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nonequilibrium nozzle flows, flowfield variables, supersonic blunt body problem, induced mass motion, vortical singularity, compressible flow applications, equilibrium chemically reacting mixture, oblique shock diffuser, vortical singularities, incident expansion wave, equilibrium chemically reacting gas, calorically perfect gas, rearward differences, entropy streamline, subsonic inflow boundary, velocity potential equation, oblique shock properties, oblique shock theory, unsteady wave motion, hypersonic similarity, flowfield values, blunt body flowfield, nonequilibrium expansion, normal shock properties, locally supersonic flow
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United States, Solution From Table, World War, Theodore von Karman, Adolf Busemann, Isaac Newton, John Stack, Substitute Eqs, Air Force, Ludwig Prandtl, Jet Propulsion Engine Thrust, Leonhard Euler, Technische Hochschule, Cal Tech, Daniel Bernoulli, English Engineering System, Langley Aeronautical Laboratory, New York, Proceedings of the Royal Society, Solution From Example, Some Theoretical Aspects of Transonic Flows, The Basics, After Anderson, Examine Eqs, General Conservation Equations Revisited
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