Problem of separation of effect of engine and propeller and of airplane on performance of whole airplane; tests made by D.V.L. (German Institute for Aeronautic Research); two new hubs for measuring propeller thrust and engine torque; limitations of accelerometer for measuring forces in airplane; more accurate method in which deflections are scratched on plate; test of float and hull resistance. For reference to original article in Zeit. fuer Flugtechnik und Motorluftschiffahrt, Oct. 7, 1929; see Engineering Index, 1928, p. 88.


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    Titel :

    Force measurements on airplanes


    Weitere Titelangaben:

    Nat. Advisory Committee Aeronautics -- Tech. Memorandums


    Beteiligte:
    Seewald, F. (Autor:in)


    Erscheinungsdatum :

    1929


    Format / Umfang :

    22 pages


    Anmerkungen:

    16 Figs.


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Force measurements on airplanes

    Seewald, F | NTRS | 1929


    Magnus force applied to airplanes

    Kucher, A.A. | Engineering Index Backfile | 1928


    Direct force control for light airplanes

    KOHLMAN, D. / ELLIS, D. | AIAA | 1974


    Airplanes

    Bilstein, Roger E. | Wiley | 2008


    All the U.S. Air Force Airplanes, 1907-1983

    Waters, Andrew W. / Waters, A. W. | TIBKAT | 1983