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SLAUスキームの低Re数流れ場における検証
https://jaxa.repo.nii.ac.jp/records/4904
https://jaxa.repo.nii.ac.jp/records/4904eeaf7d41-7e6a-419c-933f-b7cf7b8322c3
名前 / ファイル | ライセンス | アクション |
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64672006.pdf (987.9 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 | SLAUスキームの低Re数流れ場における検証 | |||||
言語 | ||||||
言語 | jpn | |||||
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 SLAU Scheme in Low Reynolds Number Flows | |||||
著者 |
田辺, 安忠
× 田辺, 安忠× 齊藤, 茂× 菅原, 瑛明× Tanabe, Yasutada× Saito, Shigeru× Sugawara, Hideaki |
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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運航・安全技術チーム | ||||||
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運航・安全技術チーム | ||||||
著者所属 | ||||||
菱友システムズ | ||||||
著者所属(英) | ||||||
en | ||||||
Operation and Safety Technology Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Operation and Safety Technology Team, Aviation Program Group, Japan Aerospace Exploration Agency (JAXA)(APG) | ||||||
著者所属(英) | ||||||
en | ||||||
Ryoyu Systems | ||||||
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41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2009論文集 en : JAXA Special Publication: Proceedings fo 41st Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2009 巻 JAXA-SP-09-011, 発行日 2010-02-26 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 平成21年6月18-19日. 宇宙航空研究開発機構調布航空宇宙センター | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 18 June-19 June, 2009, Japan Aerospace Exploration Agency | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A CFD code "rFlow" based on the overlapping grids method was developed. An all speed numerical scheme SLAU combined with a fourth order MUSCL-type reconstruction is used to achieve high spatial resolutions. Dual-time stepping method is used for efficient implicit unsteady flow calculations. This paper reports on the two-dimensional results of the validations in the low speed and low Reynolds number flowfields. The obtained flowfield around a cylinder shows good agreement with experimental results where the size of the wake flow bubble and Karman vortex shedding are compared. Also, the calculated lift coefficients of a wing section are agreeable with the experimental data even at high incident angles. | |||||
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: AA0064672006 | |||||
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-09-011 |