@inproceedings{oai:jaxa.repo.nii.ac.jp:00047328,
 author = {布施, 亮祐 and 保江, かな子 and 菅原, 瑛明 and 田辺, 安忠 and FUSE, Ryosuke and YASUE, Kanako and SUGAWARA, Hideaki and TANABE, Yasutada},
 book = {宇宙航空研究開発機構特別資料: 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2020オンライン論文集, JAXA Special Publication: Proceedings of Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2020 Online},
 month = {Feb},
 note = {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2020オンライン (2020年9月28日-30日. 日本航空宇宙学会 : 宇宙航空研究開発機構(JAXA)オンライン会議), Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2020 Online (September 28-30, 2020. The Japan Society for Aeronautical and Space Sciences : Japan Aerospace Exploration Agency (JAXA), Online meeting), Currently, JAXA has been developing a rotorcraft analysis module, for a CFD solver ''FaSTAR-Move'' that enables analysis of moving and deforming objects, in order to meet industrial demands. In this paper, the rotor blade control function is added to the module, which is validated by analyses of the rotor/fuselage interactions based on JMRTS (JAXA Multi-purpose Rotor Test System) experiments. The analyses were performed for a wide range of advance ratios. Compared with experiments and analysis results by rFlow3D, it is shown that reasonable results are obtained., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA2030013007, レポート番号: JAXA-SP-20-008},
 pages = {47--51},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {回転翼解析に対するFaSTAR-Moveの機能拡張},
 volume = {JAXA-SP-20-008},
 year = {2021}
}