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円筒容器内渦崩壊現象のフル三次元シミュレーション
https://jaxa.repo.nii.ac.jp/records/3248
https://jaxa.repo.nii.ac.jp/records/324865024fa1-f3c6-4f50-97a3-d9d1182ffa10
名前 / ファイル | ライセンス | アクション |
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AA1730011014.pdf (874.2 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2017-12-28 | |||||
タイトル | ||||||
タイトル | 円筒容器内渦崩壊現象のフル三次元シミュレーション | |||||
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 | Full 3D simulation of vortex breakdown in closed cylinder with rotating bottom | |||||
著者 |
山田, 健翔
× 山田, 健翔× 鈴木, 宏二郎× Yamada, Kento× Suzuki, Kojiro |
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著者所属 | ||||||
東京大学 | ||||||
著者所属 | ||||||
東京大学 | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Tokyo | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
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49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム論文集 en : JAXA Special Publication: Proceedings of the 49th Fluid Dynamics Conference / the 35th Aerospace Numerical Simulation Symposium 巻 JAXA-SP-17-004, p. 101-104, 発行日 2017-12-27 |
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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 | 第49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム (2017年6月28日-30日. 国立オリンピック記念青少年総合センター), 渋谷区, 東京 | |||||
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 | 49th Fluid Dynamics Conference /the 35th Aerospace Numerical Simulation Symposium (June 28-30, 2017. National Olympics Memorial Youth Center), Shibuya-ku, Tokyo, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Because of the singularity of the center axis, there is difficulty to accurately simulate a flow close to the axis. Vortex breakdown is known as a typical phenomenon, which takes place near the axis, and then, it is significantly important to resolve the flow around the axis. In this paper, a fully three-dimensional incompressible flow was simulated in a cylindrical coordinate system by a staggered mesh without artificial viscosity. In such a configuration, solving a radial momentum equation on the axis is required but it has singularity on the axis. Here, the singularity was removed by L’Hospital’s rule and the radial momentum equation was solved on the axis. In order to prevent the radial velocity component on the axis from a multi-value function, single-valued-reconstruction was applied. Under these considerations, a swirling flow in a closed cylinder with a rotating bottom was numerically simulated and the flow structure of a vortex breakdown, which was a bubble type, was examined. Although our result showed non-zero velocity in the radial direction on the axis, it reduced to a machine zero as the continuity equation converges. At last, it was shown that the topology of a bubble-type vortex breakdown lead to that of an axisymmetric spherical vortex (a spheromak). | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSNONLINE | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 2433-2232 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA1730011014 | |||||
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-17-004 |