Tests made on 32-ft whirling arm of Daniel Guggenheim Airship Institute of rectangular wing of NACA 23012 section to determine rolling and yawing moment due to angular velocity in yaw.


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    Title :

    Pressure-distribution measurements on rectangular wing with partial-span split flap in curved flight


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Rokus, F.G. (author)


    Publication date :

    1939


    Size :

    7 pages


    Remarks:

    8 Supp sheets


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :