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Studies on Aero-Thermal Performances of Leakage Flows lnjection from the Endwall Slot in Linear Cascade of High-Pressure Turbine

Studies on Aero-Thermal Performances of Leakage Flows lnjection from the Endwall Slot in Linear Cascade of High-Pressure Turbine
Digital博士論文障害者向け資料あり
Wan, Aizon Bin W Ghopa岩手大学2013-09-01
National Diet Library
  • Subject Heading...ansient method pressure loss slot orientation slot positio...
  • Note (General)... and the total pressure loss coefficient, Cpt as well as t...

Studies on Aero-Thermal Performances of Leakage Flows lnjection from the Endwall Slot in Linear Cascade of High-Pressure Turbine

Studies on Aero-Thermal Performances of Leakage Flows lnjection from the Endwall Slot in Linear Cascade of High-Pressure Turbine
Digital博士論文障害者向け資料あり
Wan, Aizon Bin W Ghopa岩手大学2013
National Diet Library
  • Subject Heading...ansient method pressure loss slot orientation slot positio...
  • Note (General)... and the total pressure loss coefficient, Cpt as well as t...

Studies on Aero-Thermal Performances of Leakage Flows lnjection from the Endwall Slot in Linear Cascade of High-Pressure Turbine

Studies on Aero-Thermal Performances of Leakage Flows lnjection from the Endwall Slot in Linear Cascade of High-Pressure Turbine
Digital博士論文
Wan, Aizon Bin W Ghopa岩手大学2013p.1-154
Available onlineOther Libraries in Japan
  • Subject Heading...ansient method pressure loss slot orientation slot positio...
  • Note (General)... and the total pressure loss coefficient, Cpt as well as t...

熱交換器要素の高性能化に関する実験的研究

熱交換器要素の高性能化に関する実験的研究
Digital文書・図像類
稲岡, 恭二, 千田, 衞同志社大学エネルギー変換研究センター2004-07-17研究成果報告書(2003年度)p.51-56
Available onlineOther Libraries in Japan
  • Summary, etc....h the smallest pressure loss penalty. Especially, an optim...
  • Subject Heading...ger Spring fin Pressure loss Thermal efficiency Unsteady h...

極超音速機用水素燃料ターボラム燃焼器模型の試験結果

極超音速機用水素燃料ターボラム燃焼器模型の試験結果
Digital文書・図像類
田丸, 卓, 下平, 一雄, 斎藤, 隆, 山田, 秀志, Tamaru, Takashi, Shimodaira, Kazuo, Saito, Takashi, Yamada, Hideshi航空宇宙技術研究所1993-03航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1193p.1-17
Other Libraries in Japan
  • Subject Heading...combustion gas pressure loss
  • Note (General)...alues of total pressure loss were obtained by measurements...

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