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Wing-Tip-Chained Airplanesの空力特性と飛行ダイナミクスの基礎的解析
https://jaxa.repo.nii.ac.jp/records/46348
https://jaxa.repo.nii.ac.jp/records/46348a7210bc5-eb9f-4e22-861a-ff0c2d8c5db3
名前 / ファイル | ライセンス | アクション |
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AA1930011007.pdf (1.5 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2020-02-04 | |||||
タイトル | ||||||
タイトル | Wing-Tip-Chained Airplanesの空力特性と飛行ダイナミクスの基礎的解析 | |||||
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 | Preliminary Analysis of the Aerodynamic Characteristics and Flight Dynamics of Wing-Tip-Chained Airplanes | |||||
著者 |
末永, 陽一
× 末永, 陽一× 鈴木, 宏二郎× Suenaga, Yoichi× Suzuki, Kojiro |
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著者所属 | ||||||
東京大学 | ||||||
著者所属 | ||||||
東京大学 | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Tokyo | ||||||
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51回流体力学講演会/第37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 51st Fluid Dynamics Conference / the 37th Aerospace Numerical Simulation Symposium 巻 JAXA-SP-19-007, p. 113-118, 発行日 2020-02-04 |
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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51回流体力学講演会/第37回航空宇宙数値シミュレーション技術シンポジウム (2019年7月1日-3日. 早稲田大学早稲田キャンパス国際会議場), 新宿区, 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 | 51st Fluid Dynamics Conference / the 37th Aerospace Numerical Simulation Symposium (July 1-3, 2019. International Conference Center, Waseda University), Shinjuku-ku, Tokyo, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Traditional planetary exploration mainly utilizes orbital satellites or surface explorer robots. However if there is a gas atmosphere around the planet, unmanned airplanes could provide a much more detailed data of the planet surface compared to satellites, and data could be obtained at a much wider area compared to surface explorer robots. In this paper, a new design concept for a Mars airplane, and the preliminary analysis of the characteristics and flight dynamics for it was introduced. The new concept is called the “Wing-Tip-Chained” airplanes, and consist of multiple small airplanes joined together at the wing tips by releasable hinged joints. By connecting the wing tips and creating one (or several) large airplanes with a high aspect ratio, the total induced drag could be largely reduced thus, expanding the possible exploration area by increasing the efficiency of the flight. In order to clarify the fundamental characteristics of such joined wing system, trail calculation was made with a preliminary model consisting of 2 joint wings, to research the effect of hinge angle and other parameters on the damping of wing oscillation around the hinges when disturbed. | |||||
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: AA1930011007 | |||||
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-19-007 |