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横流れを考慮した高揚力翼型展開形態の設計探査
https://jaxa.repo.nii.ac.jp/records/5618
https://jaxa.repo.nii.ac.jp/records/5618eba69d4d-cbaf-4be6-baf4-17bfec1d5107
名前 / ファイル | ライセンス | アクション |
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63742012.pdf (977.2 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 横流れを考慮した高揚力翼型展開形態の設計探査 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高揚力翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 翼型プロフィル | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | レイノルズ平均化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | ナビエ・ストークス方程式 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 航空機設計 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 複合領域設計最適化 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 遺伝的アルゴリズム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 前縁スラット | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | フラップ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 後退翼 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 分散解析 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high lift wing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | airfoil profile | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Reynolds averaging | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Navier-Stokes equation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aircraft design | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | multidisciplinary design optimization | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | genetic algorithm | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | leading edge slat | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flap | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | sweptback wing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | analysis of variance | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | High-lift wing design based on design exploration with considering cross-flow effect | |||||
著者 |
金崎, 雅博
× 金崎, 雅博× 今村, 太郎× Jeong, Shinkyu× 山本, 一臣× Kanazaki, Masahiro× Imamura, Taro× Jeong, Shinkyu× Yamamoto, Kazuomi |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 航空プログラムグループ | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 航空プログラムグループ | ||||||
著者所属 | ||||||
東北大学流体科学研究所 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 航空プログラムグループ | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Aviation Program Group | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Aviation Program Group | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Fluid Science, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Aviation Program Group | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料: 第39回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2007論文集 en : JAXA Special Publication: Proceedings of 39th Fluid Dynamics Conference/Aerospace Numerical Simulation Symposium 2007 巻 JAXA-SP-07-016, p. 68-74, 発行日 2008-02-29 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this paper, a multi-objective design exploration for a three-element airfoil which consists of a slat, main wing, and flap was carried out by paying attention to the span wise flow effect. Reynolds Averaged Navier-Stokes Solver (RANS) was used for the evaluation during the design process. To reduce computational time, '2.5-dimensional span wise calculation' was used. In this calculation, two same planes were arranged along span wise direction. They were diagonally arranged to represent the sweep angle and periodic boundary condition was used for the infinite span wise calculation. Kriging based Multi-Objective Genetic Algorithm (MOGA) and ANalysis Of VAriance (ANOVA) were used for the design exploration. The objective functions were defined as the maximization of lift coefficient at landing and near stall conditions simultaneously. In this study, 54 sample points were evaluated for the construction of the Kriging model. Based on present evaluation method, the span wise flow was observed and it has an influence on the separation on the flap. Through the design exploration process, the differences of the designed results between 2.5D and 2D evaluation were observed by visualizing the design space. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0063742012 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-07-016 |