MATH 220: Problem Set 3 Solutions

Similar documents
MATH 220: Problem Set 3 Solutions

MATH 220: MIDTERM OCTOBER 29, 2015

MATH 173: PRACTICE MIDTERM SOLUTIONS

Math Partial Differential Equations 1

Chapter 3 Second Order Linear Equations

Math 220A - Fall 2002 Homework 5 Solutions

Final: Solutions Math 118A, Fall 2013

Summer 2017 MATH Solution to Exercise 5

x ct x + t , and the characteristics for the associated transport equation would be given by the solution of the ode dx dt = 1 4. ξ = x + t 4.

Math 124A October 11, 2011

MA 201: Partial Differential Equations D Alembert s Solution Lecture - 7 MA 201 (2016), PDE 1 / 20

Math 220a - Fall 2002 Homework 6 Solutions

Differential equations, comprehensive exam topics and sample questions

MATH 131P: PRACTICE FINAL SOLUTIONS DECEMBER 12, 2012

MATH 425, FINAL EXAM SOLUTIONS

Math 311, Partial Differential Equations, Winter 2015, Midterm

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

Mathematical Methods - Lecture 9

The first order quasi-linear PDEs

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

Partial Differential Equations

HOMEWORK 5. Proof. This is the diffusion equation (1) with the function φ(x) = e x. By the solution formula (6), 1. e (x y)2.

0.3.4 Burgers Equation and Nonlinear Wave

Math 126 Final Exam Solutions

Partial Differential Equations, Winter 2015

UNIVERSITY OF MANITOBA

Math 342 Partial Differential Equations «Viktor Grigoryan

There are five problems. Solve four of the five problems. Each problem is worth 25 points. A sheet of convenient formulae is provided.

Propagation of discontinuities in solutions of First Order Partial Differential Equations

Numerical Solutions to Partial Differential Equations

CLASSIFICATION AND PRINCIPLE OF SUPERPOSITION FOR SECOND ORDER LINEAR PDE

Partial Differential Equations

First order wave equations. Transport equation is conservation law with J = cu, u t + cu x = 0, < x <.

Partial Differential Equations Separation of Variables. 1 Partial Differential Equations and Operators

The second-order 1D wave equation

Analysis III (BAUG) Assignment 3 Prof. Dr. Alessandro Sisto Due 13th October 2017

Homework 3 solutions Math 136 Gyu Eun Lee 2016 April 15. R = b a

Hyperbolic PDEs. Chapter 6

LECTURE NOTES FOR MATH 124A PARTIAL DIFFERENTIAL EQUATIONS

Math 4263 Homework Set 1

UNIVERSITY OF MANITOBA

ENGI 4430 PDEs - d Alembert Solutions Page 11.01

Metric Spaces. Exercises Fall 2017 Lecturer: Viveka Erlandsson. Written by M.van den Berg

Diffusion on the half-line. The Dirichlet problem

MATH 819 FALL We considered solutions of this equation on the domain Ū, where

MATH 32A: MIDTERM 2 REVIEW. sin 2 u du z(t) = sin 2 t + cos 2 2

First order Partial Differential equations

Modeling Rarefaction and Shock waves

z x = f x (x, y, a, b), z y = f y (x, y, a, b). F(x, y, z, z x, z y ) = 0. This is a PDE for the unknown function of two independent variables.

Week 4 Lectures, Math 6451, Tanveer

6 Non-homogeneous Heat Problems

Chapter 1: Introduction

Salmon: Lectures on partial differential equations

UNIVERSITY of LIMERICK OLLSCOIL LUIMNIGH

Notes: Outline. Shock formation. Notes: Notes: Shocks in traffic flow

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

WEAK ASYMPTOTIC SOLUTION FOR A NON-STRICTLY HYPERBOLIC SYSTEM OF CONSERVATION LAWS-II

Some Aspects of Solutions of Partial Differential Equations

MATH 220: PROBLEM SET 1, SOLUTIONS DUE FRIDAY, OCTOBER 2, 2015

Introduction of Partial Differential Equations and Boundary Value Problems

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

The Maximum and Minimum Principle

PARTIAL DIFFERENTIAL EQUATIONS. Lecturer: D.M.A. Stuart MT 2007

u xx + u yy = 0. (5.1)

2. Method of Characteristics

Reading: P1-P20 of Durran, Chapter 1 of Lapidus and Pinder (Numerical solution of Partial Differential Equations in Science and Engineering)

Lecture 19: Heat conduction with distributed sources/sinks

Introduction to Partial Differential Equations, Math 463/513, Spring 2015

= 2e t e 2t + ( e 2t )e 3t = 2e t e t = e t. Math 20D Final Review

Georgia Tech PHYS 6124 Mathematical Methods of Physics I

2.3. VECTOR SPACES 25

Advanced Calculus Math 127B, Winter 2005 Solutions: Final. nx2 1 + n 2 x, g n(x) = n2 x

Dynamics of Propagation and Interaction of Delta-Shock Waves in Conservation Law Systems

Math 4B Notes. Written by Victoria Kala SH 6432u Office Hours: T 12:45 1:45pm Last updated 7/24/2016

Solutions in the sense of distributions. Solutions in the sense of distributions Definition, non uniqueness

9 More on the 1D Heat Equation

Nonlocal Symmetry and Generating Solutions for the Inhomogeneous Burgers Equation

Quasi-linear first order equations. Consider the nonlinear transport equation

Partial Differential Equations Summary

Part A 5 Shorter Problems, 8 points each.

Vibrating-string problem

MATH 425, HOMEWORK 3 SOLUTIONS

Problem Set 1. This week. Please read all of Chapter 1 in the Strauss text.

MATH 23 Exam 2 Review Solutions

Lecture Notes on PDEs

(1) u (t) = f(t, u(t)), 0 t a.

MATH 31BH Homework 5 Solutions

Suggested Solution to Assignment 7

Waves in a Shock Tube

Hyperbolic Systems of Conservation Laws. in One Space Dimension. I - Basic concepts. Alberto Bressan. Department of Mathematics, Penn State University

Classification of Second order PDEs

CHAPTER 3. Analytic Functions. Dr. Pulak Sahoo

Math 5588 Final Exam Solutions

MATH 251 Final Examination December 16, 2014 FORM A. Name: Student Number: Section:

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

Applied Math Qualifying Exam 11 October Instructions: Work 2 out of 3 problems in each of the 3 parts for a total of 6 problems.

THE NATIONAL UNIVERSITY OF IRELAND, CORK COLÁISTE NA hollscoile, CORCAIGH UNIVERSITY COLLEGE, CORK. Summer Examination 2009.

Math 342 Partial Differential Equations «Viktor Grigoryan

Strauss PDEs 2e: Section Exercise 3 Page 1 of 13. u tt c 2 u xx = cos x. ( 2 t c 2 2 x)u = cos x. v = ( t c x )u

A Recursion Formula for the Construction of Local Conservation Laws of Differential Equations

Transcription:

MATH 220: Problem Set 3 Solutions Problem 1. Let ψ C() be given by: 0, x < 1, 1 + x, 1 < x < 0, ψ(x) = 1 x, 0 < x < 1, 0, x > 1, so that it verifies ψ 0, ψ(x) = 0 if x 1 and ψ(x)dx = 1. Consider (ψ j ) j 1 constructed as ψ j (x) = jψ(jx), so that ψ j (x) = 0 if x 1/j, and ψ j(x)dx = 1, for all j 1. (1) Let us show that ι ψj δ 0 in D (). By definition, it means that we need to prove that, for all φ Cc (), ψ j (x)φ(x)dx δ 0 (φ) = φ(0). So let s prove that for every ɛ > 0, there exists j 0 such that for all j j 0, ψ j (x)φ(x)dx φ(0) < ɛ. (2) Let ɛ > 0 and φ Cc (). Since φ is continuous, there exists η > 0 such that for all x < η, φ(x) φ(0) < ɛ. Then consider j 0 such that 1/j 0 < η. Since we know that ψ j (x) = 0 for all x 1/j, ψ j(x)dx = 1, and ψ j (x) 0 for all x, for all j j 0 we have: ψ j (x)φ(x)dx φ(0) = ɛ 1/j ψ j (x)φ(x)dx 1/j 1/j 1/j ψ j (x) φ(x) φ(0) dx ψ j (x)dx = ɛ. ψ j (x)φ(0)dx (2) Let φ C c () be such that φ(x) = 1 for all x < 1. Then, for j 1, ψ j (x) 2 φ(x)dx = 0 1/j (1) (3) 1/j j 2 (1 + jx) 2 dx + j 2 (1 jx) 2 dx = 2j 0 3. (4) 1

Therefore, as j +, converge. } + Consequently, {ι ψ 2j j=1 ψ j (x) 2 φ(x)dx +, and does not converge to any distribution since does not converge for the very φ we exhibited. { } + ι ψ 2 j (φ) does not j=1 { } + ι ψ 2 j (φ) { } + (3) We have just shown that ι ψj δ 0, but ι ψ 2 j (φ) does not converge j=1 to any distribution. Therefore there is no continuous extension of the map Q : f f 2 on C() to D (). j=1 Problem 2. We consider the conservation law: u t + (f(u)) x = 0, u(x, 0) = φ(x), (5) with f C 2 (). Since u is continuous and f is C 2, v = f (u) is also continuous. Since u is C 1 apart from jump discontinuities in its first derivatives, away from the jumps, u t (resp. u x ) is perfectly defined and continuous. Therefore, since f is C 1, and away from the discontinuities, v t = f (u)u t (resp. v x = f (u)u x ) is also continuous, v is C 1 apart from jump discontinuities in its first derivatives (the same ones as u). Therefore v has the same properties as u. Moreover, we have, away from discontinuities: v t +vv x = f (u)u t +f (u)f (u)u x = f (u)(u t +f (u)u x ) = f (u)(u t +(f(u)) x ) = 0. (6) So v verifies the Burger s equation (the ankine-hugoniot condition is vacuous: there are no shock since v is continuous). If f > 0, f is strictly convex and f is strictly increasing and therefore the inverse function (f ) 1 exists. We can therefore first solve for v from the Burger s equation: v t + vv x = 0, v(x, 0) = f (φ(x)), (7) and then u = (f ) 1 (v) is solution of the original PDE. Suppose now that u has a jump discontinuity. ankine-hugoniot condition: Then, according to the ξ (t) = f(u +) f(u ) u + u. (8) If v could have been defined as previously, v would have the same discontinuity (v = f (u)) and again by ankine-hugoniot: ξ (t) = v 2 + 2 v2 2. = 1 v + v 2 (v + + v ) = 1 2 (f (u + ) + f (u )). (9) 2

But in general, f(u + ) f(u ) u + u. 1 2 (f (u + ) + f (u )) (10) (consider for instance f(x) = e x ) and the statement is FALSE. Problem 3. Consider Burger s equation u t + uu x = 0, u(x, 0) = φ(x), (11) with initial condition 0, x < 1, 1 x, 1 < x < 0, φ(x) = 1 + x, 0 < x < 1, 0, x > 1. (12) (1) To build the weak solution, it is very convenient to draw the characteristic curves. In the Burger case, we know that the solution u is constant along the characteristic curves x r (t) = φ(r)t + r. As long as the characteristic curves don t intersect, we have: If r < 1, then φ(r) = 0, which implies that the characteristic curves are and the solution u(x, t) = 0 along those curves, x r (t) = r, r < 1, (13) If 1 < r < 0, then φ(r) = 1 r, which implies that the characteristic curves are x r (t) = ( 1 r)t + r, 1 < r < 0, (14) and the solution u(x, t) = 1 r = 1 x + t 1 t = x + 1 along those t 1 curves. If 0 < r < 1, then φ(r) = 1 + r, which implies that the characteristic curves are x r (t) = ( 1 + r)t + r, 0 < r < 1, (15) and the solution u(x, t) = 1 + r = 1 + x + t 1 + t = x 1 along those t + 1 curves. If r > 1, then φ(r) = 0, which implies that the characteristic curves are and the solution u(x, t) = 0 along those curves. x r (t) = r, r > 1, (16) 3

To sum up, we have that, for t small, 0, x < 1, x + 1 u(x, t) = t, x 1 t + 1, 0, x > 1. x+t 1 < x < t, ( 1 < 1 t < 0) x+t 1 < x < t, (0 < 1+t < 1) (17) Now, from the sketch of the characteristic curves and/or the condition 1 < x < t of the solution, we can see that the characteristic curves don t intersect while t < 1. Therefore the above solution is valid for t < 1. The curves intersect at t = 1 Beyond that time, we therefore consider a weak solution satisfying the ankine-hugoniot condition. At the level of the discontinuity ξ(t), we have that u (ξ(t), t) = 0 and u + (ξ(t), t) = ξ(t) 1 t + 1, and ξ(1) = 1. Therefore the ankine-hugoniot condition is 0 1 ξ 2 (t) = ( ) 2 ξ(t) 1 t+1 0 ξ(t) 1 t+1 Hence, ξ verifies the following ODE: ξ (t) = 1 ξ(t) 1 2 t + 1, ξ(1) = 1. = 1 ξ(t) 1 2 t + 1. (18) (19) Solve it (say, by separation of variables) and you get ξ(t) = 1 2(1 + t). Therefore, for t 1, the solution is 0, 1 < x < 1 2(1 + t), x 1 u(x, t) = t + 1, 1 2(1 + t) < x < 1, (20) 0, x > 1. (2) There are two cases for t to consider. For 0 t < 1, And for t > 1, Therefore u(x, t)dx = t 1 u(x, t)dx = x + 1 1 t 1 dx + t 1 1 2(1+t) u(x, t)dx is indeed constant. x 1 dx = 1. (21) t + 1 x 1 dx = 1. (22) t + 1 4

(3) Let us call E(t) = For 0 t < 1, we have E(t) = w(x, t)dx = t 1 w(x, t)dx, where w = u 3. ( ) 3 x + 1 1 dx + t 1 t ( ) 3 x 1 dx = 1 t + 1 2. (23) So E(t) is indeed constant before a shock develops, but for t > 1, E(t) = w(x, t)dx = 1 and E(t) is no longer a constant. 1 2(1+t) Let s now explain what is going on here. ( ) 3 x 1 dx = 1 t + 1 t + 1, (24) Following Problem 2, if we define g(x) = 3 4 x4/3, we have that u = g (w). From Problem 2, we know that w t + (g(w)) x = 0. After the shock develops, we have for u: d u(x, t)dx = d 1 u(x, t)dx dt dt ξ(t) = = 1 ξ(t) 1 ξ(t) (u + ) t ξ (t)u + (ξ(t), t) ( ) 1 2 u2 + ξ (t)u + (ξ(t), t) x = 1 2 u +(ξ(t), t) 2 ξ (t)u + (ξ(t), t) = 0, (25) from the ankine-hugoniot jump condition (remember u = 0). Meanwhile for w we have: d w(x, t)dx = d dt dt = = 1 ξ(t) 1 ξ(t) 1 ξ(t) w(x, t)dx (w + ) t ξ (t)w + (ξ(t), t) (g(w + )) x ξ (t)w + (ξ(t), t) = g(w + (ξ(t), t)) ξ (t)w + (ξ(t), t) 0, (26) because w does not satisfy the same ankine-hugoniot condition. Problem 4. 5

(1) u xx u xy 2u yy = 0. (27) ( ) 1 1/2 We have A =. Therefore det(a) = 2 1/4 = 9/4 < 0, 1/2 2 and T r(a) = 1 + 2 = 3 < 0. Therefore the eigenvalues of A are non zero and of opposite signs: Hyperbolic PDE. (2) u xx 2u xy + u yy = 0. (28) ( ) 1 1 We have A =. Therefore det(a) = 0. Therefore at least one 1 1 of the eigenvalues of A is zero: Degenerate PDE. (3) u xx + 2u xy + 2u yy = 0. (29) ( ) 1 1 We have A =. Therefore det(a) = 2 1 = 1 > 0 and T r(a) = 1 2 3 > 0. Therefore the eigenvalues of A are non zero and of the same sign: Elliptic PDE. Problem 5. (1) Let s find the general C 2 solution of the PDE u xx u xt 6u tt = 0, (30) by reducing it to a system of first order PDEs (by the way, this is an elliptic PDE). We are looking for a, b, c, d that formally verify: xx xt 6 tt = (a x + b t ) (c x + d t ) = ac xx + (ad + bc) xt + bd tt. So we get the (under-determined) system: ac = 1 ad + bc = 1 bd = 6. (31) (32) From the first equation, let us simply take a = c = 1. Then the system reduces to { d + b = 1 (33) bd = 6, which gives b = 2 and d = 3. 6

Therefore we can write u xx u xt 6u tt = 0 as ( x + 2 t ) ( x 3 t ) u = 0. Now let v = ( x 3 t ) u. Then v verifies v x + 2v t = 0 (first order linear PDE!). And we know that the solution writes v(x, t) = h(t 2x) for some h C 1. Now for u we have the system: u x 3u t = h(t 2x). (34) Using the method of characteristics, we get the following equations: x r(s) = 1, x r (0) = 0, t r(s) = 3, t r (0) = r, v r(s) = h(t r (s) 2x r (s)), v r (0) = φ(r), (35) for some function φ C 2. Therefore we have x r (s) = s, t r (s) = 3s + r, and and by integrating from s = 0, we get: v r(s) = h( 3s + r 2s) = h( 5s + r), (36) v r (s) = s 0 = 1 5 h( 5s + r)ds + φ(r) 5s+r r h(y)dy + φ(r), (37) after a change of variables. Now, since we have s = x and r = t + 3x, we finally get: for some f, g C 2. t+3x u(x, t) = 1 h(y)dy + φ(t + 3x) 5 t 2x = f(t + 3x) + g(t 2x), (38) eciprocally, we verify that u of the form u(x, t) = f(t + 3x) + g(t 2x) for f, g C 2 indeed solves the PDE. (2) For an arbitrary φ Cc ( 2 ) we have to show that u(φ xx φ xt 6φ tt ) = v(φ xx φ xt 6φ tt ) + w(φ xx φ xt 6φ tt ) = 0. (39) But from Problem 2 of Pset 2, we have: v(φ xx φ xt 6φ tt ) = v(( x 3 t ) (φ x + 2φ t )) = 0, (40) and similarly, w(φ xx φ xt 6φ tt ) = w(( x + 2 t ) (φ x 3φ t )) = 0. (41) 7

Problem 6. Let us solve (in the strong sense): { uxx + 3u x, y, xy 4u yy = xy, u(x, x) = sin x, u x (x, x) = 0. (42) Same strategy here, we reduce it to a system of first order PDEs (by the way, this is an hyperbolic PDE!). We are looking for a, b, c, d that formally verify: xx + 3 xy 4 yy = (a x + b y ) (c x + d y ) = ac xx + (ad + bc) xy + bd yy. So we get the (under-determined) system: ac = 1 ad + bc = 3 bd = 4. (43) (44) From the first equation, let us simply take a = c = 1. Then the system reduces to { d + b = 3 (45) bd = 4, which gives, say, b = 1 and d = 4. Therefore we can write u xx + 3u xy 4u yy = 0 as ( x y ) ( x + 4 y ) u = 0. Now let v = ( x + 4 y ) u. Then v verifies v x v y = xy (first order semilinear PDE!), and (u x + u y ) (x,x) = sin (x) = cos(x), u x (x, x) = 0 imply that u y (x, x) = cos(x) and v(x, x) = 4 cos(x). Therefore v satisfies the following PDE: { vx v y = xy, (46) v(x, x) = 4 cos(x). The ODEs for the characteristics are then: x r(s) = 1, x r (0) = r, y r(s) = 1, y r (0) = r, v r(s) = x r (s)y r (s), v r (0) = 4 cos(r). After solving, we get: x r (s) = s + r, y r (s) = r s, (47) (48) v r (s) = r 2 s s3 3 + 4 cos(r). Therefore we get the PDE for u: ( ) 2 ( ) x + y x y u x + 4u y = v(x, y) = + 1 ( ) 3 ( ) x y x + y + 4 cos, 2 2 3 2 2 u(x, x) = sin(x). (49) 8

Writing once again the characteristic ODEs for the PDE, we get: x r(s) = 1, x r (0) = r, y r(s) = 4, y r (0) = r, v r(s) = v(x r (s), y r (s)), v r (0) = sin(r). (50) After solving, we get: x r (s) = s + r, y r (s) = 4s + r, v r (s) = sin(r) + s 0 ( 1 3 ( 3 2 τ ) 3 = 9 32 s4 75 32 s4 5 2 s3 r 3 4 s2 r 2 + 8 5 sin Therefore (and finally): u(x, t) = 1 16 ( ) 2 ( ) ( y x 5x + y 5y + 13x 3 3 3 ( ) 2 ( ) ) 5τ + 2r 3τ 5τ + 2r 2 2 + 4 cos dτ 2 ( ) 5s + 2r 3 2 5 sin (r). (51) ) + 8 ( ) x + y 5 sin 3 ( 4x y 2 5 sin 3 (52) ). Problem 7. with and Let s solve the wave equation on the line: u tt c 2 u xx = 0, u(x, 0) = φ(x), u t (x, 0) = ψ(x), (53) 0, x < 1, 1 + x, 1 < x < 0, φ(x) = 1 x, 0 < x < 1, 0, x > 1, 0, x < 1, ψ(x) = 2, 1 < x < 1, 0, x > 1. (54) (55) We know from the course (method of characteristics) that the solution is: u(x, t) = 1 2 (φ(x + ct) + φ(x ct)) + 1 2c x+ct ψ(y)dy. (56) Now, notice first that since c, t 0, then x ct x + ct. As you can see in the figure, there are 10 cases to consider for the solution: 1. If x + ct < 1 and x ct < 1 (domain 1), then u(x, t) = 0. 9

2. If 1 x + ct < 0 and x ct < 1 (domain 2), then u(x, t) = 1 2 (1 + x + ct + 0) + 1 x+ct ( 1 2dy = 2c 2 + 1 ) (1 + x + ct). (57) c 3. If 0 x + ct < 1 and x ct < 1 (domain 3), then u(x, t) = 1 2 (1 +0)+ 1 2c 1 x+ct 4. If 1 x + ct and x ct < 1 (domain 4), then 1 u(x, t) = 0 + 1 2c 2dy = 1 2 (1 x ct)+ 1 (1 + x + ct). c (58) 1 5. If 1 x + ct < 0 and 1 < x ct < 0 (domain 5), then 1 u(x, t) = 1 2 (1 + x + ct + 1 + x ct) + 1 2c 2dy = 2 c. (59) x+ct 6. If 0 x + ct < 1 and 1 < x ct < 0 (domain 6), then u(x, t) = 1 2 (1 x ct + 1 + x ct) + 1 2c x+ct 7. If 1 x + ct and 1 x ct < 0 (domain 7), then u(x, t) = 1 2 (0+1+)+ 1 2c 1 8. If 0 x + ct < 1 and 0 x ct < 1 (domain 8), then u(x, t) = 1 2 (1 x ct + 1 x + ct) + 1 2c 2dy = 1 + x + 2t. (60) 2dy = 1 ct + 2t. (61) 2dy = 1 2 (1 + x ct)+ 1 (1 x + ct). c (62) x+ct 9. If 1 x + ct and 0 x ct < 1 (domain 9), then u(x, t) = 1 2 (1 x ct) + 1 2c 1 2dy = 1 x + 2t. (63) 2dy = 1 2 (1 + x ct) + 1 (1 x + ct). c (64) 10. If 1 x + ct and 1 x ct (domain 10), then u(x, t) = 0. Finally, as we can now see, u(x, t) vanishes in region (1) and (10). Since φ(x) = 0 and ψ(x) = 0 in x > 1, this result corresponds to Huygens principle. Moreover, u(x, t) is C 1 except on the lines x + ct = 1, x + ct = 0, x + ct = 1, x ct = 1, x ct = 0 and x ct = 1. Since φ(x) and ψ(x) are C 1 everywhere except at x = 1, 0, 1, this result corresponds to the propagation of singularities: u(x, t) is C 1 near (x, t) if φ and ψ are such near x ± ct. 10