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New numerical solver for flows at various Mach numbers

机译:用于各种马赫数流量的新型数值求解器

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摘要

Context. Many problems in stellar astrophysics feature flows at low Mach numbers. Conventional compressible hydrodynamics schemes frequently used in the field have been developed for the transonic regime and exhibit excessive numerical dissipation for these flows. Aims. While schemes were proposed that solve hydrodynamics strictly in the low Mach regime and thus restrict their applicability, we aim at developing a scheme that correctly operates in a wide range of Mach numbers. Methods. Based on an analysis of the asymptotic behavior of the Euler equations in the low Mach limit we propose a novel scheme that is able to maintain a low Mach number flow setup while retaining all effects of compressibility. This is achieved by a suitable modification of the well-known Roe solver. Results. Numerical tests demonstrate the capability of this new scheme to reproduce slow flow structures even in moderate numerical resolution. Conclusions. Our scheme provides a promising approach to a consistent multidimensional hydrodynamical treatment of astrophysical low Mach number problems such as convection, instabilities, and mixing in stellar evolution.
机译:上下文。恒星天体物理学中的许多问题都以低马赫数流动。已经为跨音速方案开发了在本领域中经常使用的常规可压缩流体力学方案,并且对于这些流动表现出过多的数值耗散。目的虽然提出了严格在低马赫数范围内解决流体动力学从而限制其适用性的方案,但我们的目标是开发一种可在广泛的马赫数范围内正确运行的方案。方法。基于对在低马赫数限制下的Euler方程的渐近行为的分析,我们提出了一种新颖的方案,该方案能够在保持所有可压缩性影响的同时保持低马赫数流动设置。这可以通过对著名的Roe解算器进行适当的修改来实现。结果。数值测试表明,即使在中等数值分辨率下,该新方案也能够重现缓慢流动的结构。结论。我们的方案为天体物理低马赫数问题(例如对流,不稳定性和恒星演化中的混合)的一致多维流体力学处理提供了一种有前途的方法。

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