A wall-injected, hydrogen-fueled scramjet is modeled numerically using a parabolic Navier-Stokes computer code with a k-epsilon turbulence model and finite-rate chemistry. The numerical results are compared to experimental scramjet data taken in a shock tunnel and are found to be in reasonable agreement. Under the conditions studied, the numerical results show that combustion in the scramjet is mainly mixing limited.


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    Title :

    Numerical modeling of wall-injected scramjet experiments


    Contributors:

    Published in:

    Publication date :

    1993-04-01



    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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