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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    Title :

    Evidence of Reynolds number sensitivity in supersonic turbulent shocklets


    Contributors:

    Published in:

    Publication date :

    1988-04-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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