低马赫数冲击的结构和离子动力学行为

D. B. Graham, Yu. V. Khotyaintsev
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摘要

在太阳风和行星体上游经常观测到低马赫数的无碰撞冲击。然而,大多数现场观测都缺乏必要的时间分辨率来直接研究离子穿过这些冲击的动力学行为。我们研究了磁层多尺度(MMS)飞行任务观测到的一系列五个低马赫数弓形冲击穿越。这五个冲击的马赫数相当,但冲击法向角(66^{circ} \lesssim \theta_{Bn} \lesssim 89^{circ}$)和斜坡宽度(5~\mathrm{km} \lesssim l \lesssim 100~\mathrm{km}$)各不相同。结果表明,冲击宽度对决定质子反射和被冲击激发的比例至关重要,质子反射随着冲击宽度的减小而增加。随着冲击宽度的增加,质子反射会完全停止。对于近乎垂直的冲击,反射质子呈现出准周期结构,这种结构在冲击下游很远的地方持续存在。当冲击-法向角变得越来越斜时,这些周期性质子结构就会扩大,从而形成一个高能卤群。冲击下游磁场的周期性波动是由α粒子的动态压力波动产生的,这些α粒子在跨冲击电势的作用下减速,随后在日格相束流作用下减速。这些结果表明,在低马赫数冲击中发生了复杂的动力学尺度离子动力学,这在很大程度上取决于冲击剖面。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The Structure and Kinetic Ion Behavior of Low Mach Number Shocks
Low Mach number collisionless shocks are routinely observed in the solar wind and upstream of planetary bodies. However, most in situ observations have lacked the necessary temporal resolution to directly study the kinetic behavior of ions across these shocks. We investigate a series of five low Mach number bow shock crossings observed by the Magnetospheric Multiscale (MMS) mission. The five shocks had comparable Mach numbers, but varying shock-normal angles ($66^{\circ} \lesssim \theta_{Bn} \lesssim 89^{\circ}$) and ramp widths ($5~\mathrm{km} \lesssim l \lesssim 100~\mathrm{km}$). The shock width is shown to be crucial in determining the fraction of protons reflected and energized by the shock, with proton reflection increasing with decreasing shock width. As the shock width increases proton reflection is arrested entirely. For nearly perpendicular shocks, reflected protons exhibit quasi-periodic structures, which persist far downstream of the shock. As the shock-normal angle becomes more oblique these periodic proton structures broaden to form an energetic halo population. Periodic fluctuations in the magnetic field downstream of the shocks are generated by fluctuations in dynamic pressure of alpha particles, which are decelerated by the cross-shock potential and subsequently undergo gyrophase bunching. These results demonstrate that complex kinetic-scale ion dynamics occur in low Mach number shocks, which depend significantly on the shock profile.
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