AER E 311: Aerodynamics II: Compressible Flow
(3-0) Cr. 3. F.S.
Prereq: AER E 310, M E 231
Review of thermodynamics, energy equation, compressible flow, and isentropic flow. Normal and oblique shocks. Mach waves and expansion fans. Applications to ducts and nozzles. Compressible airfoil and wing theory. Introduction to advanced compressible flow topics.
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