Investigation of 2-dimensional airfoil; maximum lift of wing without suction was increased 43% for section flow coefficient of 0.0010 at free stream velocity of 162 fps. See also Engineering Index 1953 p 55.


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    Title :

    Section characteristics of NACA 0006 airfoil with area suction near leading edge


    Additional title:

    NACA -- Tech Note


    Contributors:


    Publication date :

    1954


    Size :

    47 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :