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非構造格子法を用いた航空機高揚力装置周りの流れ場解析の精度検証
https://jaxa.repo.nii.ac.jp/records/6453
https://jaxa.repo.nii.ac.jp/records/6453a29180fc-2a6b-4928-8ba1-e890f97e7b04
名前 / ファイル | ライセンス | アクション |
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48469013.pdf (1.6 MB)
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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 | 非構造格子法を用いた航空機高揚力装置周りの流れ場解析の精度検証 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 高揚力構造 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 流れ場解析 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 精度 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 非構造格子 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 信頼性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 剥離流 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 境界層剥離 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 空力最適化 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | high lift configuration | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | flow analysis | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | CFD | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | accuracy | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | unstructured grid | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reliability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | separated flow | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | boundary layer separation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | aerodynamic optimization | |||||
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 | Validation of flow analysis on high-lift configurations by unstructured mesh method | |||||
著者 |
村山, 光宏
× 村山, 光宏× 山本, 一臣× Murayama, Mitsuhiro× Yamamoto, Kazuomi |
|||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
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: 航空宇宙数値シミュレーション技術シンポジウム2004論文集 en : JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2004 巻 JAXA-SP-04-012, p. 82-86, 発行日 2005-03-25 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this paper, flow computations around a 3D high-lift configuration with three-element (slat-main-flap) wing were performed on structured and unstructured meshes. The results were used to analyze and improve the accuracy and reliability of the aerodynamic analyses for high-lift system. Computed lift and drag coefficients both on structured and unstructured meshes showed good agreement with the experimental data. In the computations, it was also shown that further mesh refinement should be used to improve the resolution for slat wake, wing tip, and trailing edge for more accurate prediction by detail comparison with wind tunnel test data and computational data. | |||||
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: AA0048469013 | |||||
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-04-012 |