Study of shaping of bodies for different Mach numbers; wing, designed to have high performance characteristics when used with indented body, was tested in combination with unindented body and bodies for 1.0, 1.2, and 1.4 Mach; lowest values of zero lift wave drag and highest values of maximum lift drag ratio were obtained at or near Mach number for given indentations.


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    Title :

    Transonic investigation of changing indentation design Mach number on aerodynamic characteristics of 45° sweptback-wing-body combination designed for high performance


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1961


    Size :

    86 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :