ANALYTICAL MODEL OF THE PLANETARY BOW SHOCK FOR VARIOUS MAGNETIC FIELD DIRECTIONS BASED ON MHD CALCULATIONS

G. Kotova, M. Verigin, T. Gomboshi, K. Kabin
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引用次数: 1

Abstract

Study of physical processes in plasma near planets often requires knowledge of the position and shape of the planetary bow shock. Empirical models are usually used since theoretical MHD and kinetic models consume too much computer time and cannot be used to track fast processes. M.I. Verigin proposed a semi-empirical approach based on the use of exact theoretical expressions with a small number of parameters, which have a clear physical meaning. These parameters are estimated by fitting experimental data or detailed MHD calculations. A model of the bow shock near an arbitrary-shaped obstacle has previously been developed for a gas-dynamic flow. This model can be applied to any sonic Mach numbers and large values of the Alfven Mach number. In addition, the asymptotic Mach cone — the angle of inclination of the shock wave at an infinite distance from the planet — has been calculated analytically in the MHD approximation. In this paper, we propose a model of the bow shock for any direction of the magnetic field with respect to the upcoming flow and for any Mach numbers. Parameters of the model are the distance of the nose point from the obstacle, radius of curvature and bluntness of the bow shock at the nose point, a parameter related to the transition to the asymptotic downstream slope of the shock, and a skewing angle appearing when the interplanetary magnetic field is directed at an angle to the solar wind velocity.
基于MHD计算的不同磁场方向下行星弓形激波解析模型
研究行星附近等离子体的物理过程通常需要了解行星弓形激波的位置和形状。通常使用经验模型,因为理论MHD和动力学模型消耗太多的计算机时间,不能用于跟踪快速过程。M.I. Verigin提出了一种基于使用具有少量参数的精确理论表达式的半经验方法,这些参数具有明确的物理含义。这些参数是通过拟合实验数据或详细的MHD计算来估计的。以前已经为气体动力流动建立了一个靠近任意形状障碍物的弓形激波模型。该模型适用于任何音速马赫数和较大的阿尔芬马赫数。此外,还在MHD近似中解析地计算了渐近马赫锥,即激波在离行星无限远处的倾斜角。在本文中,我们提出了一个关于任何方向的磁场对即将到来的流动和任何马赫数的弓形激波模型。模型参数包括机头点到障碍物的距离、机头点弓形激波的曲率半径和钝度、一个与激波向渐近下游斜坡过渡有关的参数,以及行星际磁场与太阳风速度成一定角度时出现的偏斜角。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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