University at Buffalo 3 credits Mechanical & Aerospace Engr
Kinetic theory; governing equations for inviscid compressible flow of perfect gases; wave phenomena in one-dimensional unsteady flows; basic approximations and applications for steady flows in the subsonic, transonic, supersonic, and hypersonic regimes, including flow similitudes, imperfect gas effects at hypersonic speeds; viscous and aerodynamic heating effects, including compressible laminar boundary layers and shock-wave boundary layer interactions.
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