Naval Air Test Center is engaged in development of method for measuring in-flight net thrust for turbojet airplanes; most satisfactory methods stuied were Gas Generator method and Traversing Rake method; latter system is composed of hydraulic rotary actuator, torque shaft assembly that is coaxial with actuator, and rake which measures total and static pressures, and temperature; automatic data processing system involves data acquisition via airborne analog magnetic tape, analog to digital conversion, computer processing on IBM 7030-Stretch System, high speed printing and cathode ray tube plotting; concept was evaluated using North American Vigilante airpalen; system provided exceptional accuracy of thrust measurement.


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    Titel :

    Method of net thrust measurement in supersonic flight


    Weitere Titelangaben:

    AGARDograph


    Beteiligte:
    Davidson, T.W. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    28 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Full Flight Envelope Direct Thrust Measurement on a Supersonic Aircraft

    Conners, T. R. / Sims, R. L. / American Institute of Aeronautics and Astronautics et al. | British Library Conference Proceedings | 1998


    Full Flight Envelope Direct Thrust Measurement on a Supersonic Aircraft

    Conners, Timothy R. / Sims, Robert L. | NTRS | 1998




    Thrust measurement in flight

    Humphreys, J.D. | Engineering Index Backfile | 1954