Modifications to model such as changes in fuselage shape, leading edge extensions on wing, special wing bodies, and lower surface ridges on wing were investigated to determine effects on longitudinal stability and maximum lift-drag ratio; Mach number range from 0.40 to 0.96 was covered.


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    Title :

    Longitudinal aerodynamic characteristics of high-subsonic-speed transport airplane model with cambered 40° sweptback wing of aspect ratio 8 at Mach numbers to 0.96


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    88 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :