aa210a fundamentals of compressible flow

Stanford University Department of Aeronautics and Astronautics AA210A Fundamentals of Compressible Flow Example - Drag of a 2-D airfoil

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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.

Page 3: AA210A Fundamentals of Compressible Flow

Stanford University Department of Aeronautics and Astronautics

Page 4: AA210A Fundamentals of Compressible Flow

Stanford University Department of Aeronautics and Astronautics

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