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二次元翼まわりの非圧縮性流れ
https://jaxa.repo.nii.ac.jp/records/43207
https://jaxa.repo.nii.ac.jp/records/4320781db4f8f-621d-4e8b-8efb-0906ce6112e9
名前 / ファイル | ライセンス | アクション |
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nalsp0005027.pdf (1.0 MB)
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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 | 二次元翼まわりの非圧縮性流れ | |||||
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 | Two-Dimensional Incompressible Flows around an Airfoil at Several Attack Angles | |||||
著者 |
中村, 佳朗
× 中村, 佳朗× 石黒, 満津夫× 保原, 充× Nakamura, Yoshiaki× Ishiguro, Mitsuo× Yasuhara, Michiru |
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著者所属 | ||||||
名古屋大学工学部 | ||||||
著者所属 | ||||||
名古屋大学工学部 | ||||||
著者所属 | ||||||
名古屋大学工学部 | ||||||
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-5 巻 5, p. 217-228, 発行日 1985-11 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Two-dimensional incompressible flows were numerically solved for two problems, using stream function-vorticity formulation with second-order accuracy in space and first-order accuracy in time. First, we solved flows around an NACA0012 airfoil at a Reynolds number of 10000 at angles of attack up to 15. Separation and generation of vortices were well simulated. Secondly, we applied this method to a flow around a circulation controlled airfoil, where a jet is emitted along the airfoil surface. The result indicates that outside the jet near the trailing edge the flow is deflected downward, and that vortices play a significant role at the initial stage. | |||||
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: NALSP0005027 | |||||
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-5 |