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曲がり管内の流れ
https://jaxa.repo.nii.ac.jp/records/43198
https://jaxa.repo.nii.ac.jp/records/431989e003794-5f3e-40b3-b607-6a905a3aaa2e
名前 / ファイル | ライセンス | アクション |
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nalsp0005018.pdf (1.4 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 | 曲がり管内の流れ | |||||
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 | Computational Stud of Flow in Curved Pipes with Circular-Section | |||||
著者 |
白山, 晋
× 白山, 晋× 河村, 哲也× 桑原, 邦郎× Shirayama, Susumu× Kawamura, Tetsuya× Kuwahara, Kunio |
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著者所属 | ||||||
東京大学工学部大学院 | ||||||
著者所属 | ||||||
東京大学工学部 | ||||||
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-5 巻 5, p. 139-146, 発行日 1985-11 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | By solving the incompressible Navier-Stokes equations the flow field is calculated in a circular-sectioned pipe with a straight inlet or gradually enlarged inlet in the higher Dean number. With the straight inlet, a secondary flow of cross-stream planes was obtained and with the higher Dean number some different flow patterns were obtained. With the gradually enlarged inlet, the difference of flow patterns corresponding to Reynolds number could be simulated. | |||||
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: NALSP0005018 | |||||
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 |