@inproceedings{oai:jaxa.repo.nii.ac.jp:00047335,
 author = {齊藤, 健一 and 有薗, 仁 and 杉岡, 洋介 and SAITO, Kenichi and ARIZONO, Hitoshi and SUGIOKA, Yosuke},
 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), JAXA's CFD code ''FaSTAR'' is being enhanced for flutter analysis and design in the ISSAC research frame work. The original experimental data is acquired for verification with the wind tunnel scale model. The wind tunnel test with rigid model was performed to obtain pressure distribution and deformation prior to the elastic model. Outline of the test and analysis are reported., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA2030013014, レポート番号: JAXA-SP-20-008},
 pages = {103--107},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {ISSACフラッタ解析・試験技術におけるクリーン形態剛体模型圧力分布計測とその対応解析について},
 volume = {JAXA-SP-20-008},
 year = {2021}
}