System is needed in isolating causes of performance deficiencies in airplane development program, determining accuracy of predictions of performance and of flight testing, etc; 2 methods under study are gas-generator method, by General Electric, and traversing-rake method, by Grumman Aircraft Engineering Corp; feasibility and accuracy of latter which samples pressures and temperatures through engine exhaust, were compared with gas-generator method in subsonic flight; results of first 8 runs show agreement within 1% gross thrust and 5% net thrust with rake as standard; rake promises developmental and research application bypassing extensive engine-test cell calibrations.


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    Titel :

    Measurement of net thrust in flight


    Weitere Titelangaben:

    J Aircraft


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

    Erschienen in:

    Erscheinungsdatum :

    1964


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Thrust measurement in flight

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


    Measurement of net thrust in flight

    DAVIDSON, T. W. | AIAA | 1964


    MEASUREMENT OF NET THRUST IN FLIGHT

    DAVISON, T. | AIAA | 1963


    THRUST MEASUREMENT FOR FLAPPING-FLIGHT COMPONENTS

    Send, W. / Scharstein, F. / International Council of the Aeronautical Sciences; Optimage Ltd | British Library Conference Proceedings | 2010


    Method of net thrust measurement in supersonic flight

    Davidson, T.W. | Engineering Index Backfile | 1965