Investigation of lifting effectiveness and flow requirements of blowing boundary layer control applied to trailing edge flaps and ailerons of aircraft, with sufficient blowing jet momentum to prevent flow separation on flap, lift increment increased for flap deflections up to 80°.


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    Title :

    Large-scale wind-tunnel tests of airplane model with un-swept, aspect-ratio-10 wing, two propellers, and blowing flaps


    Additional title:

    NASA -- Memo


    Contributors:


    Publication date :

    1958


    Size :

    47 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :