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AERO ENG 3171 Aerodynamics II (LEC 3.0)

Three dimensional incompressible wing theory. Compressible one dimensional flow with normal and oblique shock waves, heat addition, and friction. Compressible transonic, and supersonic linearized flow theory. Supersonic wings and wing/fuselage configurations. Prerequisite: "C" or better in Aero Eng 3131 and Mech Eng 2519.