@inproceedings{oai:jaxa.repo.nii.ac.jp:00003395,
 author = {磯貝, 紘二 and Isogai, Koji},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication: Proceedings of the First International Symposium on Flutter and its Application},
 month = {Mar},
 note = {First International Symposium on Flutter and its Application (May 15-17, 2016. Mielparque-tokyo), Minato-ku, Tokyo, Japan, Flapping wing has been utilized in many engineering fields such as power generation, micro aerial vehicles, under water vehicles, etc.. As is well known, flapping wing motion is governed by many parameters such as frequency, heaving amplitude, pitching (or feathering) amplitude, phase difference between heaving and pitching motions for rigid wing and additional parameters such as bending and torsion rigidity, mass distribution, etc. for elastic wings. Therefore, the application of optimum design technique plays crucial role for the design of high performance devices/vehicles using flapping wing. In this paper, some applications of an optimization technique to the flapping wing designs that the present author has studied during last fifteen years of his career are outlined. They are a flutter power generation system, a micro aerial vehicle and its use for the estimation of the propulsive performance of dolphin., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1630046002, レポート番号: JAXA-SP-16-008E},
 pages = {33--42},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {Some applications of an optimum design technique to flapping wing designs},
 volume = {JAXA-SP-16-008E},
 year = {2017}
}