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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    Title :

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


    Additional title:

    Nat. Advisory Committee Aeronautics -- Tech. Note


    Contributors:


    Publication date :

    1928


    Size :

    7 pages


    Remarks:

    19 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :