Considering both maximum lift coefficient and speed-range ratio CLmax CDmin, with flap neutral no appreciable improvement was found with use of more than single leading-edge slot.


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    Title :

    Effect of multiple fixed slots and trailing-edge flap on lift and drag of Clark Y airfoil


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:
    Weick, F.E. (author) / Shortal, J.A. (author)


    Publication date :

    1932


    Size :

    8 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :




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