Force tests on monoplane and biplane wing models with angle of attack from minus 45 to plus 90 deg. were conducted in Langley atmospheric wind tunnel; tests were to determine effects of variations of tip shape, aspect ratio, flap setting, stagger, gap, decalage, sweep back, and airfoil profile; effects produced given in preliminary form by comparative curves.


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    Titel :

    Wind tunnel force tests in wing systems through large angles of attack


    Weitere Titelangaben:

    Nat. Advisory Committee Aeronautics -- Tech. Note


    Beteiligte:
    Wenzinger, C.J. (Autor:in) / Harris, T.A. (Autor:in)


    Erscheinungsdatum :

    1928


    Format / Umfang :

    7 pages


    Anmerkungen:

    19 Figs.


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :