The paper discusses mixing problems in hypervelocity scramjet combustors. Techniques for providing turbulence and/or mixing enhancement are described. One such technique, the oscillating shock interaction, is studied numerically and options for producing oscillatory shock waves for mixing augmentation in scramjet combustors are discussed.


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    Titel :

    A mixing augmentation technique for hypervelocity scramjets


    Beteiligte:
    Kumar, A. (Autor:in) / Bushnell, D. M. (Autor:in) / Hussaini, M. Y. (Autor:in)

    Erscheinungsdatum :

    01.06.1987


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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