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