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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    Titel :

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


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Report


    Beteiligte:
    Weick, F.E. (Autor:in) / Shortal, J.A. (Autor:in)


    Erscheinungsdatum :

    1932


    Format / Umfang :

    8 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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