Stanford University Department of Aeronautics and Astronautics
AA210AFundamentals of Compressible Flow
Example - Drag of a 2-D airfoil
Stanford University Department of Aeronautics and Astronautics
Control Volume
Problem - Relate the drag of a 2-D airfoil in steady flow to itswake flow field.
Stanford University Department of Aeronautics and Astronautics
Stanford University Department of Aeronautics and Astronautics
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