1–20 von 38 Ergebnissen
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    Scramjet inlet flow computations by hybrid grid method

    Kodera, Masatoshi / Nakahashi, Kazuhiro / Hiraiwa, Tetsuo et al. | AIAA | 1998

    Extension of unstructured hybrid grid method to supersonic combustion flows

    Kodera, Masatoshi / Nakahashi, Kazuhiro | AIAA | 1999

    Numerical analysis of scramjet combusting flows by unstructured hybrid grid method

    Kodera, Masatoshi / Sunami, Tetsuji / Nakahashi, Kazuhiro | AIAA | 2000

    Effect of airframe geometry on thrust performance of aerospace plane

    Kodera, Masatoshi / Kanda, Takeshi / Tani, Kouichiro | AIAA | 2000

    Numerical study of mixing and combustion process of a scramjet engine model

    Kodera, Masatoshi / Sunami, Tetsuji / Nakahasi, Kazuhiro | AIAA | 2001

    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

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

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

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

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

    Effect of Ingested Boundary Layer on Scramjet Engines' Thrust and Combustion Characteristics

    Hiraiwa, Tetsuo / Kanda, Takeshi / Kodera, Masatoshi et al. | AIAA | 2003

    Numerical Simulation of a Scramjet Engine for JAXA's Flight Experiment Using Hyshot

    Kodera, Masatoshi / Sunami, Tetsuji / Itoh, Katsuhiro | AIAA | 2005

    Experimental Study of Strut Injectors in a Supersonic Combustor Using OH-PLIF

    Sunami, Tetsuji / Magre, Philippe / Bresson, Alexandre et al. | AIAA | 2005

    Performance Characteristics of a Scramjet Engine at Mach 10 to 15 Flight Condition

    Takahashi, Masahiro / Sunami, Tetsuji / Tanno, Hideyuki et al. | AIAA | 2005

    Effect of Combustor Shape on Scramjet Characteristics at Hypervelocity Condition over Mach 10 Flight

    Takahashi, Masahiro / Komuro, Tomoyuki / Sato, Kazuo et al. | AIAA | 2006

    Ignition Transient Phenomena in a Scramjet Engine at Mach 12 Flight Condition

    Kodera, Masatoshi / Yang, Vigor / Takahashi, Masahiro et al. | AIAA | 2007

    Improvement of Scramjet Combustor Performance at Hypervelocity Condition over Mach 10 Flight

    Takahashi, Masahiro / Komuro, Tomoyuki / Sato, Kazuo et al. | AIAA | 2008

    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

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

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