Results of wind-tunnel tests made as part of investigation of lateral control devices; spoilers with chords up to 15.0% of wing chord tested in several locations on plain rectangular wing, and in two locations on same wing equipped with 20.0% chord split flap down 60°.


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    Title :

    Effect of retractable-spoiler location on rolling- and yawing-moment coefficients


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Contributors:


    Publication date :

    1934


    Size :

    12 pages


    Remarks:

    5 Supp plates, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English