Tests to find lift, drag, and center-of-pressure characteristics of split-flap airfoil with internal air passage; highest lift coefficient 2.08 obtained with passage closed.


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    Title :

    Wind-tunnel tests of hall high-lift wing


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Contributors:
    Weick, F.E. (author) / Sanders, R. (author)


    Publication date :

    1932


    Size :

    4 pages


    Remarks:

    6 Supp plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Wind tunnel tests of a hall high lift wing

    Weick, Fred E. ;Sanders, Robert | SLUB | 1932


    Wind-tunnel Tests of a Hall High-life Wing

    Weick, Fred E / Sanders, Robert | NTRS | 1932