An airflow and thrust calibration of an F100 engine was conducted in coordination with a flight test program to study airframe-propulsion system integration characteristics of turbofan-powered high-performance aircraft. The tests were conducted with and without augmentation for a variety of simulated flight conditions with emphasis on the transonic regime. Test results for all conditions are presented in terms of corrected airflow and corrected gross thrust as functions of corrected fan speed for nonaugmented power and an augmented thrust ratio as a function of fuel-air ratio for augmented power. Comparisons of measured and predicted data are presented along with the results of an uncertainty analysis for both corrected airflow and gross thrust.


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    Titel :

    Altitude Calibration of an F100, S/N P680063, Turbofan Engine


    Beteiligte:
    T. J. Biesiadny (Autor:in) / D. Lee (Autor:in) / J. R. Rodriguez (Autor:in)

    Erscheinungsdatum :

    1978


    Format / Umfang :

    23 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Altitude calibration of an F100, S/N P680063, turbofan engine

    Biesiadny, T. J. / Lee, D. / Rodriguez, J. R. | NTRS | 1978


    Altitude calibration of an F100, S/N P680063, turbofan engine

    Biesiadny, Thomas J. / Lee, Douglas / Rodriguez, Jose R. | TIBKAT | 1978


    Multivariable control altitude demonstration on the F100 turbofan engine

    Lehtinen, B. / Dehoff, R. L. / Hackney, R. D. | NTRS | 1979


    Multivariable control altitude demonstration on the F100 turbofan engine

    Lehtinen, B. / Dehoff, R. L. / Hackney, R. D. | NTRS | 1979


    Multivariable control altitude demonstration on the F100 turbofan engine

    LEHTINEN, B. / DEHOFF, R. / HACKNEY, R. | AIAA | 1979