@inproceedings{oai:jaxa.repo.nii.ac.jp:00003403,
 author = {佐藤, 圭悟 and 横関, 智弘 and Sato, Keigo and Yokozeki, Tomohiro},
 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, Morphing wings are anticipated as a way to improve efficiency over a wider range of flight conditions, but it is difficult to realize morphing because there are two conflicting demands, i.e. stiffness for aerodynamic forces and flexibility for morphing. Super-anisotropy of the corrugated panels is a solution to satisfy those demands. In this paper, in order to realize morphing control surface, the model which has corrugated panels driven by skins is proposed. The deformation analysis and the aerodynamic analysis are conducted. The parametric study showed the efficiency of this model compared with the plain flap., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1630046010, レポート番号: JAXA-SP-16-008E},
 pages = {105--110},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {Structural design of morphing control surface using corrugated panels},
 volume = {JAXA-SP-16-008E},
 year = {2017}
}