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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    Titel :

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


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    McCullough, G.B. (Autor:in) / Gault, D.E. (Autor:in)


    Erscheinungsdatum :

    1948


    Format / Umfang :

    41 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :