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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    Title :

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


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1938


    Size :

    7 pages


    Remarks:

    Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    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