Section provided with 16 different slots near leading edge investigated to determine whether or not laminar stall characteristics of basic section might be delayed; substantial increases in maximum lift were realized with increasing flow into slot; chordwise location and width of slot found to be important.


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    Title :

    Experimental investigation of NACA 63-012 airfoil section with leading-edge suction slots


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    41 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :