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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    Title :

    A mixing augmentation technique for hypervelocity scramjets


    Contributors:

    Publication date :

    1987-06-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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