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AE 312 Compressible Flow
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 385, ME 300; credit or concurrent registration in AE 201.
Section Information
| CRN | Type | Section | Time | Days | Location | Instructor |
| 29874 | lecture- discussion | A | 01:00 PM - 01:50 PM | MWF | room 103 Talbot Laboratory | Elliott, G |
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