@inproceedings{oai:jaxa.repo.nii.ac.jp:00005658,
 author = {磯貝, 紘二 and 上澤, 裕一 and 播野, 洋平 and 佐藤, 寛幸 and Isogai, Koji and Kamisawa, Yuichi and Harino, Yohei and Sato, Hiroyuki},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication: Proceedings of Lectures and Workshop International: Recent Advances in Multidisciplinary Technology and Modeling},
 month = {Feb},
 note = {A method is presented for the optimum aeroelastic design of a flapping wing employing lifting-surface theory as an aerodynamic tool and the complex method as the optimization algorithm. The method is applied to the optimum design of a flapping wing of a Kite Hawk (Milvus migrans) UAV (Unmanned Aerial Vehicle) and the optimum thickness distribution of the main-spar is determined. As the result of the optimization, a high propulsive efficiency of 75 percent is attained considering only dihedral flapping of the main spar. By evaluating the viscous effect for this optimum design using a three-dimensional Navier-Stokes code, the effectiveness of the design is confirmed., 資料番号: AA0063824003, レポート番号: JAXA-SP-07-008E},
 pages = {20--36},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Optimum aeroelastic design of flapping wing for micro air vehicles},
 volume = {JAXA-SP-07-008E},
 year = {2008}
}