Available data in subsonic and supersonic flow for effects of free stream turbulence, surface curvature, pressure gradient, surface roughness, surface temperature, and Mach number on transition position; new supersonic data included from rocket flights, firing range tests, and wind tunnel tests.


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    Title :

    Boundary-layer stability and transition in subsonic and supersonic flow


    Additional title:

    J Aeronautical Sciences


    Contributors:

    Published in:

    Publication date :

    1953


    Size :

    10 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :