AE 416
Fall 2015 Part of Term 1
Part of Term 1
Aug 24-Dec 9
Aug 24-Dec 9
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.
Section Status updates every 10 minutes.
| CRN | Type | Section | Time | Day | Location | Instructor | Section Details | |
|---|---|---|---|---|---|---|---|---|
|
29803
|
Lecture-Discussion
|
A
|
1:00PM
-1:50PM
|
MWF
|
Digital Computer Laboratory
|
Selig, M
|
|