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 (15):
Tsuyoshi Oishi, Mitsuru Tamari, Takashi Sakurai. Experimental Investigation of a Swirling-Oxidizer-Flow-Type Hybrid Rocket Engine Using Low-Melting-Point Thermoplastic Fuel and Oxygen. Aerospace. 2023. 10. 8. 713-713
Takashi Sakurai, Takehiro Sekiguchi, Sora Inoue. Evaluation of Pressure Gain and Turbine Inlet Conditions in a Pulse Combustion Gas Turbine. Volume 3B: Combustion, Fuels, and Emissions. 2022
Takashi Sakurai, Shunsuke Nakamura, Takehiro Sekiguchi, Sora Inoue. Theoretical Performance of Gas Turbines Operating with Pressure-Gain Combustion. JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 2022. 70. 6. 215-226