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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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Stanford University Department of Aeronautics and Astronautics
Introduction to Symmetry Analysis
Brian CantwellDepartment of Aeronautics and Astronautics
Stanford University
Chapter 9 - Partial Differential Equations
Stanford University Department of Aeronautics and Astronautics
Finite transformation of partial derivatives
Stanford University Department of Aeronautics and Astronautics
The p-th extended finite group is
Stanford University Department of Aeronautics and Astronautics
Variable count
Stanford University Department of Aeronautics and Astronautics
Infinitesimal transformation of first partial derivatives
Stanford University Department of Aeronautics and Astronautics
Substitute
Stanford University Department of Aeronautics and Astronautics
The (p-1)th order extended infinitesimal transformation is
Stanford University Department of Aeronautics and Astronautics
The number of terms in the infinitesimal versus the derivative order
Stanford University Department of Aeronautics and Astronautics
Stanford University Department of Aeronautics and Astronautics
Isolating the determining equations of the group - the Lie algorithm
Stanford University Department of Aeronautics and Astronautics
The classical point group of the heat equation
Stanford University Department of Aeronautics and Astronautics
Invariance condition
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
Stanford University Department of Aeronautics and Astronautics
The determining equations of the point group of the heat equation
Stanford University Department of Aeronautics and Astronautics
Series solution of the determining equations
Stanford University Department of Aeronautics and Astronautics
The classical six-parameter group of the heat equation
Stanford University Department of Aeronautics and Astronautics
Impulsive source solutions of the heat equation
Boundary conditions
Stanford University Department of Aeronautics and Astronautics
Is the integral conserved?
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.
Stanford University Department of Aeronautics and Astronautics
Similarity variables are the invariants of the infinitesimal transformation.
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.
Stanford University Department of Aeronautics and Astronautics
Stanford University Department of Aeronautics and Astronautics
A modified problem of an instantaneous heat source
Stanford University Department of Aeronautics and Astronautics
Stanford University Department of Aeronautics and Astronautics
Invariant group