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A note on the compression ratio in MHD shocks

机译:关于MHD冲击的压缩比的说明

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We present an analysis of the compression ratio in MHD shocks. Although the equation describing the compression ratio has been in the literature for decades, we believe that our results are interesting and complementary to the earlier research. We concentrate on the behavior of the compression ratio in a bow shock as a function of the angle between the shock normal and the plasma velocity. For this problem, we find non-unique solutions in certain regimes, which we investigate in detail. We also find regimes where the compression ratio in fast bow shocks achieves a local maximum in more than one location. In the last section, we consider the compression ratio in slow shocks and make some conclusions about the shape of the shock in this flow regime.
机译:我们对MHD冲击的压缩比进行分析。尽管描述压缩比的方程式在文献中已有数十年之久,但我们认为我们的研究结果很有趣,并且是对早期研究的补充。我们专注于弓形冲击中压缩比的行为,该变化是冲击法线与等离子速度之间的角度的函数。对于此问题,我们在某些情况下发现了非唯一解,我们将对其进行详细研究。我们还发现在快速船首冲击中的压缩比在一个以上的位置达到局部最大值的状态。在最后一节中,我们考虑了慢速冲击中的压缩比,并对这种流动状态下的冲击形状做出了一些结论。

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