Stanford University Department of Aeronautics and Astronautics.

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Presentation transcript:

Stanford University Department of Aeronautics and Astronautics

Introduction to Symmetry Analysis Brian Cantwell Department of Aeronautics and Astronautics Stanford University Chapter 1 - Introduction to Symmetry

Stanford University Department of Aeronautics and Astronautics (1.1) Symmetry in Nature Iconaster Longimanus Sunflower

Stanford University Department of Aeronautics and Astronautics

Angelina Jolie Original Image Right side reflection Left side reflection

Stanford University Department of Aeronautics and Astronautics (1.3) The discrete symmetries of objects 3x(4-1)=9 4x(3-1)=8 6x(2-1)=6 1 identity operation 24 member rotation group

Stanford University Department of Aeronautics and Astronautics (1.4) The twelve-fold discrete symmetry group of a snowflake

Stanford University Department of Aeronautics and Astronautics One can tell that the snowflake has been rotated. Therefore the 30° rotation is not a symmetry operation for the snowflake.

Stanford University Department of Aeronautics and Astronautics

(1.1) (1.2) Insert the discrete values  60°, 120°, 180°, 240°, 300° and 360°. The result is a set of six matrices corresponding to the six rotations. We can express the symmetry properties of the snowflake mathematically as a transformation.

Stanford University Department of Aeronautics and Astronautics (1.3)

Stanford University Department of Aeronautics and Astronautics

(1.4)

Stanford University Department of Aeronautics and Astronautics (1.5) (1.6) The group is closed under matrix multiplication.

Stanford University Department of Aeronautics and Astronautics

(1.7) (1.8)

Stanford University Department of Aeronautics and Astronautics

(1.4) The principle of covariance

Stanford University Department of Aeronautics and Astronautics (1.9) (1.5) Continuous symmetries of functions and differential equations

Stanford University Department of Aeronautics and Astronautics (1.10)

Stanford University Department of Aeronautics and Astronautics (1.11) (1.12)

Stanford University Department of Aeronautics and Astronautics (1.13) Use the transformation (1.9) and (1.13) to transform an ODE of the form (1.14) The symmetry of a first order ODE is analyzed in the tangent space (x, y, dy/dx) Transform the first derivative.

Stanford University Department of Aeronautics and Astronautics (1.15) (1.16)

Stanford University Department of Aeronautics and Astronautics

(1.17) (1.18)

Stanford University Department of Aeronautics and Astronautics (1.19) (1.20) (1.21) The solution curve (1.20) is transformed to

Stanford University Department of Aeronautics and Astronautics (1.22) (1.23)

Stanford University Department of Aeronautics and Astronautics

(1.24) (1.25) (1.26)

Stanford University Department of Aeronautics and Astronautics (1.27)

Stanford University Department of Aeronautics and Astronautics (1.28) (1.29)

Stanford University Department of Aeronautics and Astronautics (1.30) (1.31) (1.32)

Stanford University Department of Aeronautics and Astronautics (1.34) (1.35)

Stanford University Department of Aeronautics and Astronautics (1.36) (1.37) (1.38)

Stanford University Department of Aeronautics and Astronautics (1.39) (1.40) (1.41) For example let u=0 and let f = - t - x 2 /2 then

Stanford University Department of Aeronautics and Astronautics (1.6) Some Notation Conventions In group theory we make use of transformations of the following form (1.42) where the partial derivatives are (1.43)

Stanford University Department of Aeronautics and Astronautics Notation

Stanford University Department of Aeronautics and Astronautics Einstein used the following notation for partial derivatives. Note the comma (1.44) We use the Einstein convention on the summation of repeated indices (1.45)

Stanford University Department of Aeronautics and Astronautics Much of the theory of Lie groups relies on the infinitesimal form of the transformation expanded about small values of the group parameter. The function that infinitesimally transforms the derivative is of the form (1.46) (1.47) Function label Derivative

Stanford University Department of Aeronautics and Astronautics (1.7) Concluding Remarks (1.8) Exercises

Stanford University Department of Aeronautics and Astronautics