Conference Paper 迎角再突入時でのMHD Flow Controlに与えるホール効果の影響
Influence of Hall Effect on MHD Flow Control in Reentry Flight with Attack Angle

益田, 克己  ,  下澤, 雄太  ,  藤野, 貴康  ,  Masuda, Katsumi  ,  Shimosawa, Yuta  ,  Fujino, Takayasu

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.
会議情報: 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
形態: カラー図版あり
Meeting Information: 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
Physical characteristics: Original contains color illustrations

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