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高効率手法を適用した静粛超音速航空機の多分野融合最適設計
http://hdl.handle.net/10748/7783
http://hdl.handle.net/10748/7783b5770b5a-d3b0-4b90-a346-0d4a027ba62b
名前 / ファイル | ライセンス | アクション |
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10172-001.pdf (2.6 MB)
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Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2016-07-04 | |||||
タイトル | ||||||
タイトル | 高効率手法を適用した静粛超音速航空機の多分野融合最適設計 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Multidisciplinary Design | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Supersonic Wing | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Global Optimization | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Design Knowledge | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
著者 |
瀬戸, 直人
× 瀬戸, 直人× 牧野, 好和× 高戸谷, 健× 金崎, 雅博 |
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著者別名 |
Seto, Naoto
× Seto, Naoto× Makino, Yoshikazu× Takatoya, Takeshi× Kanazaki, Masahiro |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | In this study, high efficient design tool is developed with several informatics approaches for Multidisciplinary Design Optimization (MDO) and knowledge discovery of supersonic wing design. In this design, Multi-Objective Genetic Algorithm (MOGA) is applied as an optimizer, while Kriging model is also used to reduce computational cost. To obtain the information of the design space, functional ANalysis Of VAriance (ANOVA) and Parallel Coordinate Plot (PCP) is applied. For Kriging model construction, 107 sample points are evaluated. This tool is applied to the multidisciplinary design problem of supersonic wing. The objective functions are to maximize lift to drag ratio and to minimize sonic boom intensity at supersonic cruise, and to minimize wing weight. According to the results, there are trade-off relationships among three objective functions. The ANOVA results indicate that the cambers of the wing section at the root and the kink have an influence on the lift to drag ratio, the inner wing sweep back angle affects the sonic boom intensity, and the camber of wing section at the kink and aspect ratio affect the wing weight. The design space information could be visualized quantitatively from the sampling results with PCP technique. Since the design space exploration using MOGA is carried out based on Kriging surrogate models, the proposed MDO process is effective in terms of computational cost. | |||||
書誌情報 |
日本航空宇宙学会論文集 巻 59, 号 686, p. 61-69, 発行日 2011-03 |
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ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 13446460 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11307372 | |||||
DOI | ||||||
関連タイプ | isIdenticalTo | |||||
識別子タイプ | DOI | |||||
関連識別子 | http://doi.org/10.2322/jjsass.59.61 | |||||
権利 | ||||||
権利情報 | 社団法人日本航空宇宙学会 | |||||
著者版フラグ | ||||||
出版タイプ | VoR | |||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
その他のタイトル | ||||||
その他のタイトル | Multidisciplinary Design Optimization of Silent Supersonic Transport with Efficient Optimization Techniques | |||||
出版者 | ||||||
出版者 | 日本航空宇宙学会 | |||||
資源タイプ | ||||||
内容記述タイプ | Other | |||||
内容記述 | postprint |