Sakurai Takashi 櫻井毅司

… Alternative Names

SAKURAI Takashi 櫻井毅司

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Researcher Number	10433179
Other IDs
Affiliation (Current)	2025: 東京都立大学, システムデザイン研究科, 准教授
Affiliation (based on the past Project Information) *help	2025: 東京都立大学, システムデザイン研究科, 准教授 2021 – 2023: 東京都立大学, システムデザイン研究科, 准教授 2014 – 2018: 首都大学東京, システムデザイン研究科, 准教授 2009 – 2010: Tokyo Metropolitan University, 大学院・システムデザイン研究科, 助教 2007 – 2010: 首都大学東京, システムデザイン研究科, 助教
Review Section/Research Field	Principal Investigator Aerospace engineering / Basic Section 24010:Aerospace engineering-related Except Principal Investigator Aerospace engineering
Keywords	Principal Investigator ハイブリッドロケット / 超小型ガスタービン / 超臨界圧力 / 再生冷却ノズル / サイクル解析 / 熱効率 / ガスタービン / パルス燃焼 / 圧力増大燃焼 / 旋回流 … More / 端面燃焼 / ロケットエンジン / 低融点燃料 / 燃料後退速度 / LOX / WAX燃料 / 旋回流端面燃焼 / 多孔質体 / 灯油燃料 / 予蒸発予混合燃焼 / 多孔質燃焼 / 超小型燃焼器 / 燃焼工学 / 航空宇宙工学 / 航空宇宙推進 / PDE / デトネーション / パルスデトネーション燃焼器 … More Except Principal Investigator 燃焼器 / 超小型 / プロパン / Flat-flame / 超小型燃焼器 / Flat-flameプロパン / 高負荷燃焼 / ウルトラマイクロガスタービン Less

低融点燃料を用いた再生冷却ハイブリッドロケットエンジンにおける超臨界圧力の影響Principal Investigator
- Principal Investigator
  
  櫻井毅司
- Project Period (FY)
  2025 – 2028
- Research Category
  
  Grant-in-Aid for Scientific Research (B)
- Review Section
  
  Basic Section 24010:Aerospace engineering-related
- Research Institution
  Tokyo Metropolitan University
Research on gas turbine using pressure gain combustion for improving thermal efficiencyPrincipal Investigator
- Principal Investigator
  
  Sakurai Takashi
- Project Period (FY)
  2021 – 2023
- Research Category
  
  Grant-in-Aid for Scientific Research (C)
- Review Section
  
  Basic Section 24010:Aerospace engineering-related
- Research Institution
  Tokyo Metropolitan University
Engine Performance of Swirling-Injection End-Burning Hybrid Rocket Engine using paraffin-WAX FuelsPrincipal Investigator
- Principal Investigator
  
  Sakurai Takashi
- Project Period (FY)
  2016 – 2018
- Research Category
  
  Grant-in-Aid for Scientific Research (C)
- Research Field
  
  Aerospace engineering
- Research Institution
  Tokyo Metropolitan University
High intensity, clean combustion for liquid fuel combustor for micro gas turbine by using porous material injectorPrincipal Investigator
- Principal Investigator
  
  Sakurai Takashi
- Project Period (FY)
  2014 – 2015
- Research Category
  
  Grant-in-Aid for Young Scientists (B)
- Research Field
  
  Aerospace engineering
- Research Institution
  Tokyo Metropolitan University
Development of a Pulse Detonation Combustor for a Several kW-class Micro Gas TurbinePrincipal Investigator
- Principal Investigator
  
  SAKURAI Takashi
- Project Period (FY)
  2009 – 2010
- Research Category
  
  Grant-in-Aid for Young Scientists (B)
- Research Field
  
  Aerospace engineering
- Research Institution
  Tokyo Metropolitan University
Development of C_3H_8-fueled Ultra-micro Combustors with High Space Heating Rates for UMGT
- Principal Investigator
  
  YUASA Saburo
- Project Period (FY)
  2007 – 2009
- Research Category
  
  Grant-in-Aid for Scientific Research (B)
- Research Field
  
  Aerospace engineering
- Research Institution
  Tokyo Metropolitan University

All 2024 2023 2022 2021 2018 2017 2016 2015 2010 2009 2008 2007 Other

All Journal Article Presentation

[Journal Article] Evaluation of Pressure Gain and Turbine Inlet Conditions in a Pulse Combustion Gas Turbine2022
- Author(s)
  Sakurai Takashi、Sekiguchi Takehiro、Inoue Sora
- Journal Title
  
  Proceedings of ASME Turbo Expo 2022
  
  Volume: -
- DOI
  10.1115/gt2022-83528
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-21K04481
[Journal Article] Theoretical Performance of Gas Turbines Operating with Pressure-Gain Combustion2022
- Author(s)
  櫻井毅司，中村駿介，関口武央，井上素良
- Journal Title
  
  JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
  
  Volume: 70 Issue: 6 Pages: 215-226
- DOI
  10.2322/jjsass.70.215
- ISSN
  1344-6460, 2432-3691
- Language
  Japanese
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-21K04481
[Journal Article] Heat Loss Reduction and Hydrocarbon Combustion in Ultra-micro Combustors for Ultra-micro Gas Turbines2009
- Author(s)
  Sakurai, T., Yuasa, S., Honda, T., Shimotori, S.
- Journal Title
  
  Proc. Combust. Inst. Vol.32
  
  Pages: 3067-3073
- NAID
  120006627237
- Data Source
  KAKENHI-PROJECT-19360383
[Journal Article] Heat Loss Reduction and Hydrocarbon Combustion in Ultra-micro Combustors for UMGT2009
- Author(s)
  Sakurai, T.
- Journal Title
  
  Proceedings of the Combustion Institute 32
  
  Pages: 3067-3073
- NAID
  120006627237
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-19360383
[Journal Article] Development of Engineering-models of H2-fueled and C3H8-fueled Ultra-micro Combustors for UMGT2009
- Author(s)
  Yuasa, S., Sakurai, T., Shimotori, S., Honda, T., Fueda, T.
- Journal Title
  
  Proc. 19th International Symposium on Airbreathing Engines
  
  Pages: 2009-1310
- Data Source
  KAKENHI-PROJECT-19360383
[Journal Article] Issues for Developing Ultra-micro Combustors for UMGT : Heat Loss, Combustion Method and Fuel2007
- Author(s)
  Yuasa, S., Sakurai, T., Shimotori, S., Wong, S.F.
- Journal Title
  
  Proc. 18th International Symposium on Airbreathing Engines
  
  Pages: 2007-1167
- Data Source
  KAKENHI-PROJECT-19360383
[Journal Article] Concept and Experiment of a Propane-fueled Flat-flame Ultra-Micro Combustor for UMGT2007
- Author(s)
  Sakurai, T., Yuasa, S., Honda, T.
- Journal Title
  
  Proc. International Gas Turbine Congress 2007
- NAID
  120006660089
- Data Source
  KAKENHI-PROJECT-19360383
[Journal Article] Concept and Experiment of a Propane-Fueled Flat-Flame Ultra-Micro Combustor for UMGT2007
- Author(s)
  SAKURAI Takashi
- Journal Title
  
  Proceeding of the International Gas Turbine Congress 2007 Tokyo IGTC2007 Tokyo TS-147(CD-ROM)
- NAID
  120006660089
- Peer Reviewed
- Data Source
  KAKENHI-PROJECT-19360383
[Presentation] アクティブパルス燃焼器における水素－空気乱流火炎の伝播速度と燃焼圧力2024
- Author(s)
  井上素良，櫻井毅司
- Organizer
  第63回航空原動機・宇宙推進講演会
- Data Source
  KAKENHI-PROJECT-21K04481
[Presentation] Cycle Analysis of Small Gas Turbine with Pressure Gain Combustion and Experiment of Miniature Engine2023
- Author(s)
  Sakurai, T., Inoue, S., Sekiguchi, T., Sato, A.
- Organizer
  International Gas Turbine Congress 2023
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-21K04481
[Presentation] Pressure gain combustionを適用するガスタービンのサイクル解析2023
- Author(s)
  井上素良，櫻井毅司
- Organizer
  第51回日本ガスタービン学会定期講演会
- Data Source
  KAKENHI-PROJECT-21K04481
[Presentation] Operating Condition of a Miniature Gas Turbine with a Pulse Combustor2023
- Author(s)
  Inoue, S., Sekiguchi, T., Sato, A., Sakurai, T.
- Organizer
  11th Asian Joint Conference on Propulsion and Power, AJCPP2023-084
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-21K04481
[Presentation] Evaluation of pressure gain and turbine inlet conditions in a pulse combustion gas turbine2022
- Author(s)
  Sakurai, T., Sekiguchi, T., Inoue, S.
- Organizer
  ASME Turbo Expo 2022
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-21K04481
[Presentation] Performance characteristics of miniature gas turbine with a pulse combustor2022
- Author(s)
  Sakurai, T., Nakamura, S., Sekiguchi, T., Inoue, S.
- Organizer
  Proceedings of ISABE 2022, ISABE2021-061
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-21K04481
[Presentation] パルス燃焼ガスタービンの運転特性2022
- Author(s)
  関口武央，井上素良，佐藤あすか，櫻井毅司
- Organizer
  第50回日本ガスタービン学会定期講演会，B-10
- Data Source
  KAKENHI-PROJECT-21K04481
[Presentation] 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2022
- Author(s)
  井上素良，関口武央，櫻井毅司
- Organizer
  第61回航空原動機・宇宙推進講演会
- Data Source
  KAKENHI-PROJECT-21K04481
[Presentation] パルス燃焼と定圧燃焼を組み合わせた圧力増大燃焼ガスタービンの性能評価2021
- Author(s)
  関口武央，中村駿介，櫻井毅司
- Organizer
  第49回日本ガスタービン学会定期講演会
- Data Source
  KAKENHI-PROJECT-21K04481
[Presentation] 低融点燃料を用いた旋回流端面燃焼型ハイブリッドロケットエンジンの燃焼挙動2018
- Author(s)
  斎藤和幸，松田彩夏，櫻井毅司
- Organizer
  第62回宇宙科学技術連合講演会
- Data Source
  KAKENHI-PROJECT-16K06889
[Presentation] Fuel Regression Behavior of Swirling-Injection End-Burning Hybrid Rocket Engine2018
- Author(s)
  Sakurai, T., Oishige, Y., Saito, K.
- Organizer
  15th ICFD
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-16K06889
[Presentation] Engine Performance of a Swirling-Injection End-Burning Hybrid Rocket Engine using LOX/Paraffin-based Fuel2017
- Author(s)
  Saito, K., Oishige, Y., Hayashi, D., Sakurai, T.
- Organizer
  30th ISTS
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-16K06889
[Presentation] Various studies on swirling-injection hybrid rocket engines2016
- Author(s)
  Sakurai, T., Tomizawa, T., Hayashi, D., Oishige, Y.
- Organizer
  13th ICFD
- Place of Presentation
  Sendai international center （宮城県仙台市）
- Year and Date
  2016-10-10
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-16K06889
[Presentation] Fuel Regression Behavior of a Swirling-Injection End-Burning Hybrid Rocket Engine using Paraffin-based Fuels2016
- Author(s)
  Oishige, Y., Hayashi, D., Sakurai, T.
- Organizer
  52nd AIAA Joint Propulsion Conference
- Place of Presentation
  Salt lake city (USA)
- Year and Date
  2016-07-25
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-16K06889
[Presentation] Development of a Prevaporized Combustor using a Porous Media for a Kerosene-fueled Micro Gas Turbine2015
- Author(s)
  Harada, R., Kobori, Y., Sakurai, T.
- Organizer
  International Gas Turbine Congress 2015
- Place of Presentation
  Toranomon Hills Forum，Toranomon,Tokyo
- Year and Date
  2015-11-15
- Int'l Joint Research
- Data Source
  KAKENHI-PROJECT-26820373
[Presentation] Development of a Hydrogen-fueled Pulse Detonation Combustor for 1 kW-class Micro Gas Turbine2010
- Author(s)
  Sakurai, T., Yuasa, S.
- Organizer
  46th AIAA Joint Propulsion Conference
- Place of Presentation
  Nashville Convention Center (Nashville, TN, USA)
- Year and Date
  2010-07-27
- Data Source
  KAKENHI-PROJECT-21760653
[Presentation] Combustion Characteristics of a Propane-fueled Combustor for a Several Hundred W-class Micro Gas Turbine2008
- Author(s)
  Sakurai, T.
- Organizer
  PowerMEMS十μEMS 2008
- Place of Presentation
  仙台
- Year and Date
  2008-11-10
- Data Source
  KAKENHI-PROJECT-19360383
[Presentation] Development of a Prevaporized Combustor using a Porous Media for a Kerosene-fueled Micro Gas turbine
- Author(s)
  Ryo Harada, Yuho Kobori, Takashi Sakurai
- Organizer
  International Gas Turbine Congress 2015
- Place of Presentation
  虎ノ門ヒルズ
- Year and Date
  2015-11-15 – 2015-11-20
- Data Source
  KAKENHI-PROJECT-26820373
[Presentation] 超小型ガスタービン用灯油燃料燃焼器への多孔質体を用いた予蒸発燃焼の検討
- Author(s)
  原田亮，櫻井毅司，湯浅三郎
- Organizer
  第42回日本ガスタービン学会定期講演会
- Place of Presentation
  熊本市国際交流会館
- Year and Date
  2014-10-22 – 2014-10-23
- Data Source
  KAKENHI-PROJECT-26820373

1. YUASA Saburo (60123147)

# of Collaborated Projects: 1 results

# of Collaborated Products: 4 results

Sakurai Takashi 櫻井 毅司

SAKURAI Takashi 櫻井 毅司

Research Projects

Research Products

Co-Researchers

低融点燃料を用いた再生冷却ハイブリッドロケットエンジンにおける超臨界圧力の影響Principal Investigator

Principal Investigator

Project Period (FY)

Research Category

Review Section

Research Institution

Research on gas turbine using pressure gain combustion for improving thermal efficiencyPrincipal Investigator

Principal Investigator

Project Period (FY)

Research Category

Review Section

Research Institution

Engine Performance of Swirling-Injection End-Burning Hybrid Rocket Engine using paraffin-WAX FuelsPrincipal Investigator

Principal Investigator

Project Period (FY)

Research Category

Research Field

Research Institution

High intensity, clean combustion for liquid fuel combustor for micro gas turbine by using porous material injectorPrincipal Investigator

Principal Investigator

Project Period (FY)

Research Category

Research Field

Research Institution

Development of a Pulse Detonation Combustor for a Several kW-class Micro Gas TurbinePrincipal Investigator

Principal Investigator

Project Period (FY)

Research Category

Research Field

Research Institution

Development of C_3H_8-fueled Ultra-micro Combustors with High Space Heating Rates for UMGT

Principal Investigator

Project Period (FY)

Research Category

Research Field

Research Institution

[Journal Article] Evaluation of Pressure Gain and Turbine Inlet Conditions in a Pulse Combustion Gas Turbine2022

Author(s)

Journal Title

DOI

Data Source

[Journal Article] Theoretical Performance of Gas Turbines Operating with Pressure-Gain Combustion2022

Author(s)

Journal Title

DOI

ISSN

Language

Data Source

[Journal Article] Heat Loss Reduction and Hydrocarbon Combustion in Ultra-micro Combustors for Ultra-micro Gas Turbines2009

Author(s)

Journal Title

NAID

Data Source

[Journal Article] Heat Loss Reduction and Hydrocarbon Combustion in Ultra-micro Combustors for UMGT2009

Author(s)

Journal Title

NAID

Data Source

[Journal Article] Development of Engineering-models of H2-fueled and C3H8-fueled Ultra-micro Combustors for UMGT2009

Author(s)

Journal Title

Data Source

[Journal Article] Issues for Developing Ultra-micro Combustors for UMGT : Heat Loss, Combustion Method and Fuel2007

Author(s)

Journal Title

Data Source

[Journal Article] Concept and Experiment of a Propane-fueled Flat-flame Ultra-Micro Combustor for UMGT2007

Author(s)

Journal Title

NAID

Data Source

[Journal Article] Concept and Experiment of a Propane-Fueled Flat-Flame Ultra-Micro Combustor for UMGT2007

Author(s)

Journal Title

NAID

Sakurai Takashi 櫻井毅司

SAKURAI Takashi 櫻井毅司