In this paper, a method of evaluation of the turbojet engine regulation condition in flight, based on information from its ground tests was presented. The tested engine was presented by the single comprehensive model which links input (in form of the modified signal mp4) and engine output (in form of the modified signal np2). Changes of the model parameters following during its operation can be defined using changes of the proposed simulation model parameters describing the engine operation both in flight and during ground tests.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Validity Check of the Assessment of a Jet Turbine Engine Regulation in Flight Using a Computer Simulation


    Beteiligte:
    Golak, Karol (Autor:in)


    Erscheinungsdatum :

    2013


    Format / Umfang :

    6 Seiten




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Print


    Sprache :

    Englisch




    Flight Training Selection Using Simulators - A Validity Assessment

    Garvin, J. / Acosta, S. / Murphy, T. | British Library Conference Proceedings | 1995


    Flight path cross check

    ALVAREZ JORGE A / LEEDOM DAVID L / MISHMASH BRIAN E | Europäisches Patentamt | 2018

    Freier Zugriff

    Analysis of Aircraft Simulation Validity in Different Flight Conditions

    Benyamen, Hady / Mays, Benjamin S. / Chowdhury, Mozammal et al. | IEEE | 2023


    In-Flight Gas Turbine Engine Icing: Review

    Tetteh, Edem / Loth, Eric / Neuteboom, Martin O. et al. | AIAA | 2022


    TRANSMISSION DATA FOR FLIGHT CHECK

    OTSUBO TOM / MULLIN RICHARD | Europäisches Patentamt | 2019

    Freier Zugriff