Rchr
J-GLOBAL ID:201801001684052866   Update date: Feb. 01, 2024

Sakurai Takashi

サクライ タカシ | Sakurai Takashi
Affiliation and department:
Job title: 准教授
Homepage URL  (1): https://www.sd.tmu.ac.jp/RDstaff/data/sa/660.html
Research field  (1): Aerospace engineering
Research keywords  (6): Hybrid rocket propulsion ,  Hydrogen Combustion ,  Detonation ,  Gas Turbine Combustor ,  Combustion ,  Aerospace Propulsion
Research theme for competitive and other funds  (5):
  • 2021 - 2024 圧力増大燃焼で作動する高効率ガスタービンの実証研究
  • 2016 - 2019 Engine Performance of Swirling-Injection End-Burning Hybrid Rocket Engine using paraffin-WAX Fuels
  • 2014 - 2016 High intensity, clean combustion for liquid fuel combustor for micro gas turbine by using porous material injector
  • 2009 - 2010 Development of a Pulse Detonation Combustor for a Several kW-class Micro Gas Turbine
  • 2007 - 2009 Development of C_3H_8-fueled Ultra-micro Combustors with High Space Heating Rates for UMGT
Papers (14):
more...
Books (1):
  • Chemical Rocket Propulsion
    Springer 2017 ISBN:9783319277486
Lectures and oral presentations  (40):
  • Performance characteristics of miniature gas turbine with a pulse combustor
    (Proceedings of ISABE 2022, ISABE2021-061 2022)
  • パルス燃焼ガスタービンにおける燃焼圧力の評価および性能への影響
    (第61回航空原動機・宇宙推進講演会,JSASS-2022-0004-1A05,2022.)
  • Unsteady Heat Transfer Analysis and Experimental Evaluation of LOX Regenerative-cooling Nozzle for SOFT Hybrid Rocket Engines
    (33rd ISTS, 2022-o-1-17, 2022.)
  • Performance Evaluation of Swirling-Oxidizer-Flow-Type Hybrid Rocket Engine using Low Viscosity Low-Melting-Point Thermoplastic Fuel
    (33rd ISTS, 2022-o-1-12, 2022.)
  • 水素マイクロ拡散火炎を棚田状に配置したバーナの燃焼特性
    (第59回燃焼シンポジウム,B111,2021.)
more...
Awards (1):
  • 2010/10 - 日本航空宇宙学会 第19回(平成21年度)航空宇宙学会奨励賞 パルスデトネーションエンジンの安定作動に関するパージ空気の噴射量および分布の影響
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