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エンジン筒内流動解析における格子細分化法の適用
https://jaxa.repo.nii.ac.jp/records/3244
https://jaxa.repo.nii.ac.jp/records/324406fb07fc-99e5-4573-b721-569428003153
名前 / ファイル | ライセンス | アクション |
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AA1730011010.pdf (1.7 MB)
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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 | エンジン筒内流動解析における格子細分化法の適用 | |||||
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 | Application of an adaptive mesh refinement method to the analysis of flow inside an engine cylinder | |||||
著者 |
松尾, 裕一
× 松尾, 裕一× 南部, 太介× 溝渕, 泰寛× 桑原, 匠史× 桐原, 亮平× 中森, 一郎× Matsuo, Yuichi× Nambu, Taisuke× Mizobuchi, Yasuhiro× Kuwabara, Takuhito× Kirihara, Ryohei× Nakamori, Ichiro |
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著者所属 | ||||||
宇宙航空研究開発機構航空技術部門(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空技術部門(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空技術部門(JAXA) | ||||||
著者所属 | ||||||
アドバンスソフト株式会社 | ||||||
著者所属 | ||||||
アドバンスソフト株式会社 | ||||||
著者所属 | ||||||
アドバンスソフト株式会社 | ||||||
著者所属(英) | ||||||
en | ||||||
Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Aeronautical Technology Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
AdvanceSoft Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
AdvanceSoft Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
AdvanceSoft Corporation | ||||||
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. 79-82, 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-40日. 国際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 | This paper describes the application of an adaptive mesh refinement method based on the block-based adaptation to the analysis of flow inside an engine cylinder. The suitability of the present AMR methodology, particularly of the time integration method and the effect of AMR to the computational results is shown. By comparing the results obtained using 1mm uniform mesh, 0.5mm uniform mesh, AMR mesh, we find the present block-based AMR method is effective for the high resolution of the flow analysis in the engine cylinder. | |||||
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: AA1730011010 | |||||
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 |