Flight Investigation of Laminar and Turbulent Boundary Layers Passing Through Shock Waves at Full-Scale Reynolds Numbers.


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    Title :

    Flight investigation of laminar and turbulent boundary layers passing through shock waves at full-scale Reynolds numbers


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1953


    Size :

    20 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :