Review of current studies of compressible flow problems connected with extremely high speeds and altitudes contemplated in supersonic aircraft design; design features of 11-in. hypersonic tunnel; air condensation experiments; flow visualization at low pressures; boundary layer effects at hypersonic speeds; research on unsteady flows. (Abstract) (See also J Applied Physics v 21 n 7 July 1950 p 619-28)


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    Title :

    Results of recent hypersonic and unsteady flow research at Langley Aeronautical Laboratory


    Additional title:

    Aviation Week


    Contributors:

    Published in:

    Aviation Week ; 53 , n 5


    Publication date :

    1950


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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