@inproceedings{oai:jaxa.repo.nii.ac.jp:00003448,
 author = {亀山, 正樹 and 槙原, 幹十朗 and Kameyama, Masaki and Makihara, Kanjuro},
 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, The present paper treats the piezoelectric energy harvesting from aeroelastic vibration with cantilevered laminated plates. The aeroelastic flutter energy harvester is composed of a piezoelectric patch attached to the structures and a conventional harvesting circuit. A diode bridge of four diodes is connected to the piezoelectric patch and it provides a mechanism of current rectification. Aeroelastic analysis of composite plate wings with a piezoelectric patch is based on the finite element method and the subsonic unsteady lifting surface theory. The effect on location of piezoelectric patch on converged voltage in the harvesting system is examined through the numerical examples., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1630046055, レポート番号: JAXA-SP-16-008E},
 pages = {517--524},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {Piezoelectric energy harvesting from aeroelastic vibration with composite plate wings},
 volume = {JAXA-SP-16-008E},
 year = {2017}
}