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編隊飛行時の空力特性と翼端渦の干渉
https://jaxa.repo.nii.ac.jp/records/4883
https://jaxa.repo.nii.ac.jp/records/48833c7394c6-6659-408f-83ef-4ac7d97f6107
名前 / ファイル | ライセンス | アクション |
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64575007.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 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 編隊飛行時の空力特性と翼端渦の干渉 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Aerodynamics, Formation Flight, Trailing Vortices, Vortex interaction | |||||
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 | Interactions of wing-tip vortices and their effects on the aerodynamic characteristics in formation flight | |||||
著者 |
森, 文秀
× 森, 文秀× 浅井, 雅人× 稲澤, 歩× Mori, Fumihide× Asai, Masahito× Inasawa, Ayumu |
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著者所属 | ||||||
首都大学東京 | ||||||
著者所属 | ||||||
首都大学東京 | ||||||
著者所属 | ||||||
首都大学東京 | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University | ||||||
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: 「境界層遷移の解明と制御」研究会講演論文集(第43回・第44回) en : JAXA Special Publication: Proceedings of the 43rd and 44th JAXA Workshops on "Investigation and Control of Boundar-Layer Transition" 巻 JAXA-SP-09-014, 発行日 2010-02-26 |
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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(2008年10月2日-10月3日)「境界層遷移の解明と制御」研究会; 第44回(2009年3月26日-3月27日)「境界層遷移の解明と制御」研究会 | |||||
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 JAXA Workshops on "Investigation and Control of Boundar-Layer Transition" (October 2-3, 2008) ; 44th JAXA Workshops on "Investigation and Control of Boundar-Layer Transition" (March 26-27, 2009) | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In order to clarify influences of trailing vortices of a forward wing on the aerodynamics of a backward wing in formation flight, behaviors and interactions of trailing vortices are examined experimentally in two-wing configuration at a Reynolds number Re = 2.5 x 10(exp 5). Both the wings have a NACA23012 airfoil section and rectangular plan-form with aspect ratio of 5. The wings are arranged in the horizontal plane with streamwise distance of 2.5 times the airfoil chord, and the forward wing is fixed at an angle of attack 8 deg. In such an arrangement, the lift to drag ratio is found to increase by 25% the two wings are overlapped with each other by 2.5-5 % of the full span, i.e., about the diameter of wing-tip vortex. Flow visualization and PIV measurements show that interactions of wing-tip vortices of both the wings occur most intensively in these conditions. | |||||
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: AA0064575007 | |||||
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-09-014 |