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液体燃料微粒化初期過程の数値解析
https://jaxa.repo.nii.ac.jp/records/4928
https://jaxa.repo.nii.ac.jp/records/492807e52e1e-5af8-4d2d-8a4d-a1700ea2973d
名前 / ファイル | ライセンス | アクション |
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64672030.pdf (929.0 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 | 液体燃料微粒化初期過程の数値解析 | |||||
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_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 | Numerical Simulation of Liquid Fuel Primary Breakup | |||||
著者 |
新城, 淳史
× 新城, 淳史× 松山, 新吾× 溝渕, 泰寛× 小川, 哲× 梅村, 章× Shinjo, Junji× Matsuyama, Shingo× Mizobuchi, Yasuhiro× Ogawa, Satoru× Umemura, Akira |
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著者所属 | ||||||
宇宙航空研究開発機構研究開発本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発本部 | ||||||
著者所属 | ||||||
名古屋大学大学院工学研究科 | ||||||
著者所属(英) | ||||||
en | ||||||
Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate School of Engineering, Nagoya University | ||||||
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 | Large-scale numerical simulations of liquid fuel jet have been conducted to elucidate the physical mechanism of primary atomization near the injection nozzle. The grid resolution is made fine enough to resolve the smallest physical scale that is determined by the Weber number, i.e. surface tension effect. Such calculations have not been performed before, and this paper reports the world's first results on primary atomization in a turbulent spray. Physical processes are well captured such as surface instability development, ligament formation and droplet generation. While the aerodynamic force plays a role in developing surface instability, surface tension becomes more dominant in ligament and droplet formation. The droplet pinch-off is mostly dominated by the short-wave pinch-off mode, as the ligaments have tips. This is consistent with our previous research on droplet pinch-off from slow laminar liquid jets and provides insights into modeling. By these results, our understanding is made deeper on what is actually occurring inside a turbulent spray. The computational performance of JAXA's new supercomputer JSS is also described. Combined with the VisIMPACT parallelization method, this kind of large-scale computation can be easily implemented. With the reduction in I/O time, large unsteady simulations like this have been becoming possible. | |||||
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 | |||||
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: AA0064672030 | |||||
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 |