@inproceedings{oai:jaxa.repo.nii.ac.jp:00046358,
 author = {布施, 亮祐 and 上島, 啓司 and 菅原, 瑛明 and 保江, かな子 and 石田, 崇 and 口石, 茂 and 青山, 剛史 and 田辺, 安忠 and Fuse, Ryosuke and Ueshima, Keiji and Sugawara, Hideaki and Yasue, Kanako and Ishida, Takashi and Kuchiishi, Shigeru and Aoyama, Takashi and Tanabe, Yasutada},
 book = {宇宙航空研究開発機構特別資料: 第51回流体力学講演会/第37回航空宇宙数値シミュレーション技術シンポジウム論文集, JAXA Special Publication: Proceedings of the 51st Fluid Dynamics Conference / the 37th Aerospace Numerical Simulation Symposium},
 month = {Feb},
 note = {第51回流体力学講演会/第37回航空宇宙数値シミュレーション技術シンポジウム (2019年7月1日-3日. 早稲田大学早稲田キャンパス国際会議場), 新宿区, 東京, 51st Fluid Dynamics Conference / the 37th Aerospace Numerical Simulation Symposium (July 1-3, 2019. International Conference Center, Waseda University), Shinjuku-ku, Tokyo, Japan, A CFD solver “FaSTAR-Move” that enables analysis around moving and deformed objects have been developed by JAXA, and was applied to the analysis of separation of mounted objects, etc. Currently, the rotorcraft analysis module has been added to FaSTAR-Move in order to meet industrial needsdemands for the rotorcraft analysis . In this paper, comparisons and validations of the developed module with experiments of hovering rotor are performed and 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: AA1930011017, レポート番号: JAXA-SP-19-007},
 pages = {193--199},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {非構造移動重合格子解析プログラム (FaSTAR-Move) の回転翼解析への拡張},
 volume = {JAXA-SP-19-007},
 year = {2020}
}