It was found that, when airplane was rotated positively in pitch through angle of stall at rates of order of 0.1° per second, maximum lift coefficient was considerably higher than that obtained in standard tests, in which forces are measured with angles of attack fixed; all tests made on Fairchild 22. (10¢)


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    Titel :

    Comparative flight and full-scale wind-tunnel measurements of maximum lift of airplane


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Report


    Beteiligte:
    Silverstein, A. (Autor:in) / Katzoff, S. (Autor:in) / Hootman, J.A. (Autor:in)


    Erscheinungsdatum :

    1938


    Format / Umfang :

    7 pages


    Anmerkungen:

    Bibliography


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Comparative flight and full-scale wind tunnel measurements of maximum lift of airplane

    Silverstein, A. / Katzoff, S. / Hootman, J.A. | Engineering Index Backfile | 1938


    Comparative flight and full-scale wind-tunnel measurements of maximum lift of airplane

    Silverstein, A. / Katzoff, S. / Hootman, J.A. | Engineering Index Backfile | 1938



    Comparative flight and full-scale wind-tunnel measurements of the maximum lift of an airplane

    Silverstein, Abe / Katzoff, S. / Hootman, James A. | TIBKAT | 1938