1–11 von 11 Ergebnissen
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    Numerical Analysis of Transient Phenomena to Ramjet Mode in a RBCC Combustor (AIAA 2015-3591)

    Kodera, Masatoshi / Ueda, Shuichi | British Library Conference Proceedings | 2015

    Influence of Turbulence Modelling on Combustor Flowfield in Scramjet Mode of RBCC Engine

    Salloum, Joseph / Candon, Michael / Ogawa, Hideaki et al. | AIAA | 2020

    Numerical Study on the Supersonic Mixing Enhancement Using Streamwise Vortices

    Kodera, Masatoshi / Sunami, Tetsuji / Sheel, Frithjof | AIAA | 2002

    Numerical Experiments of Scramjet Combustion with Boundary-Layer Bleeding

    Kouchi, Toshinori / Mitani, Tohru / Kodera, Masatoshi et al. | AIAA | 2003

    Influence of Thermal Non-equilibrium on Nozzle Flow Condition of High Enthalpy Shock Tunnel HIEST

    Takahashi, Masahiro / Kodera, Masatoshi / Itoh, Katsuhiro et al. | AIAA | 2009

    Mach 6 Test of a Scramjet Engine with Boundary-Layer Bleeding

    Kodera, Masatoshi / Tomioka, Sadatake / Kanda, Takeshi et al. | AIAA | 2003

    Study on Aerodynamic Characteristics of a High Enthalpy Flow around Blunt-nosed Body

    Takahashi, Masahiro / Satou, Kazuo / Itoh, Katsuhiro et al. | AIAA | 2012

    Effect of Airframe Configuration on Airflow Condition to Engine in Hypersonic Flow

    Kanda, Takeshi / Kato, Kanenori / Kodera, Masatoshi et al. | AIAA | 2003

    Comparison of Re-Entry Flow Computations with High Enthalpy Shock Tunnel Experiments

    Kodera, Masatoshi / Tanno, Hideyuki / Takahashi, Masahiro et al. | AIAA | 2009

    Flow Characterization of High Enthalpy Shock Tunnel Based on Shock Stand-off Distance

    Itoh, Katsuhiro / Komuro, Tomoyuki / Tanno, Hideyuki et al. | AIAA | 2009