@inproceedings{oai:jaxa.repo.nii.ac.jp:00004385,
 author = {柳田, 祥之 and 小森, 瑛 and 大竹, 智久 and 村松, 旦典 and 本橋, 龍郎 and Yanagida, Shoji and Komori, Akira and Otake, Tomohisa and Muramatsu, Akinori and Motohashi, Tatsuo},
 book = {宇宙航空研究開発機構特別資料: 第43回流体力学講演会: 航空宇宙数値シミュレーション技術シンポジウム2011論文集, JAXA Special Publication: Proceedings of 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011},
 month = {Mar},
 note = {第43回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2011 (2011年7月7日-8日. 早稲田大学国際会議場) 東京, 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011 (July 7-8,  2011. Waseda University, International Conference Center), Tokyo Japan, A SDBD plasma actuator has been proposed to use pulse modulation in order to increase the efficiency of the perfomance. We examined the perfomance of the SDBD plasma actuator by varying both duty ratio and frequency of pulse modulation. The distributions of velocity induced by the SDBD plasma actuator in the still air were measured using a hot-wire anemometer. Induced flows were visualized by Mie scattering.The induced flows depend on both the duty ratio and the modulation frequency. The flow widens vertically when the duty ratio is high and the modulation frequency is low., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065207013, レポート番号: JAXA-SP-11-015},
 pages = {77--82},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {パルス変調を用いたSDBDプラズマアクチュエータが誘起する流れ},
 volume = {JAXA-SP-11-015},
 year = {2012}
}