AE 416
Fall 2004 Part of Term 1
Part of Term 1
Aug 25-Dec 10
Aug 25-Dec 10
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.
Section Status updates every 10 minutes.
| CRN | Type | Section | Time | Day | Location | Instructor | Section Details | |
|---|---|---|---|---|---|---|---|---|
|
29803
|
Lecture-Discussion
|
A
|
12:00PM
-12:50PM
|
MWF
|
Talbot Laboratory
|
Selig, M
|
|