Tests with three different sized split trailing-edged flaps, in N.A.C.A. 7 by 10-ft wind tunnel; split flaps when deflected about their original axis locations gave slightly higher maximum lift coefficients than conventional trailing-edge flaps, and lift coefficients were increased still further by moving axes toward rear.


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    Title :

    Aerodynamic characteristics of model wing having split flap deflected downward and moved to rear


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Contributors:
    Weick, F.E. (author) / Harris, T.A. (author)


    Publication date :

    1932


    Size :

    7 pages


    Remarks:

    11 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :