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Planform Dependency on Airfoil Design Results for Supersonic Wing in Supersonic and Transonic
https://jaxa.repo.nii.ac.jp/records/22740
https://jaxa.repo.nii.ac.jp/records/227407c40834c-5333-4f13-8b57-8ea03d088d00
Item type | 学術雑誌論文 / Journal Article(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2016-05-31 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Planform Dependency on Airfoil Design Results for Supersonic Wing in Supersonic and Transonic | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Supersonic Wing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Multi-Point Design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Airfoil Design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Knowledge Discovery | |||||
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 | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
著者 |
岸, 祐希
× 岸, 祐希× 金崎, 雅博× 牧野, 好和× 松島, 紀佐× Kishi, Yuki× Kanazaki, Masahiro× Makino, Yoshikazu× Matsushima, Kisa |
|||||
著者所属 | ||||||
首都大学東京 | ||||||
著者所属 | ||||||
首都大学東京 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空技術部門 (JAXA) | ||||||
著者所属 | ||||||
富山大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University | ||||||
著者所属(英) | ||||||
en | ||||||
Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
University of Toyama | ||||||
出版者(英) | ||||||
出版者 | Scientific Research Publishing | |||||
書誌情報 |
en : Journal of Flow Control, Measurement & Visualization 巻 4, 号 1, p. 38-48, 発行日 2016-01-29 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this study, the wing design problem for different planforms for supersonic transport (SST) under supersonic and transonic cruise conditions is discussed to obtain knowledge of the supersonic air-foil from the viewpoint of wing planform dependency. Two types of planforms were considered-a cranked arrow wing with a high sweep-back angle and a tapered wing with a low sweep- back angle. The optimum airfoils of these planforms were designed by efficient global optimization, which combined the evolutionary algorithm with the Kriging surrogate model. To acquire design knowledge, the functional analysis of variance was applied to the solution space and the design space. The design results show that the optimum airfoil and the contribution ratios of design variables for the airfoils of the two planform are different. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 2329-3322 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.4236/jfcmv.2016.41004 | |||||
関連名称 | info:doi/10.4236/jfcmv.2016.41004 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1620055000 |