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低Re 数におけるIshii 翼型まわりの流れ場
https://jaxa.repo.nii.ac.jp/records/4022
https://jaxa.repo.nii.ac.jp/records/4022640ba096-59d3-4929-a651-731334cd10b8
名前 / ファイル | ライセンス | アクション |
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62268022.pdf (923.7 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 | 低Re 数におけるIshii 翼型まわりの流れ場 | |||||
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 | Flow Field Phenomena on Ishii Airfoil at Low Reynolds Numbers | |||||
著者 |
大竹, 智久
× 大竹, 智久× 互井, 梨絵× 神田, 翔× 村松, 旦典× 本橋, 龍郎× Ohtake, Tomohisa× Tagai, Rie× Kanda, Shou× Muramatsu, Akinori× Motohashi, Tatsuo |
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著者所属 | ||||||
日本大学理工学部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空本部風洞技術開発センター(JAXA) | ||||||
著者所属 | ||||||
株式会社ケーヒン | ||||||
著者所属 | ||||||
日本大学理工学部 | ||||||
著者所属 | ||||||
日本大学理工学部 | ||||||
著者所属(英) | ||||||
en | ||||||
College of Science and Technology, Nihon University | ||||||
著者所属(英) | ||||||
en | ||||||
Wind Tunnel Technology Center, Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Keihin Corporation | ||||||
著者所属(英) | ||||||
en | ||||||
College of Science and Technology, Nihon University | ||||||
著者所属(英) | ||||||
en | ||||||
College of Science and Technology, Nihon University | ||||||
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. 121-125, 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 | Flow visualization of Ishii airfoil was performed to clarify flow field around the airfoil at chord based Reynolds number from 20,000 to 60,000. Although oil flow technique, one of common and traditional wall tracing visualization methods, was applied to visualize flow field on the airfoil, the flow field could not be visualized clearly in these low Reynolds number region. We devised and applied a new technique of visualizing the flow field on the airfoil surface with fluorescence aqueous; we named this technique as “fluorescence liquid film technique.” This technique is possible to visualize flow field on the airfoil in low Reynolds number regions. As the results of flow visualization by fluorescence liquid film technique, we recognized flow field phenomena on the airfoil in low Reynolds number region that the positions of separation point and reattachment point and the length of separation bubble were changed on the airfoil depending on Reynolds number changing. | |||||
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: AA0062268022 | |||||
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 |