Separate development of intake and nozzle may lead to components which are individually very efficient; when integrated into unit some of efficiency may be lost in producing compatibility with engine and remainder of powerplant; it is often found that the most efficient components lack flexibility in face of changing atmospheric conditions; flexibility can be achieved by suitable development and choice of components which would reduce demands on intake control system without incurring severe penalty in performance; problem is treated in terms of quasi-static effects of changes in ambient temperature on performance.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Fully integrated propulsion system for supersonic transport aircraft


    Weitere Titelangaben:

    AGARDograph


    Beteiligte:
    Talbot, J.E. (Autor:in) / Furness, B. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    26 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    SUPERSONIC AIRCRAFT PROPULSION INSTALLATION

    BRADBROOK STEPHEN J | Europäisches Patentamt | 2020

    Freier Zugriff

    Supersonic aircraft propulsion installation

    Europäisches Patentamt | 2018

    Freier Zugriff

    Integrated flight/propulsion control for supersonic STOVL aircraft

    Franklin, James A. / Stortz, Michael W. / Mihaloew, James R. | NTRS | 1990


    Supersonic aircraft propulsion installation

    BRADBROOK STEPHEN J | Europäisches Patentamt | 2022

    Freier Zugriff