AE 416
Applied Aerodynamics
Credit: 3 or 4 hours.
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; application of V/STOL aerodynamics. 3 undergraduate hours. 3 or 4 graduate hours. Prerequisite: AE 311.
| CRN | Type | Section | Time | Days | Location | Instructor |
|---|---|---|---|---|---|---|
| 29803 | lecture- discussion | A | 10:00 AM - 10:50 AM | MWF | room 4101 Materials Science and Eng Bld | Selig, M |