Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Performance Estimations of a Pulse Detonation Engine with Exit Nozzle


    Beteiligte:
    Tangirala, Venkat (Autor:in) / Dean, A. (Autor:in)

    Kongress:

    42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit



    Erscheinungsdatum :

    2006-01-01



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Performance Estimations of a Pulse Detonation Engine with Exit Nozzle

    Tangirala, V. / Dean, A. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2006


    Effects of injection nozzle exit width on rotating detonation engine

    Sun, Jian / Zhou, Jin / Liu, Shijie et al. | Elsevier | 2017


    Performance Estimations for Subsonic-to-Subsonic Flight Conditions of a Pulse Detonation Engine

    Tangirala, V. / Tsuboi, N. / Hayashi, K. et al. | British Library Conference Proceedings | 2008


    Performance Estimations for Subsonic-to-Subsonic Flight Conditions of a Pulse Detonation Engine

    Tangirala, Venkat / Tsuboi, Nobuyuki / Hayashi, Koichi | AIAA | 2008


    Effects of exit geometry on the performance of a pulse detonation engine

    Allgood, D. / Gutmark, E. / Katta, V. | AIAA | 2002