Boundary layer transition measurement on windward side of flat plate in hypersonic wind tunnel, discussing unit Reynolds number effects at Mach 6


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    Title :

    Unit Reynolds number effects on boundary-layer transition at Mach 6.


    Contributors:

    Publication date :

    1968-05-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





    Unit-Reynolds-number effects on boundary-layer transition

    STETSON, KENNETH F. / KIMMEL, ROGER L. | AIAA | 1993