火星准垂直弓形冲击区的宽度

S. Nesbit‐Östman, H. Gunell, M. Hamrin, H. Opgenoorth, Laila Andersson
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引用次数: 0

摘要

我们的目标是量化准垂直火星弓形震荡区域的宽度,以加深对宽度变化的原因和影响因素的理解,并探索其对热化的影响。为了量化宽度,对数据库中的 2074 个准垂直弓形冲击交叉点进行了研究。研究考虑了上游条件,如马赫数、动态压力、离子密度和其他因素。此外,还测量了下游和上游的温度差。我们发现,冲击区域的宽度与磁声波马赫数、临界比率和过冲幅度相关。该区域与动态压力反相关。宽度不受所研究物种的上游离子密度或上游温度的影响。下游和上游温度之间的差异也不受冲击区宽度的影响。我们发现,磁声波马赫数和动压等影响弓形冲击距离的因素也会影响宽度。宽度与过冲幅度也呈正相关,这表明这两种结构是耦合的,或者说它们受到的影响条件大致相同。与离子温差缺乏相关性表明,冲击区宽度并不影响离子热化。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Width of the quasi-perpendicular bow shock region at Mars
We aim to quantify the width of the quasi-perpendicular Martian bow shock region to deepen the understanding of why the width is variable and which factors affect it, and to explore the implications on thermalization. To quantify the width, 2074 quasi-perpendicular bow shock crossings from a database were studied. Upstream conditions, such as Mach numbers, dynamic pressure, ion densities, and other factors, were considered. Furthermore, the difference between the downstream and upstream temperature was measured. We found that the shock region width is correlated with the magnetosonic Mach number, the critical ratio, and the overshoot amplitude. The region was found to be anticorrelated with dynamic pressure. The width is not affected by the upstream ion density of the investigated species or by the upstream temperature. The difference between the downstream and upstream temperature is not affected by the shock region width. We found that the factors that affect the stand-off distance of the bow shock, such as the magnetosonic Mach number and dynamic pressure, also affect the width. The width is also positively correlated with the overshoot amplitude, indicating that the structures are coupled or that they are affected by largely the same conditions. The lack of a correlation with the ion temperature difference indicates that the shock region width does not affect the ion thermalization.
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