Design and Evaluation of a Multi-point Iriduim Thermocouple Rake to Measure High Temperature Combustion Gas at over 1900℃

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概要

• 論文の詳細を見る
• 1997-03-01

著者

• Tamaru Takashi

  National Aerospace Laboratory

• SHIMODAIRA Kazuo

  National Aerospace Laboratory

• KUROSAWA Youji

  National Aerospace Laboratory

関連論文

• Report on Organized Sessions
• 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
• 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)

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