@inproceedings{oai:jaxa.repo.nii.ac.jp:00006595,
 author = {塚原, 孝則 and 橋口, 祐子 and 太田, 智基 and 小生方, 正裕 and Tsukahara, Takanori and Hashiguchi, Yuko and Ota, Tomoki and Obukata, Masahiro},
 book = {宇宙航空研究開発機構特別資料: 第66回　風洞研究会議論文集, JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 66th Meeting},
 month = {Mar},
 note = {This paper presents the outline of the scaled model rotor system, which was used in 2 m by 2 m FHI low-speed wind tunnel, and some typical wind tunnel tests. The scaled model rotor system has been applied for many fundamental tests and development tests since 1991. The system consists of teetering type hub, blades, pylon, rotary balance and servomotor etc. The collective pitch and cyclic pitch can be changed with remote control., 資料番号: AA0047428006, レポート番号: JAXA-SP-03-003},
 pages = {44--50},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {ロータ模型回転装置を用いた風洞試験},
 volume = {JAXA-SP-03-003},
 year = {2004}
}