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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    Titel :

    Shock-wave patterns on cranked-wing configuration


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Sammonds, R.I. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :





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