后激波区域湍流的发展

Michael M. Foley, Philip Mocz, Blakesley Burkhart, Lars Hernquist and Alyssa Goodman
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摘要

超音速等温湍流在星际介质中是普遍存在的。本文采用高分辨率的AREPO流体动力学模拟技术,研究了超声速湍流中孤立激波的发展和演化过程。我们发现激波可以放大后激波区域的湍流能量,同时诱导涡度的优先取向。这导致在震波后区域产生各向异性湍流。激波锋面附近湍流能量和耗散也得到强烈增强。通过将冷中性介质的典型尺度应用于模拟,我们发现在超级气泡尺度上进入湍流的激波可以产生103 M⊙mir - 1数量级的压缩流。我们的结果也与纯流体力学中关于冲击产生的湍流波动的相关研究结果一致。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Development of Turbulence in Postshock Regions
Supersonic isothermal turbulence is ubiquitous in the interstellar medium. This work presents high-resolution AREPO hydrodynamical simulations of isolated shocks moving through supersonic turbulence to study the development and evolution of turbulence in the pre- and postshock regions. We find that shocks can amplify turbulent energy in the postshock region while inducing a preferential orientation for the vorticity. This results in the creation of anisotropic turbulence in the postshock region. Turbulent energy and dissipation are also strongly enhanced near the shock front. By applying typical scalings from the cold neutral medium to simulations, we find that shocks moving into turbulence on the scale of superbubbles can generate compressive flows on the order of 103 M⊙ Myr–1. Our results also show good agreement with related studies on turbulent fluctuations generated by shocks in pure fluid mechanics.
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