AE628A - Continuum Hypersonic Aerodynamics
Prerequisites:
3-0-0-9
Course Contents
Continuum hyper Sonics in entry flight. Gen features, Mach no. Small disturb theory, similitude. Large deflect similitude; wedge, cone, wing. Unified similitude. Light hill & other piston analogies, Newton Busemann theory, thin shock layers, viscous in viscid interaction. Real gas. Frozen flow. Non equilibrium flow.
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