Study made of 2 methods proposed to reduce high sinking speeds and improve landing characteristics of low aspect ratio hypersonic aircraft by placing wing at large angles of sideslip to increase its effective aspect ratio; summary of results obtained.


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    Title :

    Low-speed investigation of effects of large wing-sideslip angles on aerodynamic characteristics of two arrow-wing -- Fuselage arrangements


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1961


    Size :

    41 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :