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

Sunami Tetsuji

スナミ テツジ | Sunami Tetsuji
Affiliation and department:
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)
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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
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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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