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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 9 - Partial Differential Equations

Introduction to Symmetry Analysis

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

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Page 1: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

Introduction to Symmetry Analysis

Brian CantwellDepartment of Aeronautics and Astronautics

Stanford University

Chapter 9 - Partial Differential Equations

Page 2: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

Finite transformation of partial derivatives

Page 3: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

The p-th extended finite group is

Page 4: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

Variable count

Page 5: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

Infinitesimal transformation of first partial derivatives

Page 6: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

Substitute

Page 7: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

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

Page 8: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

The number of terms in the infinitesimal versus the derivative order

Page 9: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

Page 10: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

Isolating the determining equations of the group - the Lie algorithm

Page 11: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

The classical point group of the heat equation

Page 12: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

Invariance condition

Page 13: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

The fully expanded invariance condition is

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

Page 14: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

The determining equations of the point group of the heat equation

Page 15: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

Series solution of the determining equations

Page 16: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

The classical six-parameter group of the heat equation

Page 17: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

Impulsive source solutions of the heat equation

Boundary conditions

Page 18: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

Is the integral conserved?

Page 19: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

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 Analysis

Stanford University Department of Aeronautics and Astronautics

Similarity variables are the invariants of the infinitesimal transformation.

Page 21: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

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 Analysis

Stanford University Department of Aeronautics and Astronautics

Page 23: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

A modified problem of an instantaneous heat source

Page 24: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

Page 25: Introduction to Symmetry Analysis

Stanford University Department of Aeronautics and Astronautics

Invariant group