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.


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    Title :

    Transparency assumption in hypersonic radiative gas dynamics


    Additional title:

    AIAA J


    Contributors:

    Published in:

    AIAA Journal ; 3 , n 8


    Publication date :

    1965


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :