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![Page 1: AA210A Fundamentals of Compressible Flow - Stanford …cantwell/AA210A_Course_Material/Wing... · Stanford University Department of Aeronautics and Astronautics AA210A Fundamentals](https://reader034.vdocuments.net/reader034/viewer/2022050722/5a94a8b97f8b9a18628c4bcd/html5/thumbnails/1.jpg)
Stanford University Department of Aeronautics and Astronautics
AA210AFundamentals of Compressible Flow
Example - Drag of a 2-D airfoil
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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.
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Stanford University Department of Aeronautics and Astronautics
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Stanford University Department of Aeronautics and Astronautics