@inproceedings{oai:jaxa.repo.nii.ac.jp:00003648,
 author = {益田, 克己 and 下澤, 雄太 and 藤野, 貴康 and Masuda, Katsumi and Shimosawa, Yuta and Fujino, Takayasu},
 book = {宇宙航空研究開発機構特別資料: 第47回流体力学講演会/第33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 47th Fluid Dynamics Conference / the 33rd Aerospace Numerical Simulation Symposium},
 month = {Mar},
 note = {第47回流体力学講演会/第33回航空宇宙数値シミュレーション技術シンポジウム (2015年7月2日-3日. 東京大学生産技術研究所), 目黒区, 東京, 47th Fluid Dynamics Conference /the 33rd Aerospace Numerical Simulation Symposium (July 2-3, 2015. Institute of Industrial Science , the University of Tokyo), Meguro-ku, Tokyo, Japan, Three-dimensional magnetohydrodynamic (MHD) numerical simulation is carried out to examine the influence of the Hall effect on MHD flow control in earth reentry flight with attack angles. In the simulation, the Hall effect is taken into account. Numerical results show that the Hall effect distorts the distribution of the electric currents around a reentry vehicle with attack angles. The distortion of electric currents leads to the generation of a side force on the vehicle, although the side force obtained under the present simulation conditions is considerably weak compared with a drag and a lift force. Furthermore, the numerical results indicate that the strength and the direction of the side force depend on attack angles, and also that the side force becomes zero at a particular attack angle., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1630005023, レポート番号: JAXA-SP-15-013},
 pages = {147--152},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {迎角再突入時でのMHD Flow Controlに与えるホール効果の影響},
 volume = {JAXA-SP-15-013},
 year = {2016}
}