Search Results1-14 of  14

  • KODERA Masatoshi ID: 9000002569001

    Combined Propulsion Research Group, Institute of Aerospace Technology (2007 from CiNii)

    Articles in CiNii:7

    • Effect of Inflow Boundary Layer Thickness on Scramjet Inlet Flowfields (1997)
    • Considerations of Mixing and Combustion of a Scramjet Engine : Transition Processes from Weak to Intensive Combustion Mode (2002)
    • Simulation of 3D Shock Wave / Turbulent Boundary Layer Interactions by Hybrid Grid Method(Proceedings of the 15th NAL Symposium on Aircraft Computational Aerodynamics) (1998)
  • KODERA Masatoshi ID: 9000005094344

    Ramjet Propulsion Research Division, National Aerospace Laboratory, Kakuda Research Center (2000 from CiNii)

    Articles in CiNii:1

    • Numerical Analysis of Scramjet Internal Flow by Hybrid Unstructured Grid Method (2000)
  • KODERA Masatoshi ID: 9000005728371

    JAXA (2009 from CiNii)

    Articles in CiNii:5

    • Scramjet testing in high enthalpy flow field (2002)
    • Hypermixer Scramjet Flight Experiment (2004)
    • Evaluation of Scramjet Testing Technology in the High Enthalpy Shock Tunnel HIEST (2004)
  • KODERA Masatoshi ID: 9000021474618

    Japan Aerospace Exploration Agency (2011 from CiNii)

    Articles in CiNii:1

    • Calibration of Oxygen Atom Mass Fraction in High Enthalpy Shock Tunnel Flow Based on Shock Stand-off Distance Measurement (2011)
  • KODERA Masatoshi ID: 9000240083091

    Japan Aerospace Exploration Agency Kakuda Space Center (2012 from CiNii)

    Articles in CiNii:1

    • Free-Flight Testing in the Gas-Driven Two-Stage Light Gas Gun HEK-G (2012)
  • KODERA Masatoshi ID: 9000254860760

    Articles in CiNii:1

    • Numerical Analysis of Scramjet Internal Flow by Hybrid Unstructured Grid Method. (2000)
  • KODERA Masatoshi ID: 9000256240958

    Articles in CiNii:1

    • Simulation of 3D Shock Wave/Turbulent Boundary Layer Interactions by Hybrid Grid Method. (1998)
  • KODERA Masatoshi ID: 9000256242032

    Articles in CiNii:1

    • Numerical Analysis of Scramjet Internal Flow by Hybrid Unstructured Grid Method. (1999)
  • KODERA Masatoshi ID: 9000256247523

    宇宙航空研究開発機構 (2004 from CiNii)

    Articles in CiNii:1

    • Evaluation of Scramjet Testing Technology in the High Enthalpy Shock Tunnel HIEST (2004)
  • KODERA Masatoshi ID: 9000256248388

    Japan Aerospace Exploration Agency, Space Propulsion Research Center (2005 from CiNii)

    Articles in CiNii:1

    • Force Measurement of Large-scale Scramjet Model within Short Test Duration (2005)
  • KODERA Masatoshi ID: 9000283632910

    Kakuda Space Center, Japan Aerospace Exploration Agency (2014 from CiNii)

    Articles in CiNii:1

    • System Analysis of a Hydrocarbon-Fueled RBCC Engine Applied to a TSTO Launch Vehicle (2014)
  • KODERA Masatoshi ID: 9000303987080

    JAXA (2013 from CiNii)

    Articles in CiNii:1

    • 214 Numerical Analysis of an Ethanol Fueled RBCC Engine (2013)
  • KODERA Masatoshi ID: 9000323299895

    Kakuda Space Center, Japan Aerospace Exploration Agency (2016 from CiNii)

    Articles in CiNii:1

    • Some Aspects on Hydrocarbon-fueled RBCC Engines for a TSTO Launch Vehicle (2016)
  • KODERA Masatoshi ID: 9000399851246

    Research and Development Directorate, Japan Aerospace Exploration Agency (2019 from CiNii)

    Articles in CiNii:1

    • Arrangement of Rocket Engine Location in a Combined Cycle Engine (2019)
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