Rchr
J-GLOBAL ID：200901089880702873   Update date: Sep. 20, 2022

Sunami Tetsuji

スナミ テツジ | Sunami Tetsuji
Affiliation and department：
Japan Aerospace Exploration Agency Office of Space Flight and Operations Kakuda Space Center, Combined Engine Research Group, High Enthalpy Shock Tunnel Section

About Japan Aerospace Exploration Agency Office of Space Flight and Operations Kakuda Space Center, Combined Engine Research Group, High Enthalpy Shock Tunnel Section


Job title： Associate senior researcher
Research field  (1)： Aerospace engineering
Research keywords  (24)： 飛行実験 ,  宇宙航空機 ,  極超音速流 ,  不始動 ,  インレット ,  エンジン制御 ,  乱流制御 ,  縦渦 ,  乱流燃焼 ,  乱流混合 ,  超音速燃焼 ,  超音速混合 ,  スクラムジェット ,  Hypersonic Flow ,  Unstart ,  Inlet ,  Engine Control ,  Turbulence Control ,  Streamwise Vortex ,  Turbulent Combustion ,  Turbulent Mixing ,  Supersonic Combustion ,  Supersonic Mixing ,  Scramjet
Research theme for competitive and other funds  (5)：
  • 2009 - 2014 HyperMixer Scramjet Engine for Wide Flight Mach Number Range
  • 2002 - 2007 飛行マッハ数8~15の高速域スクラムジェットエンジンの研究
  • 1995 - 2007 超音速混合燃焼制御の研究
  • 1995 - 2002 飛行マッハ数4~8の低・中速域スクラムジェットエンジン作動特性の研究
  • 1. Control of Supersonic Mixing and Supersonic Combustion 2. Research of Scramjet Engine
Papers (41)：
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MISC (42)：
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Patents (2)：
  • 境界層剥離制御装置と燃料噴射器および制御方法
  • スクラムジェット燃焼器およびその制御法
Lectures and oral presentations  (16)：
  • Numerical Investigation on a Detonation Wave System in a HyperMixer Scramjet Combustor
    (Scramjet Symposium Munich 2012 2012)
  • Research Activities on the HyperMixer Scramjet Engine for Wide Flight Mach Number Range
    (Scramjet Symposium Munich 2012 2012)
  • On the Flameholding Flowfields with the HyperMixer Fuel Injector in Scramjet Combustors
    (Annual meeting of North-Branch of Japan Society for Aeronautical and Space Sciences 2012)
  • Combustion Characteristics of Hyper-Mixer Injectors for Scramjet Engine - Effects of the Aero-Ramp Applied to the Ramp-Wedge Type Injector -
    (47th Annual meeting of Tohoku-Branch of th Japan Society of Mechanical Engineers 2012)
  • On the Processes of Ignition and Flameholding in a Scramjet Combustor with the HyperMixer Fuel Injector
    (49th Combustion Symposium Japan 2011)
ｍore...
Works (3)：
  • Scramjet Combustion
    2000 - 2003
  • Study on Strut Injectors with Streamwise Vortices Generation for Scramjet Combustion
    2002 -
  • Control of Supersonic Mixing and Combustion for Scramjet Engine
    2001 -
Education (4)：
  • - 1995 Osaka Prefecture University
  • - 1995 Osaka Prefecture University Graduate School, Division of Engineering Aeronautics
  • - 1990 Osaka Prefecture University School of Engineering
  • - 1990 Osaka Prefecture University Faculty of Engineering Aeronautics
Professional career (1)：
  • Doctor of Engineering (Osaka Prefecture University)
Work history (7)：
  • 2003 - - 宇宙航空研究開発機構 主任研究員
  • 2003 - - Associate Senior Researcher, Japan Aerospace Exploration Agency
  • 2001 - 2002 年 ドイツ航空宇宙センター(DLR Lampoldshausen)客員研究員
  • 2001 - 2002 Visiting Reearcher, German Aerospace Center (DLR Lampoldshausen)
  • 2001 - 独立行政法人 航空宇宙技術研究所 主任研究員
Show all
Awards (2)：
  • 2006 - The Japan Society for Aeronautical and Space Sciences Ronbun-Prize Experiments of Supersonic Mixing and combustion Enhancement Using Alternating-Wedge Strut: Part-1 - Effects of Supersonic Streamwise Vortices in a Scramjet Combustor
  • 1999 - Japan Society of Fluid Mechanics Ryumon-Prize Breakdown Proceses of Supersonic Streamwise Vortices in Spanwise-Row Configurations
Association Membership(s) (7)：
国際衝撃波学会 ,  日本流体力学会 ,  日本航空宇宙学会 ,  米国航空宇宙学会 ,  The Japan Society for Aeronautical and Space Sciences ,  The American Institute of Aeronautics and Astronautics ,  Japan Society of Fluid Mechanics
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