation with variable dissipation u t k u xx + cos(t) u =, < x <, t >, u(x, ) = e x, < x <, (Hint. See part (a).) Solution. Let v(x, t) be the solution of the diffusion equation v t k v xx =, < x <, t >, Then, v(x, t) = = = v(x, ) = e x, < x <, 1 4πkt 1 4πkt 1 4πkt = e kt x 1 4πkt e (x y)2 /4kt e y dy e (x2 2 (x 2 kt) y+y 2 )/4kt dy e (x 2 kt y)2 /4kt e ( 4ktx+4 k2 t 2 )/4kt dy e (x 2 kt y)2 /4kt After making the change of variable, ( x + 2 kt + y)/ 4kt = s with dy = 4kt ds, we obtain v(x, t) = e kt x 1 π } } =1 e s2 ds = e kt x. Using part (a), we first need to find g(t) the solution of g (t) cos(t) g(t) = with g() = 1. The integrating factor is exp( cos t dt) = e sin t. We have thus (g(t) e sin t ) = or g(t) e sin t = C, a constant. Since g() = 1, C = 1 and g(t) = e sin t. By part (a), the solution is u(x, t) = v(x, t) g(t) = e sin t e kt x = e sin t+k t x. Continued... Page 11 of 22

7. (a) (8 pts.) Use the method of separation of variables together with the superposition principle to find the solution u = u(x, y) of the boundary-value problem for the Laplace equation u xx + u yy =, < x < π, < y < 1, u x (, y) = u x (π, y) =, < y < 1, u(x, ) =, u(x, 1) = cos x, < x < π. Solution. We first look for solutions of the PDE that satisfy the boundary conditions and are of the form u(x, y) = X(x) Y (y). We have and X (x) Y (y) + X(x) Y (y) = or X (x) X(x) = Y (y) Y (y) = λ X () Y (y) = X (π) Y (y) = which yields X () = X (π) =. We obtain thus the eigenvalue problem for X(x): X (x) + λ X(x) =, X () = X (π) = The eigenvalues are λ n = n 2 for n with corresponding eigenfunctions X (x) = 1 and X n = cos(nx) for n 1. For each n, the DE for Y (y) is Y (y) n 2 Y (y) =. If n =, the solution is Y (y) = A + B y and for n 1, the solution is Y n (y) = A n cosh(ny) + B n sinh(ny). We obtain thus particular solutions of the form A + B y and (A n cosh(ny) + B n sinh(ny)) cos(nx) n 1. By the superposition principle, the general solution has the form u(x, y) = A + B y + (A n cosh(ny) + B n sinh(ny)) cos(nx), < x < π, < y < 1. The boundary condition u(x, ) = yields = A + and implies that A n = for all n. A n cos(nx), The boundary condition u(x, 1) = cos x then yields cos x = B + < x < π B n sinh(n) cos(nx), < x < π. Continued... Page 12 of 22

By inspection, B 1 sinh(1) = 1 or B 1 = 1/ sinh(1) and B n = otherwise. The solution is thus u(x, y) = sinh y sinh 1 cos(x). (b) (4 pts.) Find the maximum value of the solution u(x, y) in part (a) on the rectangle (x, y), x π, y 1}. How does this relate to the maximum principle? Solution. If x π, cos x 1 = cos and if y 1, sinh y sinh 1 as sinh y is an increasing function. It follows that u(x, y) = sinh y sinh 1 cos(x) sinh 1 sinh 1 cos() = 1 = u(, 1). The maximum value of u(x, y) on the rectangle (x, y), x π, y 1} is thus 1 and is reached at the point (, 1) which is on the boundary of the rectangle and not an interior point in accordance with the maximum principle. Continued... Page 13 of 22

8. (1 pts.) Solve the Poisson equation u xx + u yy = x 2 + y 2, x 2 + y 2 < 1, u(x, y) =, x 2 + y 2 = 1. by passing to polar coordinates (See Problem 4). Express your final answer in rectangular coordinates. (Hint. Look for a solution that depends only on r.) Solution. Let x = r cos θ and y = r sin θ and suppose that u(x, y) = v(r), for some function v. Then, v (r) + 1 r v (r) = r 2 and v(1) =. The function w = v satisfies the first-order linear ODE The integrating factor is e 1/r dr = e ln r = r. We have thus Integrating yields w (r) + 1 w(r) = r2 r r w (r) + w(r) = (r w(r)) = r 3 r w(r) = r4 r3 + C or w(r) = 4 4 + C r. Since w(r) = v (r) should be continuous at r =, we need C =. We have thus v (r) = w(r) = r3 4 and thus after integrating, v(r) = r4 16 + D. The condition v(1) = yields D = 1. We have thus 16 v(r) = r4 1 16 and the solution is given in rectangular coordinates as u(x, y) = (x2 + y 2 ) 2 1. 16 Continued... Page 14 of 22

Continued... Page 15 of 22

9. (a) (5 pts.) Compute the Fourier series of the function f(x) = e x, π < x < π, in its complex form (i.e. e x = n= c n e inx, π < x < π). Solution. We have c n = 1 2 π = 1 2 π = 1 2 π = 1 2 π π π π π [ e (1 in)x e x e inx dx e (1 in)x dx 1 in ] π π e (1 in)π e (1 in)π 1 in The Fourier series expansion of e x is thus given by e x = n= ( 1) n 2 π = ( 1)n 2 π e π e π 1 in ( ) e π e π e inx, π < x < π. 1 in Continued... Page 16 of 22

(b) (7 pts.) Apply Parseval s identity to the function in part (a) and the complete orthogonal system e inx } n Z on the interval ( π, π) to prove the formula n= 1 1 + n 2 = π eπ + e π e π e π. Solution. Letting X n (x) = e inx for n Z and f(x) = e x, we have using (a), π ( ) e (f, X n ) = e x e inx dx = ( 1) n π e π, n Z, 1 in π and f 2 = (f, f) = X n 2 = (X n, X n ) = π π f(x) 2 dx = π π π π e inx e inx dx = (e x ) 2 dx = π π π π 1 dx = 2 π, [ e e 2x 2x dx = 2 ] π π = e2π e 2π. 2 Since Parseval s identity yields ( ) (f, X n ) 2 = e π e π 2 ( 1)n = (eπ e π ) 2, 1 in 1 + n 2 f 2 = e2π e 2π 2 = n= (f, X n ) 2 X n 2 = n= (e π e π ) 2 2 π (1 + n 2 ) which shows that n= 1 1 + n 2 = π e2π e 2π (e π e π ) 2 = π (eπ + e π ) (e π e π ) (e π e π ) 2 = π eπ + e π e π e π. Continued... Page 17 of 22

SCRATCH Continued... Page 18 of 22

SCRATCH Continued... Page 19 of 22

SCRATCH Continued... Page 2 of 22

SCRATCH Continued... Page 21 of 22

Some formulas you may use: where a n = 1 l f(x) a 2 + f(x) l l ( nπx a n cos l ), a n = 2 l ( nπx ) b n sin, b n = 2 l l f(x) a 2 + ( nπx ) f(x) cos dx, n, l l l ( nπx ) ( nπx a n cos + b n sin l l b n = 1 l ( nπx ) f(x) cos dx, < x < l. l ( nπx ) f(x) sin dx, < x < l. l l l ), l < x < l, ( nπx ) f(x) sin dx, n 1. l f(x) c n e πinx/l, l < x < l, with c n = 1 2 l n= If X n (x)} is a complete orthogonal system on (a, b), l l f(x) e πinx/l dx. with f(x) n X (x) + λx(x) =, (f, X n ) X n 2 X n(x), λ n = X() = X(l) =, X (x) + λx(x) =, λ X () = X n = (l) =, X (x) + λx(x) =, X(l) = X( l), X ( l) = X (l) =, f 2 = n (f, X n ) 2 X n 2. ( nπ ) 2, Xn (x) = sin(nπx/l), n 1. l ( nπ ) 2, Xn (x) = cos(nπx/l), n. l λ n = ( nπ ) 2, n l X (x) = 1, X n (x) = A n cos(nπx/l) + B n sin(nπx/l), n 1. u(x, t) = 1 4πkt e (x y)2 /4kt φ(y) dy. *** THE END*** Page 22 of 22