Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    DESIGN AND ANALYSIS OF A HIGH PRESSURE RATIO MIXED FLOW COMPRESSOR STAGE (AIAA 2016-4744)


    Beteiligte:
    Nassar, Abdul (Autor:in) / Giri, Gaurav (Autor:in) / Moroz, Leonid (Autor:in) / Sherbina, Andrey (Autor:in) / Klimov, Ivan (Autor:in)

    Kongress:

    Joint propulsion conference



    Erscheinungsdatum :

    01.01.2016


    Format / Umfang :

    12 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



    Nr. 4744

    DataCite | 1936


    Effect of Serpentine Nozzle on Bypass Ratio of Turbofan Engine Exhaust (AIAA 2018-4744)

    Sun, Peng / Zhou, Li / Wang, Zhanxue et al. | British Library Conference Proceedings | 2018


    Design and Analysis of a High Pressure Ratio Mixed Flow Compressor Stage

    Nassar, Abdul / Giri, Gaurav / Moroz, Leonid et al. | AIAA | 2016


    AIAA-2002-4744 The Impact of Maneuver Failures on the EOS Afternoon Constellation

    Demarest, P. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2002


    AIAA-2002-4744 The Impact of Maneuver Failures on the EOS Afternoon Constellation

    Demarest, P. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2002