This report deals with the accelerations obtained in flight on various airplanes at Langley Field for the purpose of obtaining the magnitude of the load factors in flight and to procure information on the behavior of an airplane in various maneuvers. The instrument used in these tests was a recording accelerometer of a new type designed by the technical staff of the National Advisory Committee for Aeronautics. The instrument consists of a flat steel spring supported rigidly at one end so that the free end may be deflected by its own weight from its neutral position by any acceleration acting at right angles to the plane of the spring. This deflection is measured by a very light tilting mirror caused to rotate by the deflection of the spring, which reflected the beam of light onto a moving film. The motion of the spring is damped by a thin aluminum vane which rotates with the spring between the poles of an electric magnet. Records were taken on landings and takeoffs, in loops, spins, spirals, and rolls.


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    Titel :

    Accelerations in Flight


    Beteiligte:
    Norton, F H (Autor:in) / Allen, E T (Autor:in)

    Erscheinungsdatum :

    01.01.1921


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



    Accelerations in flight

    Doolittle, J.H. | Engineering Index Backfile | 1925


    Accelerations in flight

    Norton, F. H. / Allen, E. T. | TIBKAT | 1921


    Accelerations in flight

    Norton, F.H. / Allen, E.T. | Engineering Index Backfile | 1921


    Accelerations in Flight

    Doolittle, J H | NTRS | 1925


    Instrument for measuring low frequency accelerations in flight

    Draper, C.S. / Wrigley, W. | Engineering Index Backfile | 1940