Location of separation point on surface of body is determined by pressure rise communicated upstream through subcritical base flow; by using moment method of Reeves and Lees, separation-interaction region is joined to near-wake interaction region passing through "throat" downstream of rear stagnation point; viscous flow over blunt body overexpands and goes supercritical; flow is joined to near-wake by means of supercritical-subcritical "jump" upstream of separation, and jump location is determined; application of method and comparison of results.


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    Titel :

    Laminar boundary-layer separation and near-wake flow for smooth blunt body at supersonic and hypersonic speeds


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Grange, J.M. (Autor:in) / Klinenberg, J.M. (Autor:in) / Lees, L. (Autor:in)

    Erschienen in:

    AIAA Journal ; 5 , n 6


    Erscheinungsdatum :

    1967


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :