ME 609 - High-Speed Aerodynamics

3 credit(s)
Aerothermodynamics of high-speed aerodynamics. One-dimensional, high-speed flow. Prandtl-Meyer expansion waves, normal shock waves, and oblique shock waves. Shock-expansion theory of supersonic airfoils. Linearized theory of compressible high-speed flow over airfoils, Prandtl-Glauert equations, and supersonic flow over airfoils. Supersonic wing lift and pressure drag calculations.
Prerequisite(s): Graduate standing with M 344 or equivalent.

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