Most promising arrangement of full span lift flap and plain aileron combination tested, both for high lift and lateral control, was rectangular wing with 0.20cw flap deflected 60 at 0.90cw location with 0.10cw semi-span ailerons.


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    Title :

    Wind-tunnel investigation of rectangular and tapered N.A.C.A. 23012 wings with plain ailerons and full-span split flaps


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1938


    Size :

    11 pages


    Remarks:

    9 Supp sheets, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :