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Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford University Chapter 16 -Backlund Transformations And Nonlocal Groups
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Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Dec 18, 2015

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Page 1: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

Introduction to Symmetry Analysis

Brian CantwellDepartment of Aeronautics and Astronautics

Stanford University

Chapter 16 -Backlund TransformationsAnd Nonlocal Groups

Page 2: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

Singular behavior of Burgers’ Equation. Work out the steady state solution - invariant under translation in time.

Burgers’ Equation.

Page 3: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

C1 =1 / 2C2 =0

ν =2

ν =1 / 2

ν =1 / 8

Page 4: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

Exact solution of Burgers’ Equation

Conserved integral

Integrate the equation in space

Initial velocity distribution

Page 5: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

Non-dimensionalize the equation

The conserved integral becomes

Where the Reynolds number is

Page 6: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

Symmetries of the Burgers potential equation

Invariance condition

Group operators

Page 7: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

There is another solution of the invariance condition !!

With the independent variables not transformed,the invariance condition takes the following form

The invariance condition is satisfied by the infinitedimensional group

Where f is a solution of the heat equation

Page 8: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

What finite transformation does this correspond to ?To find out we have to sum the Lie series.

Where

First few terms

Page 9: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

Let

Page 10: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

The finite transformation of the Burgers potential equation is

Page 11: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

This group can be used to generate a corresponding transformation of the Burgers equation. Let

The transformation of Burgers equation is

This is an example of a nonlocal group

Page 12: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

The Cole-Hopf transformation. Let U = 0

Let

Page 13: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

The classical single hump solution of Burgers equation. Let

The Cole-Hopf transformation gives

where

Page 14: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

Page 15: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

Solitary Waves

Page 16: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

The Great Eastern

Page 17: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

Page 18: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

Page 19: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

Page 20: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

The Korteweg de Vries equation

is often used to study the relationship between nonlinear convection and dispersion.

Begin with the KdV potential equation

Page 21: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

Invariance condition for the KdV potential equation

Assume an infinitesimal transformation of the form

The invariance condition becomes

Page 22: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

The KdV potential equation admits the group with infinitesimal

The Lie series is

where

Page 23: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

Summing the Lie series leads to the non-local finite transformation

The simplest propagating solution of the KdV potential equation is

which generates the solution

Page 24: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

The corresponding solution of the KdV equation is the solitary wave

Page 25: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

One can use the group to generate an exact solution for two colliding solitons.

Page 26: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

Page 27: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

Singular behavior of Burgers’ Equation

d

dx

u2

2−ν

dudx

⎝⎜⎞

⎠⎟=0

u2

2−ν

dudx

=C1

dudx

=u2

2ν−C1

ν

u x( ) = 2C1Tanh 2C1 C2 −x2ν

⎛⎝⎜

⎞⎠⎟

⎛⎝⎜

⎞⎠⎟

Work out the steady state solution - invariant under translation in time

Page 28: Stanford University Department of Aeronautics and Astronautics Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics.

Stanford University Department of Aeronautics and Astronautics

C1 =1 / 2C2 =0

ν =2

ν =1 / 2

ν =1 / 8