Purpose of study is to outline approximate methods that allow prediction of effects of high angle of attack, nonequilibrium flow chemistry, and vapor injection on subsonic flow field of blunt body in hypersonic speed range, to present results in terms of shockwave shape and location, stagnation-point location, and surface pressure for equilibrium flow, and in terms of shock-wave shape and location for nonequilibrium flow, and flow with vapor injection, and to compare, where possible, these results with available experiment or more exact theory.
Inviscid hypersonic flow around blunt bodies
AIAA J
AIAA Journal ; 3 , n 7
1965
8 pages
Article (Journal)
English
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Inviscid hypersonic flow around blunt bodies
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