@inproceedings{oai:jaxa.repo.nii.ac.jp:00038190,
 author = {近藤, 夏樹 and 末永, 尚史 and 白井, 正孝 and 齊藤, 茂 and 赤坂, 剛史 and 田辺, 安忠 and Kondo, Natsuki and Suenaga, Hisashi and Shirai, Masataka and Saito, Shigeru and Akasaka, Takeshi and Tanabe, Yasutada},
 book = {航空宇宙技術研究所特別資料: 平成14年度航空安全・環境適合技術研究研究交流会と研究報告会講演論文集, Special Publication of National Aerospace Laboratory: Proceedings of the Information Exchange Meeting and the Research Meeting on Aviation Safety and Environmental Compatibility Technology Research FY2001},
 month = {Dec},
 note = {This paper shows the results of the elementary wind tunnel test of blade active control using a 1-bladed model rotor at the 2.5 m x 2.5 m multi-purpose wind tunnel in Kawada Industry. In this test, the effects of higher harmonic control (HHC) and active flap control (AFC) on rotor blade-vortex interaction (BVI) noise were investigated. The frequency of the control was 20 Hz (2/rev), and the amplitudes of HHC and AFC were +/- 2.0 deg and +/- 15.0 deg, respectively. The phase of control was changed at intervals of 45 deg. Two types of BVI were tested. The one is the parallel vortex interaction using the vortex generator upstream of a non-lifting rotor. The other is self-generated vortex interaction of a lifting rotor. As a result, the effects of BVI noise reduction were observed in the some cases., 資料番号: AA0045946010, レポート番号: NAL SP-55},
 pages = {93--96},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {ロータ・アクティブ・コントロール基礎風洞試験},
 volume = {55},
 year = {2002}
}