Data presented in form of curves of sections lift, drag, and pitching moment coefficients for airfoil with flap deflected but with ailerons neutral, and of rolling, yawing, and hinge moment coefficients for rectangular wing of aspect ratio 6 with semi-span aileron and full span flap.


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    Title :

    Wind-tunnel test of three lateral-control devices in combination with full-span slotted flap on N.A.C.A. 23012 airfoil


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1938


    Size :

    11 pages


    Remarks:

    6 Supp sheets, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English