This report presents and discusses the results of an investigation to develop a rationale and technique for the validation of turbine engine steady-state mathematical models for use in predicting flight test performance, stability, and durability parameters. A validation procedure is derived and demonstrated using the YJ101 prototype engine AEDC test results and status deck as an example application of the technique. Typical status deck uncertainties as a function of flight condition, engine power setting, and deck input parameters are given. Status deck flight test input error effects are also given.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Turbine engine mathematical model validation


    Weitere Titelangaben:

    Bewertung von Turbomotoren aufgrund mathematischer Modelle


    Beteiligte:
    Hutcheson, L. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1976


    Format / Umfang :

    43 Seiten


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch






    Mathematical model of the gas turbine engine combustor fueling on ethanol

    Mykhailo Shevchenko / Maya Ambrozhevich / Oleh Selezen | DOAJ | 2024

    Freier Zugriff

    Empirical validation of turbine engine exhaust measurements

    Alwang, W.G. / Campbell, N.T. / Groth, R.H. | Tema Archiv | 1976