Rolling and yawing moments due to ailerons of various chords and spans on Clark-Y and U.S.A.-27 wing sections studied; effect of scale on rolling and yawing moments; effect of slightly rounding wing tips; results apply to level flight with wing chord set at plus 4-deg. angle of attack and to zero pitch, yaw, and roll; work conducted in 10-ft. Bureau of Standards wind tunnel.


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    Title :

    Effect of variation of chord and span of Ailerons on rolling and yawing moments in level flight


    Additional title:

    Nat. Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1929


    Size :

    19 pages


    Remarks:

    27 Figs., Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English