Investigation of influence of radiant energy transport on structure of inviscid flow field in stagnation region of blunt-nosed body in hypersonic flight; approximate solutions are obtained for various levels of approximation in treating radiative transport; higher-order approximate solution is obtained which includes at each point local self-absorption of radiation emitted by hotter gas in neighborhood of point; solution exhibits correct physical behavior throughout flow field and predicts that gas temperature approaches well-defined nonzero value at body surface.
Transparency assumption in hypersonic radiative gas dynamics
AIAA J
AIAA Journal ; 3 , n 8
1965
7 pages
Article (Journal)
English
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