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. (see also abstract in Aviation Week v 53 n 5 July 1950 p 22, 24)


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    Title :

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


    Additional title:

    J Applied Physics


    Contributors:

    Published in:

    Publication date :

    1950


    Size :

    10 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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