AE 312
spring 2005
All Classes
Compressible Flow
Credit: 3 hours.
(A A E 210) 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.
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