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    Titel :

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


    Beteiligte:

    Kongress:

    AIAA international space planes and hypersonic systems and technologies conference



    Erscheinungsdatum :

    2015-01-01


    Format / Umfang :

    10 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



    Starting Characteristics of Hypersonic Pre-cooled Turbojet Inlet

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


    Performance Evaluation of Hypersonic Pre-Cooled Turbojet Engine (AIAA 2015-3593)

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


    ACH 4 PERFORMANCE EVALUATION OF HYPERSONIC PRE-COOLED TURBOJET ENGINE (AIAA 2018-5203)

    Taguchi, Hideyuki / Hongoh, Motoyuki / Kojima, Takayuki et al. | British Library Conference Proceedings | 2018


    Mach 4 Wind Tunnel Experiment of Hypersonic Pre-Cooled Turbojet Engine (AIAA 2014-2790)

    Taguchi, H. / Harada, K. / Kobayashi, H. et al. | British Library Conference Proceedings | 2014


    Nr. 3595

    DataCite | 1914