AE 312
Spring 2008 All Classes
All Classes
Credit: 3 hours.
Compressible flow aerodynamics; conservation of mass, momentum, and energy; one-dimensional and quasi-one-dimensional flow; oblique shock waves and Prandtl-Meyer expansion waves; unsteady wave motion. Application to nozzles, diffusers, supersonic airfoils, and shock tubes.
Prerequisite: AE 311, CS 101, MATH 285, ME 300; credit or concurrent registration in AE 201.
Section Status updates every 10 minutes.
| CRN | Type | Section | Time | Day | Location | Instructor | Section Details | |
|---|---|---|---|---|---|---|---|---|
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29874
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Lecture-Discussion
|
A
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1:00PM
-1:50PM
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MWF
|
1310 Digital Computer Laboratory
|
Bodony, D
|
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