AA210A Fundamentals of Compressible Flow - Stanford …cantwell/AA210A_Course_Material/Wing... · Stanford University Department of Aeronautics and Astronautics AA210A Fundamentals

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AA210AFundamentals of Compressible Flow

Example - Drag of a 2-D airfoil

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Control Volume

Problem - Relate the drag of a 2-D airfoil in steady flow to itswake flow field.

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AA210A Fundamentals of Compressible Flow - Stanford …cantwell/AA210A_Course_Material/Wing... · Stanford University Department of Aeronautics and Astronautics AA210A Fundamentals

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