Slot injection problems include fuel injection, surface cooling and/ or skin-friction reduction, and alleviation of boundary-layer separation by energizing fluid near wall; study is divided into three areas; detailed profiles in near flowfield were determined with interferometer for air injection into Mach 2.1 airstream past flat plate; analytical treatment of turbulent mixing zone including effects of splitter plate boundary layer is presented and shown to provide predictions in excellent agreement with experiments; stability of mixing region is considered and experiments with spark shadowgraphs are reported.


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    Titel :

    Tangential slot injection in supersonic flow


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Schetz, J.A. (Autor:in) / Gilreath, H.E. (Autor:in)

    Erschienen in:

    AIAA Journal ; 5 , n 12


    Erscheinungsdatum :

    1967


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Tangential slot injection in supersonic flow.

    GILREATH, H. E. / SCHETZ, J. A. | AIAA | 1967


    Tangential slot injection in supersonic flow

    GILREATH, H. / SCHETZ, J. | AIAA | 1967



    Supersonic Skin-Friction Drag with Tangential Wall Slot Fuel Injection and Combustion

    Kirchhartz, Rainer M. / Mee, David J. / Stalker, Raymond J. | AIAA | 2012


    Combined tangential-normal injection into a supersonic flow

    KING, P. S. / THOMAS, R. H. / SCHETZ, J. A. et al. | AIAA | 1991