Real air hypersonic flow parameters are presented in tabular and graphical form for flight in earth's atmosphere as function of flight velocity and altitude; thermochemical equilibrium-flow properties are given for inviscid normal shock and stagnation point, and equilibrium and frozenflow parameters, including electron concentration, are listed for far wake of inviscid stagnation streamline.
Hypersonic shock-heated flow parameters for velocities to 46,000 feet per second and altitudes to 323,000 feet
NASA -- Tech Report
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