A local shock wave can destroy the evolution of supersonic combustion in a scramjet. The Reynolds number correlation of the systems of internal shock waves produced in such turbulent free shear layers are presently noted to imply that a direct connection with turbulence intensity exists. By way of this connection, as well as the adjustability of the Reynolds number, opportunities emerge for the control of turbulent shocklets; this will in turn allow control of their influence on supersonic mixing.


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    Titel :

    Evidence of Reynolds number sensitivity in supersonic turbulent shocklets


    Beteiligte:
    Johnson, J. A., III (Autor:in) / Zhang, Y. (Autor:in) / Johnson, L. E. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1988-04-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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