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アペックスフェンスを装備したデルタ翼の渦構造
https://jaxa.repo.nii.ac.jp/records/4413
https://jaxa.repo.nii.ac.jp/records/4413c21e09a3-e90f-4b43-ac5a-f62dee754c1d
名前 / ファイル | ライセンス | アクション |
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65207041.pdf (1.1 MB)
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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 | アペックスフェンスを装備したデルタ翼の渦構造 | |||||
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 Structure of Delta Wing with Slotted Apex Fence | |||||
著者 |
板倉, 嘉哉
× 板倉, 嘉哉× 小川, 秀介× Itakura, Yoshiya× Ogawa, Shusuke |
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著者所属 | ||||||
千葉大学教育学部 | ||||||
著者所属 | ||||||
千葉大学教育学部 | ||||||
著者所属(英) | ||||||
en | ||||||
Chiba University, Faculty of Education | ||||||
著者所属(英) | ||||||
en | ||||||
Chiba University, Faculty of Education | ||||||
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43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2011論文集 en : JAXA Special Publication: Proceedings of 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011 巻 JAXA-SP-11-015, p. 237-242, 発行日 2012-03-30 |
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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43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2011 (2011年7月7日-8日. 早稲田大学国際会議場) 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 | 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011 (July 7-8, 2011. Waseda University, International Conference Center), Tokyo Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Slotted apex fences are applied to improve low-speed aerodynamic charactenstics of 60 deg. delta wing model. The logitudinal forces and moment acting on the thin delta with apex fences (Apex fences are hinged to the delta wing upper surfaces along the leading edges at angles of 45,90 and 135 degrees.) are measured by using universal multi-component sensor and static pressure distribution on the upper surface is also measured by using pressure transducer with pressure scanner. Smoke flow visualization and the light sheet technique are being used to obtain cross sectional views of the fence induced vortices. Combination of pressure distribution maps and image of vortices provide information on the three-dimensional nature of the flow field structure induced by slotted apex fences. | |||||
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: AA0065207041 | |||||
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-11-015 |