Data presented in form of pressure distribution diagrams and graphs of calculated section coefficients for airfoil and flap combinations and also for flaps alone.


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    Title :

    Pressure distribution over N.A.C.A. 23012 airfoil with slotted and plain flap


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1938


    Size :

    32 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :