Results of force tests conducted in atmospheric wind tunnel through large range of angle of attack on series of monoplane and biplane wing models, to determine effects of variation in tip shape, aspect ratio, flap setting, stagger, gap, decalage, sweepback, and airfoil profile; effect of each and approximate autorotational characteristics in form of calculated ranges of rotary instability also given.


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    Title :

    Wind tunnel tests on a series of wing models through a large angle of attack range


    Additional title:

    Nat. Advisory Committee Aerodynamics -- Report


    Contributors:


    Publication date :

    1929


    Size :

    49 pages


    Remarks:

    60 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :