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首页> 外文期刊>Journal of Geophysical Research, A. Space Physics: JGR >Global MHD Simulations of the Earth's Bow Shock Shape and Motion Under Variable Solar Wind Conditions
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Global MHD Simulations of the Earth's Bow Shock Shape and Motion Under Variable Solar Wind Conditions

机译:全球MHD模拟地球弓形冲击形状和可变太阳风条件下的运动

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摘要

Empirical models of the Earth's bow shock are often used to place in situ measurements in context and to understand the global behavior of the foreshock/bow shock system. They are derived statistically from spacecraft bow shock crossings and typically treat the shock surface as a conic section parameterized according to a uniform solar wind ram pressure, although more complex models exist. Here a global magnetohydrodynamic simulation is used to analyze the variability of the Earth's bow shock under real solar wind conditions. The shape and location of the bow shock is found as a function of time, and this is used to calculate the shock velocity over the shock surface. The results are compared to existing empirical models. Good agreement is found in the variability of the subsolar shock location. However, empirical models fail to reproduce the two-dimensional shape of the shock in the simulation. This is because significant solar wind variability occurs on timescales less than the transit time of a single solar wind phase front over the curved shock surface. Empirical models must therefore be used with care when interpreting spacecraft data, especially when observations are made far from the Sun-Earth line. Further analysis reveals a bias to higher shock speeds when measured by virtual spacecraft. This is attributed to the fact that the spacecraft only observes the shock when it is in motion. This must be accounted for when studying bow shock motion and variability with spacecraft data.
机译:地球弓形震动的经验模型通常用于在上下文中放置原位测量,并了解止血/弓形冲击系统的全局行为。它们统计地从航天器弯曲障碍横线衍生,并且通常根据均匀的太阳风压力压力压力参数化的圆锥部分将冲击表面处理,尽管存在更复杂的模型。这里,全局磁力流体动力学模拟用于分析真正的太阳风能下地球弓形冲击的可变性。弓形冲击的形状和位置被发现是时间的函数,这用于计算冲击表面上的冲击速度。结果与现有的经验模型进行比较。在子震动位置的可变性中发现了良好的一致性。然而,经验模型不能再现模拟中冲击的二维形状。这是因为在小于弯曲冲击表面上的单个太阳能电相前方的横向时间小于时间尺度的时间尺度发生了显着的太阳风变性。因此,当解释航天器数据时,必须小心使用实证模型,特别是当观察到远离太阳地线时。进一步的分析显示通过虚拟航天器测量时偏差到更高的冲击速度。这归功于航天器仅在运动时观察震动的事实。必须考虑到使用航天器数据的弓形冲击运动和可变性时占用。

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