@inproceedings{oai:jaxa.repo.nii.ac.jp:00004389,
 author = {永田, 靖典 and 大津, 広敬 and 山田, 和彦 and 安部, 隆士 and Nagata, Yasunori and Otsu, Hirotaka and Yamada, Kazuhiko and Abe, Takashi},
 book = {宇宙航空研究開発機構特別資料: 第43回流体力学講演会: 航空宇宙数値シミュレーション技術シンポジウム2011論文集, JAXA Special Publication: Proceedings of 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011},
 month = {Mar},
 note = {第43回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2011 (2011年7月7日-8日. 早稲田大学国際会議場) 東京, 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011 (July 7-8,  2011. Waseda University, International Conference Center), Tokyo Japan, In the electrodynamic flow control, a weakly-ionized plasma flow behind the strong shock wave is controlled by the applied magnetic field around are entry vehicle. According to the experimental measurement with an arc-jet wind tunnel, the electrodynamic effect is influenced by the magnetic configuration. In this study, the numerical MHD simulation was performed to investigate the influence of the inclination angle and the intensity of the magnetic field. The present results show that the circulation region is generated around a body when the magnetic field intensity exceeds a threshold value. The manner of the variation of the aerodynamic force associated with the magnetic field inclination strongly depends on the magnetic field intensity because the circulation region causes the drastic change of the flow field and electromagnetic field., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065207017, レポート番号: JAXA-SP-11-015},
 pages = {101--106},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {弱電離プラズマ流制御における印加磁場配位の影響に関する数値解析},
 volume = {JAXA-SP-11-015},
 year = {2012}
}