Five-component force data showing effects of applying boundary layer control to flaps of fighter aircraft and data defining air flow requirements of boundary layer control system; with nose flap deflected 45° substantial improvements in maximum lift, aileron effectiveness, and longitudinal stability are obtained.


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    Title :

    Full-scale wind-tunnel tests of low-aspect-ratio, straight-wing airplane with blowing boundary-layer control on leading-and trailing-edge flaps


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1959


    Size :

    24 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :