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翼列空力解析プラットフォームの開発

翼列空力解析プラットフォームの開発
Digital文書・図像類
西澤, 敏雄, 野崎, 理, 中村, 孝, 福田, 正大, 加藤, 昭史, 助村, 俊一, 川崎, 琢治, Nishizawa, Toshio, Nozaki, Osamu, Nakamura, Takashi, Fukuda, Masahiro, Kato, Akifumi, Sukemura, Shuniti, Kawasaki, Takuji航空宇宙技術研究所2000-12航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory46p.231-236
Other Libraries in Japan
  • Subject Heading...的形状 計算流体力学 CFD blade row aerodynamic design turbomachi...
  • Note (General)...) platform for blade rows, which realiz......ic profiles of blade rows, computed dat...... the design of blade row. In this paper......wo-dimensional blade rows. A flow solver for a multi-s...
  • Alternative TitleOn development of CFD platform for blade rows

高速機械式翼列曲げ振動加振装置とその特性

高速機械式翼列曲げ振動加振装置とその特性
Digital文書・図像類
生沼, 秀司, 小林, 紘, Oinuma, Hideshi, Kobayashi, Hiroshi航空宇宙技術研究所1992-07航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory1170p.1-18
Other Libraries in Japan
  • Subject Heading...動試験 jet engine blade row flutter bending mode oscillat...
  • Note (General)... in an annular blade row in the bending......urbomachinery. Blade row oscillation te......ng the annular blade row at a constant ......of the annular blade row can be controllably-oscillate...
  • Alternative Title...ing an annular blade row in the bending mode

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