An outline of the project and recent progress toward the study of transition in hypersonic boundary layers is given. Aspects of the numerical method and the results of test computations are presented. At present the laminar flows over a flat plate have been computed for M less than or equal to 5.


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    Title :

    Transition to turbulence in hypersonic flow


    Contributors:


    Publication date :

    1990-02-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English







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