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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    Title :

    Force measurements on airplanes


    Additional title:

    Nat. Advisory Committee Aeronautics -- Tech. Memorandums


    Contributors:
    Seewald, F. (author)


    Publication date :

    1929


    Size :

    22 pages


    Remarks:

    16 Figs.


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Force measurements on airplanes

    Seewald, F | NTRS | 1929


    Magnus force applied to airplanes

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

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