Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Starting Characteristics of Hypersonic Pre-cooled Turbojet Inlet


    Beteiligte:

    Kongress:

    20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference



    Erscheinungsdatum :

    2015-01-01



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Starting Characteristics of Hypersonic Pre-cooled Turbojet Inlet (AIAA 2015-3595)

    Kojima, Takayuki / Taguchi, Hideyuki / Kobayashi, Hiroaki et al. | British Library Conference Proceedings | 2015


    Performance Evaluation of Hypersonic Pre-Cooled Turbojet Engine

    Taguchi, Hideyuki / Kobayashi, Hiroaki / Kojima, Takayuki et al. | AIAA | 2015


    HYPERSONIC FLIGHT EXPERIMENT PLAN OF PRE-COOLED TURBOJET ENGINE

    Taguchi, H. / Kobayashi, H. / Kojima, T. et al. | British Library Conference Proceedings | 2012


    Hypersonic Flight Experiment Plan of Pre-Cooled Turbojet Engine

    Taguchi, Hideyuki / Kobayashi, Hiroaki / Kojima, Takayuki et al. | AIAA | 2012


    Research on hypersonic aircraft using pre-cooled turbojet engines

    Taguchi, Hideyuki / Kobayashi, Hiroaki / Kojima, Takayuki et al. | Elsevier | 2011