Lift, drag, pitching moment, pressure distribution, and boundary layer data given for two different leading edge slots operating in conjunction with midchord slot. See also Engineering Index 1948 p 28.


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    Title :

    Experimental investigation of NACA 631-012 airfoil section with leading-edge and midchord suction slots


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1950


    Size :

    23 pages


    Remarks:

    Diagrs, charts


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :