The Liquid Metal Experimental Loop(LMEL) is an unique experimental device of magnetohydrodynamic(MHD) effect and compatibility studies for fusion in China.
液态金属实验回路（LMEL）是国内唯一用于聚变堆磁流体动力学（MHD）效应和材料相容性研究的大型实验装置。
A linear analysis of the ideal magnetohydrodynamic (MHD) stability of the Z-pinch is presented in which plasma flows are included in the equilibrium.
本文利用理想磁流体力学(MHD)模型对含有轴向流动的Z箍缩等离子体不稳定性进行了分析。
Based on two-fluid model of ion and electron and Maxwell equation, the two-dimensional magnetohydrodynamic (MHD) model of vacuum arc was obtained.
以离子与电子的双流体模型以及麦克斯韦方程为基础，推导得到了真空电弧的二维磁流体动力学(MHD)模型。
In cylindrical helical coordinates, generalized magnetohydrodynamic (MHD) equations are reduced to four first order differential equations.
采用柱螺旋坐标系，把广义磁流体力学方程组简化为四元一阶微分方程组。
The mechanism of magnetohydrodynamic (MHD) control is demonstrated in the article.
阐述了磁流体动力学(MHD)控制流场作用机理。
The ideal Magnetohydrodynamic equations (MHD), the governing equations of the solar atmosphere dynamical process, are taken to numerically simulate Coronal Mass Ejection (CME) phenomena.
采用理想磁流体力学方程组(MHD)作为太阳大气动力学过程的控制方程组，定性数值模拟日冕物质抛射(CME)现象。
Surface insulating coating can significantly reduce the magnetohydrodynamic (MHD) pressure drop in self cooled liquid metal blanket for fusion reactors.
结构材料表面涂层是解决聚变堆液态金属自冷却包层中的磁流体动力学压降(MHD)的主要方法之一。
Using the method of characteristics and shock fitting techniques, this paper simulates numerically the evolution of MHD (Magnetohydrodynamic) intermediate shocks in interplanetary space.
本文采用特征线方法和激波装配法，对磁流体中间激波在行星际空间的演化过程进行数值模拟。
Using the method of characteristics and shock fitting techniques, this paper simulates numerically the evolution of MHD (Magnetohydrodynamic) intermediate shocks in interplanetary space.
本文采用特征线方法和激波装配法，对磁流体中间激波在行星际空间的演化过程进行数值模拟。
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