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CFD 解析における物体後流域や遠方境界のメッシュの影響
https://jaxa.repo.nii.ac.jp/records/2946
https://jaxa.repo.nii.ac.jp/records/2946fdd54d7f-b0be-423a-8d25-76fa41d2eb53
名前 / ファイル | ライセンス | アクション |
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AA1830029017.pdf (5.1 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2019-02-28 | |||||
タイトル | ||||||
タイトル | CFD 解析における物体後流域や遠方境界のメッシュの影響 | |||||
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 | Effect of Mesh Condition in Wakes or Far-field Boundary Areas on CFD analysis | |||||
著者 |
高橋, 良尚
× 高橋, 良尚× 松島, 紀佐× 清水, 亮介× Takahashi, Yoshinao× Matsushima, Kisa× Shimizu, Ryosuke |
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著者所属 | ||||||
富山大学 | ||||||
著者所属 | ||||||
富山大学 | ||||||
著者所属 | ||||||
富山大学 | ||||||
著者所属(英) | ||||||
en | ||||||
University of Toyama | ||||||
著者所属(英) | ||||||
en | ||||||
University of Toyama | ||||||
著者所属(英) | ||||||
en | ||||||
University of Toyama | ||||||
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50回流体力学講演会/第36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 50th Fluid Dynamics Conference / the 36th Aerospace Numerical Simulation Symposium 巻 JAXA-SP-18-005, p. 153-158, 発行日 2019-02-25 |
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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50回流体力学講演会/第36回航空宇宙数値シミュレーション技術シンポジウム (2018年7月4日-6日. 宮崎市民プラザ), 宮崎市, 宮崎 | |||||
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 | 50th Fluid Dynamics Conference /the 36th Aerospace Numerical Simulation Symposium (July 4-6, 2018. Miyazaki Citizen's Plaza), Miyazaki, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | This article investigates effect of mesh distribution in wakes and distant flow-fields from an airplane on resulted flow phenomena when performing RANS CFD simulation. Heretofore, mesh distribution in those flow-fields is rather coarse. It is not sufficient for grasping accurate wake phenomena which are important for obtaining aerodynamic coefficient by wake integration as well as evaluating wake turbulence effect on others. The investigation is conducted regarding three subjects. The first one is mesh distribution in the vicinity of far-field boundaries of a computational domain. The second is to enlarge a computational domain, while the other is mesh distribution on downstream field of airplane. Through the investigation, several useful clues have been obtained for attaining good flow resolution in those fields by CFD. | |||||
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: AA1830029017 | |||||
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-18-005 |