@inproceedings{oai:jaxa.repo.nii.ac.jp:00006603,
 author = {中尾, 雅弘 and 内山, 直樹 and 前田, 一郎 and 齊藤, 茂 and 青山, 剛史 and 近藤, 夏樹 and Nakao, Masahiro and Uchiyama, Naoki and Maeda, Ichiro and Saito, Shigeru and Aoyama, Takashi and Kondo, Natsuki},
 book = {宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2003論文集, JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2003},
 month = {Mar},
 note = {In the present study, CFD study was performed for 4 bladed rotor in BVI condition in order to validate its predictable ability. The computation was chosen for the corresponding BVI test case which has been performed in the previous wind tunnel test that has been conducted under collaborative research with NAL and MHI in May, 2002. The wind tunnel test was performed with free stream velocity and the rotor angle of attack being the primary parameters. The blade pitch was cyclically controlled to achieve desired thrust amount. As output from the test, measured are rotor six-component force, near leading edge pressure data and sound pressure history at fixed observation. Likewise, CFD computation was performed and was validated against these corresponding data., 資料番号: AA0047427002, レポート番号: JAXA-SP-03-002},
 pages = {5--10},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {ヘリコプタBVI騒音解析},
 volume = {JAXA-SP-03-002},
 year = {2004}
}