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タービン諸特性(回転部重量，翼応力，動翼共振回避，Thomas Force)を考慮したロケットターボポンプ用タービンの多目的最適化

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瀧田, 純也, 福田, 太郎, 宇山, 遼一, 船﨑, 健一, 内海, 政春, Takida, Junya, Fukuda, Taro, Uyama, Ryoichi, Funazaki, Kenichi, Uchiumi, Masaharu宇宙航空研究開発機構(JAXA)2013-01-31宇宙航空研究開発機構研究開発資料 = JAXA Research and Development MemorandumJAXA-RM-12-007p.1-11

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Subject HeadingMulti-Objective Genetic Algorithm (MOGA) Parameter Design Rocket Turbo...
Note (General)...ter Design and Multi-Objective Genetic Algorithm (MOGA). In this paper, by increasing...

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