Tests made on 32-ft whirling arm of Daniel Guggenheim Airship Institute of tapered wing to determine rolling and yawing moments due to angular velocity in yaw; results given in form of span load distributions and in calculated moment coefficients.


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    Title :

    Pressure-distribution measurements on tapered wing with full-span split flap in curved flight


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Troller, T. (author) / Rokus, F. (author)


    Publication date :

    1939


    Size :

    8 pages


    Remarks:

    8 supp sheets, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :