Configuration was tested in Ames pressurized ballistic range at Mach number of 4.9 to determine interaction of body bow wave with flow field about wing; shadowgraph pictures indicate that body bow wave crosses outer wing panel after first being refracted by interaction with flow field about wing.


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    Title :

    Shock-wave patterns on cranked-wing configuration


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    12 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :





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