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高迎角剥離流の非定常解析に向けて
https://jaxa.repo.nii.ac.jp/records/4008
https://jaxa.repo.nii.ac.jp/records/400826fd7dbf-e79f-4bd3-b295-7c6727a62d2c
名前 / ファイル | ライセンス | アクション |
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62268008.pdf (979.6 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 | 高迎角剥離流の非定常解析に向けて | |||||
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 | Toward Unsteady Analysis of High Attack Angle Separated Flow | |||||
著者 |
橋本, 敦
× 橋本, 敦× 石田, 崇× 石向, 桂一× 青山, 剛史× Hashimoto, Atsushi× Ishida, Takashi× Ishiko, Keiichi× Aoyama, Takashi |
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著者所属 | ||||||
宇宙航空研究開発機構航空本部数値解析技術研究グループ(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空本部数値解析技術研究グループ(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空本部数値解析技術研究グループ(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空本部数値解析技術研究グループ(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Numerical Simulation research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Numerical Simulation research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Numerical Simulation research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Numerical Simulation research Group, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
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45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2013論文集 en : JAXA Special Publication 巻 JAXA-SP-13-011, p. 41-46, 発行日 2014-03-31 |
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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45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2013 (2013年7月4日-5日. タワーホール船堀), 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 | 45th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2013 (July 4-5, 2013. Tower Hall Funabori), Tokyo, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | We show a research plan toward unsteady analysis of high-attack-angle separated flow. Although the separated flow is still a challenging problem for CFD, prediction technology of separation is necessary to improve CFD capability and expand applications in the flight envelope. Our research plan consists of (1) parallel automatic grid generation and (2) highly-accurate unsteady flow analysis with unstructured grid. In this paper, we also review buffet analyses using URANS or RANS/LES hybrid methods and show the current problems to be solved. In addition, the NASA-CRM with high attack angle is computed with steady RANS analysis to know the overall flow field and RANS limitations. | |||||
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: AA0062268008 | |||||
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-13-011 |