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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    Titel :

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


    Weitere Titelangaben:

    Nat. Advisory Committee Aerodynamics -- Report


    Beteiligte:
    Knight, M. (Autor:in) / Wentzinger, C.J. (Autor:in)


    Erscheinungsdatum :

    1929


    Format / Umfang :

    49 pages


    Anmerkungen:

    60 Figs.


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :