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ダイナミック・ストールの数値解析
https://jaxa.repo.nii.ac.jp/records/43218
https://jaxa.repo.nii.ac.jp/records/43218f49488b9-2f38-48ca-8ee5-c7546056db75
名前 / ファイル | ライセンス | アクション |
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nalsp0007002.pdf (576.6 kB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | ダイナミック・ストールの数値解析 | |||||
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_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Computation of Dynamic Stall of NACA0012 Airfoil by Block Pentadiagonal Matrix Scheme | |||||
著者 |
信太, 良文
× 信太, 良文× 桑原, 邦郎× Shida, Yoshifumi× Kawahara, Kunio |
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著者所属 | ||||||
東京大学 | ||||||
著者所属 | ||||||
宇宙科学研究所 | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所特別資料 en : Special Publication of National Aerospace Laboratory SP-7 巻 7, p. 13-24, 発行日 1986-12 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | The flow field around an oscillating NACA0012 airfoil in pitch at 0.25 chord is analyzed by solving the two-dimensional compressible Navier-Stokes equations. A block pentadiagonal matrix scheme based on the approximate factorization method is adopted. Two meshes, 161 by 40 and 213 by 80, are used. With the coarse mesh, lift stall is cap-tured. With the fine mesh, not only lift stall but also the restoration process of the lift coefficient in the downstroke is captured. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALSP0007002 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL SP-7 |