With split flaps of equal length both wings had same CLmax; if 30% of flap outer span were removed for installation of ailerons, reduction in CLmax of tapered wings with flaps might be expected of order of 4 to 7%; results of tests using ailerons of same span.


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    Title :

    Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1937


    Size :

    9 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :