Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Numerical Study and Performance Evaluation for Pulse Detonation Engine with an Aerospike Nozzle


    Beteiligte:
    Tsuboi, Nobuyuki (Autor:in) / Kawakami, Yuzi (Autor:in) / Ezure, Ryosuke (Autor:in) / Hayashi, A.Koichi (Autor:in) / Yamada, Eisuke (Autor:in)

    Kongress:

    49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition



    Erscheinungsdatum :

    01.01.2011




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    NUMERICAL STUDY AND PERFORMANCE EVALUATION FOR PULSE DETONATION ENGINE WITH AN AEROSPIKE NOZZLE

    Tsuboi, N. / Kawakami, Y. / Ezure, R. et al. | British Library Conference Proceedings | 2011


    Three-dimensional Numerical Simulation on Hydrogen-Oxygen Rotating Detonation Engine with Unchoked Aerospike Nozzle

    Tsuboi, Nobuyuki / Jourdaine, Nicolas H. / Watanabe, Tomohiro et al. | AIAA | 2018


    Augmented aerospike nozzle, engine including the augmented aerospike nozzle, and vehicle including the engine

    LAPSA ANDREW / FELDMAN THOMAS | Europäisches Patentamt | 2024

    Freier Zugriff

    Pressure Characteristics of an Aerospike Nozzle in a Rotating Detonation Engine

    Schwer, Douglas A. / Brophy, Christopher M. / Kelso, Robert H. | AIAA | 2018