1–39 von 39 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

    Physical Insight into Fuel/Air Mixing with Hypermixer Injectors for Scramjet Engines

    Ogawa, Hideaki / Kodera, Masatoshi | AIAA | 2015

      Physical Insight into Fuel/Air Mixing with Hypermixer Injectors for Scramjet Engines

      Ogawa, Hideaki | Online Contents | 2015
      Beteiligte: Kodera, Masatoshi

    Turbulence Model Effects on RANS Simulations of the Direct-Connected Scramjet Combustor Test

    Nishiguchi, Hironobu / Kodera, Masatoshi / Tomioka, Sadatake | AIAA | 2020

      TURBULENCE MODEL EFFECTS ON RANS SIMULATIONS OF THE DIRECT- CONNECTED SCRAMJET COMBUSTOR TEST

      Nishiguchi, Hironobu / Kodera, Masatoshi / Tomioka, Sadatake | TIBKAT | 2020

    Flush Air Data Sensing System for a Sharp-Nosed Hypersonic Vehicle with Curved-Wedge Forebody

    Takahashi, Hidemi / Kodera, Masatoshi / Tani, Kouichiro | AIAA | 2020

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

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

      INFLUENCE OF TURBULENCE MODELLING ON COMBUSTOR FLOWFIELD IN SCRAMJET MODE OF RBCC ENGINE

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

    Construction and Validation of a CFD Prediction Tool of Scramjet Combustor Performance for a Flight Experiment

    Kodera, Masatoshi / Takahashi, Masahiro / Kobayashi, Kan et al. | AIAA | 2024

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

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

    Numerical Study on the Supersonic Mixing Enhancement Using Streamwise Vortices

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

    Combustion Characteristics of Jet Fuel in Supersonic Airflow with Hydrocarbon-Fueled Vitiation Air Heater

    Kobayashi, Kan / Tomioka, Sadatake / Takahashi, Masahiro et al. | AIAA | 2024

    Numerical Analysis of Scramjet Mode Operation of a RBCC Engine

    Kodera, Masatoshi / Tomioka, Sadatake / Ueda, Shuichi et al. | AIAA | 2012

    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

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

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

    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

    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

    Numerical investigation of an RBCC combustor during Ramjet/Scramjet mode transition

    Salloum, Joseph / Candon, Michael J. / Ridings, Andrew et al. | AIAA | 2018

    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

    Aeroheating measurements on a reentry capsule model in free-piston shock tunnel HIEST

    Tanno, Hideyuki / KODERA, Masatoshi / Tomoyuki, KOMURO et al. | AIAA | 2010

    Performance of a Rocket-Ramjet Combined-Cycle Engine Model under Ramjet-Mode Operations

    Tomioka, Sadatake / Kato, Kanenori / Tani, Kouichiro et al. | AIAA | 2012

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

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

    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

    Scramjet inlet flow computations by hybrid grid method

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

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

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

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

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

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

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

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

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

    Mach 8 Flight condition Tests of Rocket-Ramjet Combined-Cycle Engine Model

    Takegoshi, Masao / Tomioka, Sadatake / Kodera, Masatoshi et al. | AIAA | 2013

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

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

    JAXA RD1 Flight Experiment on Supersonic Combustion: Part 2 Combustion Test Result

    Takahashi, Masahiro / Kobayashi, Kan / Takegoshi, Maso et al. | AIAA | 2023

      JAXA RD1 Flight Experiment on Supersonic Combustion: Part 2 Combustion Test Result

      Takahashi, Masahiro / Kobayashi, Kan / Takegoshi, Maso et al. | TIBKAT | 2023