Hydrogen Combustion Wind Tunnel Test of 1700℃ Class Turbine Cooling Blades
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概要
- 論文の詳細を見る
- 2001-03-01
著者
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Koga Akinori
Power And Industrial Systems R&d Center Toshiba Corporation
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Suga Takeo
Power And Industrial Systems R&d Center Toshiba Corporation
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Matsuda Hisashi
Power And Industrial Systems R&d Center Toshiba Corporation
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ITOH Shoko
Power and Industrial Systems R&D Center, Toshiba Corporation
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KAWAGISHI Hiroyuki
Power and Industrial Systems R&D Center, Toshiba Corporation
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OKAMURA Takanari
Power and Industrial Systems R&D Center, Toshiba Corporation
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Ito Shoko
Power And Industrial Systems R&d Center Toshiba Corporation
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Okamura Takanari
Power And Industrial Systems R&d Center Toshiba Corporation
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Kawagishi Hiroyuki
Power And Industrial Systems R&d Center Toshiba Corporation
関連論文
- Pressure Loss Characteristics in Rotating Coolant Passages of Gas Turbine
- F315 PRESSURE LOSS CHARACTERISTICS IN ROTATING COOLANT PASSAGES OF GAS TURBINE(Fluid machinary-3)
- Hydrogen Combustion Wind Tunnel Test of 1700℃ Class Turbine Cooling Blades
- Heat Transfer Measurements on a Turbine Nozzle Surface using Liquid Crystals
- TS-47 Heat Transfer Measurements on a Turbine Nozzle Using Liquid Crystals(Session C-1 Heat Transfer 1)
- TS-46 Development of Hydrogen-Oxygen Combustion Turbine Cooling Blades in WE-NET Project(Session C-1 Heat Transfer 1)