タイトル | 編隊飛行の空気力学について |
その他のタイトル | Aerodynamics of formation flight Second Report 第2報 |
著者(日) | 河邉 博康; 畑村 透 |
著者(英) | Kawabe, Hiroyasu; Hatamura, Toru |
著者所属(日) | 日本文理大学 工学部 航空宇宙工学科; 日本文理大学 大学院工学研究科 |
著者所属(英) | Nippon Bunri University Department of Aerospace Engineering, School of Engineering; Nippon Bunri University Graduate School of Engineering |
発行日 | 2005-03-15 |
刊行物名 | 日本文理大学紀要 Bulletin of Nippon Bunri University |
巻 | 33 |
号 | 1 |
開始ページ | 17 |
終了ページ | 27 |
刊行年月日 | 2005-03-15 |
言語 | jpn |
抄録 | The wings formation flight is studied by means of theoretical aerodynamics. Each wing is modeled using the horse-shoe vortex. In formation flight each wing flies in an upwash field generated by all other wings of the formation, and consequently its flight power decreases. In V formation flight the wing in a central position has a smaller local flight power reduction, while in U formation flight the local flight power reduction of each wing remains equal. In the case of a long range flight, the optimum shape is not V formation, but U formation flight. It has turned out that the value of a local flight power reduction in V formation flight is equal to that in U formation flight when the leader wing of V formation shifts to the position of a follower wing. |
キーワード | aerodynamics; horseshoe vortex; V formation flight; U formation flight; lift; computerized simulation; induced velocity; upward field; power reduction; sweepback; 空気力学; 馬蹄形渦; V字編隊飛行; U字編隊飛行; 揚力; 計算機シミュレーション; 誘導速度; 吹き上げ; パワー減少; 後退角 |
資料種別 | Technical Report |
ISSN | 0287-3036 |
SHI-NO | AA0048497001 |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/40068 |