AE 416

fall 2022
 
All Classes

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.

Closed
Section Status Closed
Open
Section Status Open
Pending
Section Status Pending
Open (Restricted)
Section Status Open (Restricted)
Unknown
Section Status Unknown
Detail Status CRN Type Section Time Day Location Instructor