Results of test of wing equipped with Zap flap and Zap ailerons on Fairchild 22 airplanes to determine effect of flaps and ailerons on performance and control characteristics of airplane, showing that, when ailerons and horizontal tail surfaces were removed, flaps increased maximum lift coefficient from 1.48 to 2.39. (n 834)


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    Title :

    Full-scale wind-tunnel and flight tests of Fairchild 22 airplane equipped with zap flap and zap Ailerons


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Contributors:
    Dearborn, C.H. (author) / Soulee&acute (author) / H.A. (author)


    Size :

    17 pages


    Remarks:

    17 Supp sheets, Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English