@inproceedings{oai:jaxa.repo.nii.ac.jp:00047326,
 author = {深谷, 英彦 and 甲斐, 大貴 and 杉浦, 裕樹 and 手塚, 亜聖 and FUKAYA, Hidehiko and KAI, Daiki and SUGIURA, Hiroki and TEZUKA, Asei},
 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), A 60 deg delta wing model was subjected to forced sinusoidal oscillation test with an amplitude of 1.6 deg using JAXA 60 cm magnetic suspension and balance system (MSBS) wind tunnel at a wind speed of 20 m/s and an AOA of 0-10 deg and aerodynamic force were measured. The literal stability coefficients were identified from the regression analysis of the time history of the literal aerodynamic forces with the roll angle, roll angular velocity, and lateral force as parameters. The time history of the literal aerodynamic forces of the regression analysis were compared with that of experiment and showed good agreement at AOA of 10 degree. The delta wing model is statically and dynamically stable in the roll axis at all AOA., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA2030013005, レポート番号: JAXA-SP-20-008},
 pages = {37--42},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {磁力支持によって運動するデルタ翼模型に働くローリングモーメントの回帰分析による同定},
 volume = {JAXA-SP-20-008},
 year = {2021}
}