AE 451
Fall 2016 Part of Term 1
Part of Term 1
Aug 22-Dec 7
Aug 22-Dec 7
Credit: 3 OR 4 hours.
In-depth examination of aerodynamic and dynamic structural phenomena associated with flexible airplanes and missiles; divergence of linear and nonlinear elastic lifting surfaces; effect of elastic and inelastic deformations on lift distributions and stability; elastic flutter of straight and swept wings; equations of disturbed motion of elastic and inelastic aircraft; dynamic response to forces, gusts, and continuous atmospheric turbulence; creep divergence of lifting surfaces; flutter in the presence of creep; effect of temperature on inelastic divergence and flutter.
3 undergraduate hours. 3 or 4 graduate hours. Prerequisite: AE 352 or TAM 412; TAM 251.
Section Status updates every 10 minutes.
| CRN | Type | Section | Time | Day | Location | Instructor | Section Details | |
|---|---|---|---|---|---|---|---|---|
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51603
|
Lecture-Discussion
|
A
|
10:00AM
-11:50AM
|
MW
|
Mechanical Engineering Bldg
|
Balajewicz, M
|
|