Results are given in form of load distributions and as calculated moment coefficients; experimental values of rolling and yawing moment coefficients were in fairly close agreement with theory.


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    Title :

    Pressure distribution measurements on tapered wing with partial-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 :

    6 pages


    Remarks:

    6 Supp sheets, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :