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Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford University Chapter 9 - Partial Differential Equations

Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

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Page 1: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

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Introduction to Symmetry Analysis

Brian Cantwell Department of Aeronautics and Astronautics

Stanford University

Chapter 9 - Partial Differential Equations

Page 2: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

!Finite transformation of partial derivatives

Page 3: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

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The p-th extended finite group is

Page 4: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

!Variable count

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Infinitesimal transformation of first partial derivatives

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!Substitute

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The (p-1)th order extended infinitesimal transformation is

Page 8: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

!The number of terms in the infinitesimal versus the derivative order

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Page 10: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

!Isolating the determining equations of the group - the Lie algorithm

Page 11: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

!The classical point group of the heat equation

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Invariance condition

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The fully expanded invariance condition is

Apply the constraint that the solution must satisfy theheat equation and gather terms

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The determining equations of the point group of the heat equation

Page 15: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

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Series solution of the determining equations

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The classical six parameter group of the heat equation

Page 17: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

!Impulsive source solutions of the heat equation

Boundary conditions

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Is the integral conserved?

Page 19: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

!This problem is invariant under the three parameter group of dilationsin the dependent and independent variables and translation in time.

Page 20: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

!Similarity variables are the invariants of the infinitesimal transformation.

Page 21: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

!Now substitute the similarity form of the solution into the heat equation.The result is a second order ODE of Sturm-Liouville type.

Page 22: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

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Page 23: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

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Page 24: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

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Page 25: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

!Flow in porous media - A modified problem of an instantaneous heat source.

Darcy's law

Pressure diffuses in a porous medium.

Page 26: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

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Page 27: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

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Page 28: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

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Page 29: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

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Page 30: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

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Page 31: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

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9.135 9.131

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9.135 9.131

Page 33: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

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Example computation from Barenblatt Scaling, self-similarity and intermediate asymptotics

Page 34: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

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ξ = − C2 coth C2 x +C1 C2⎡⎣ ⎤⎦

Note that

Also satisfies

ξxx − 2ξξx = 0

Page 39: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

!What solutions do these groups correspond to?

dx− C2 Tanh C2 x +C1 C2⎡⎣ ⎤⎦

= dt1= du0

ordx

− C2 Coth C2 x +C1 C2⎡⎣ ⎤⎦= dt1= du0

Characteristic equations

Similarity variables (invariants)

θ = eC2tSinh[ C2 x +C1 C2 ]U = uor

θ = eC2t Cosh[ C2 x +C1 C2 ]U = u

Page 40: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

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What solution does this group correspond to?

Let u =U θ[ ]Substitute into the heat equation

ut =U ' θ[ ]θtux =U ' θ[ ]θ x

uxx =U '' θ[ ] θ x( )2 +U ' θ[ ]θ xx

ut − uxx =U ' θ[ ] θt −θ xx( )−U '' θ[ ] θ x( )2 = 0θt −θ xx = 0⇒U '' θ[ ] = 0U θ[ ] = Aθ + B

u = AeC2t Sinh[ C2 x +C1 C2 ]+ B

u = AeC2t Cosh[ C2 x +C1 C2 ]+ B

Solutions

θ = eC2tSinh[ C2 x +C1 C2 ]U = uor

θ = eC2t Cosh[ C2 x +C1 C2 ]U = u

Page 41: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

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Let’s look for a solution of the heat equation using separation of variables

ut = uxx

Let u = g t[ ] f x[ ]ut = gt fux = gfxuxx = gfxx

Substitute gt f = gfxx

This equality implies gtg= fxx

f= λ

Page 42: Introduction to Symmetry Analysiscantwell/AA218_Course_Material/... · 2018-05-08 · Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford

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The solution of the heat equation derived by separation of variables matches the solution generated from non-classical symmetries.

gtg= fxx

f= λ

g = Aeλt

f = Sinh λ x + a⎡⎣ ⎤⎦

f = Cosh λ x + a⎡⎣ ⎤⎦

u = Aeλt Sinh λ x + a⎡⎣ ⎤⎦ + B

u = Aeλt Cosh λ x + a⎡⎣ ⎤⎦ + B

Letλ = C2

a = C1 C2

u = AeC2t Sinh C2 x +C1 C2⎡⎣ ⎤⎦ + B

u = AeC2t Cosh C2 x +C1 C2⎡⎣ ⎤⎦ + B

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Include also the case c=constant. Identify the Lorentz transformation