Hydrogen Combustion of a Het Mixing Type Ramjet Engine Combustor in High Temperature Air
スポンサーリンク
概要
- 論文の詳細を見る
- 1996-03-01
著者
-
Tamaru Takashi
National Aerospace Laboratory
-
Kitajima Junichi
Kawasaki Heavy Industries Ltd.
-
SHIMODAIRA Kazuo
National Aerospace Laboratory
-
Kinoshita Yasuhiro
Kawasaki Heavy Industries Ltd.
-
KUROSAWA Youji
National Aerospace Laboratory
関連論文
- NO_x Emissions Characteristics of a Methane Fueled Ram Combustor
- Measurement of the Fuel Distributions at Gas Turbine Burner Exit
- Report on Organized Sessions
- OS-503 Research of Mach 5 Ramjet Propulsion System(Organized Session 5: HYPR-HST/SST Propulsion System)
- On-Engine Testing of a Variable Geometry Lean-Premixed Combustor
- Perfomance of a Methane-Fuel Cooled Gutter Type Flame Holder for a Ramjet Engine Combustor
- An Eeperimental Study of an Airblast Fuel Nozzle
- Small and Medium Size Gas Turbines(Gas Turbine Technology in Japan)
- Hydrogen Combustion of a Het Mixing Type Ramjet Engine Combustor in High Temperature Air
- Design and Evaluation of a Multi-point Iriduim Thermocouple Rake to Measure High Temperature Combustion Gas at over 1900℃
- Effect of Temperature, Gas Velocity and Oxygen Concentration on Evaporation of Iridium
- ORGANIZED SESSION IV: NO_x ABATEMENT COMBUSTORS(Reports on Organized Sessions,1991 Yokohama International Gas Turbine Congress)
- Organized Session VI: Low Emission Combustors(Report on Organized Sessions,1995 Yokohama International Gas Turbine Congress)