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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    Titel :

    Transparency assumption in hypersonic radiative gas dynamics


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Thomas, P.D. (Autor:in)

    Erschienen in:

    AIAA Journal ; 3 , n 8


    Erscheinungsdatum :

    1965


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :