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Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

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Page 1: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

Page 2: Stanford University 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 1 - Introduction to Symmetry

Page 3: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

(1.1) Symmetry in Nature

Iconaster LongimanusSunflower

Page 4: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

Page 5: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

Angelina Jolie

Original Image Right side reflection Left side reflection

Page 6: Stanford University Department of Aeronautics and Astronautics

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)=61 identity operation

24 member rotation group

Page 7: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

(1.4) The twelve-fold discrete symmetry group of a snowflake

Page 8: Stanford University Department of Aeronautics and Astronautics

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.

Page 9: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

Page 10: Stanford University Department of Aeronautics and Astronautics

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.

Page 11: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

(1.3)

Page 12: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

Page 13: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

(1.4)

Page 14: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

(1.5)

(1.6)

The group is closed under matrix multiplication.

Page 15: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

Page 16: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

(1.7)

(1.8)

Page 17: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

Page 18: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

(1.4) The principle of covariance

Page 19: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

(1.9)

(1.5) Continuous symmetries of functions and differential equations

Page 20: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

(1.10)

Page 21: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

(1.11)

(1.12)

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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.

Page 23: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

(1.15)

(1.16)

Page 24: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

Page 25: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

(1.17)

(1.18)

Page 26: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

(1.19)

(1.20)

(1.21)

The solution curve (1.20) is transformed to

Page 27: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

(1.22)

(1.23)

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Stanford University Department of Aeronautics and Astronautics

Page 29: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

(1.24)

(1.25)

(1.26)

Page 30: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

(1.27)

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Stanford University Department of Aeronautics and Astronautics

(1.28)

(1.29)

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Stanford University Department of Aeronautics and Astronautics

(1.30)

(1.31)

(1.32)

Page 33: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

(1.34)

(1.35)

Page 34: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

(1.36)

(1.37)

(1.38)

Page 35: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

(1.39)

(1.40)

(1.41)

For example let u=0 and let f = - t - x2/2 then

Page 36: Stanford University Department of Aeronautics and Astronautics

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)

Page 37: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

Notation

Page 38: Stanford University Department of Aeronautics and Astronautics

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)

Page 39: Stanford University Department of Aeronautics and Astronautics

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

Page 40: Stanford University Department of Aeronautics and Astronautics

Stanford University Department of Aeronautics and Astronautics

(1.7) Concluding Remarks

(1.8) Exercises

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Stanford University Department of Aeronautics and Astronautics

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Stanford University Department of Aeronautics and Astronautics