Numerical Simulation of 2D Supersonic Magnetohydrodynamic Channel and Study on Hall Effect

作     者：ZHENG Xiaomei LU Haoyu XU Dajun CAI Guobiao 

作者机构：School of Astronautics Beihang University Beij'ing 100191 China 

出 版 物：《Chinese Journal of Aeronautics》 (中国航空学报（英文版）)

年 卷 期：2011年第24卷第2期

页      面：136-144页

核心收录：

学科分类：0809[工学-电子科学与技术（可授工学、理学学位）] 080704[工学-流体机械及工程] 08[工学] 080401[工学-精密仪器及机械] 0807[工学-动力工程及工程热物理] 0804[工学-仪器科学与技术] 

主　　题：hypersonic vehicles scramjet magnetohydrodynamics Hall effect numerical simulation 

摘      要：In this research effort,numerical simulation of two-dimensional magnetohydrodynamic（MHD） channel is performed and Hall effect is *** computational model consists of the Navier-Stokes（N-S） equations coupled with electrical-magnetic source terms,Maxwell equations and the generalized Ohm＇s *** conditions for the electrical potential equation considering Hall effect are *** start with,the MHD channel with single-pair electrodes is studied and flow of the electric current is in accordance with physical *** the MHD channel with five-pair electrodes is numerically *** results show that the electrical current concentrates on the downstream of the anode and the upstream of the cathode due to Hall effect,and the flow field becomes *** the current value of the magnetic interaction parameter,the electrical-magnetic force affects the flow remarkably,decreasing the outlet Mach number and increasing the outlet pressure;what＇s more,the flow structure in the channel becomes extremely *** of MHD channels with continual electrodes and segmented electrodes are *** results show that performance of the MHD channel with segmented electrodes is better than that with continual electrodes with the increase of Hall parameter.