AE 416
fall 2005
All Classes
Applied Aerodynamics
Credit: 3 OR 4 hours.
(A A E 316) Two-dimensional and finite wing theory with emphasis on the mechanisms of lift and drag generation; Reynolds number and Mach number effects; drag analysis; high-lift wing systems; propeller and rotor aerodynamics; control surface design; and application of V/STOL aerodynamics. 3 undergraduate hours. 3 or 4 graduate hours. Prerequisite: AE 311 or equivalent; or consent of instructor.
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