The aircraft/engine integration design numerical simulation model was established. The engine design performance specifications were obtained by calculating aircraft lift-drag characteristics, mission analysis, constraint analysis. Combining engine cycle parametric analysis with installation loss computing, the engine performance parameters can be found, which meet the aircraft flight envelope performance requirements. Taking double bypass variable cycle engine as an example to check the model, the results show that the variable cycle engine can meet aircrafts thrust and fuel consumption demands under different operating conditions, and achieve cruise thrust adjustment at the same inlet mass flow to reduce installation losses.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Areo-Engine Cycle Parametric Analysis and Installed Performance Calculation Based on Aircraft Flight Mission



    Erschienen in:

    Erscheinungsdatum :

    2013-12-19


    Format / Umfang :

    5 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Integrated Engine and Aircraft Mission Performance Analysis Using NPSS

    Kestner, Brian / Nam, Taewoo / Flett, Andrew et al. | AIAA | 2012


    Integrated Engine and Aircraft Mission Performance Analysis Using NPSS

    Kestner, B. / Nam, T. / Flett, A. et al. | British Library Conference Proceedings | 2012



    Parametric Cycle Analysis of Adaptive Cycle Engine

    Patel, Harinkumar R. / Wilson, Donald | AIAA | 2018