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arXiv 2308.03428math.NAcs.NAphysics.flu-dyn
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强激波捕捉方法的数值稳定性分析 II:高阶有限体积格式

Numerical stability analysis of shock-capturing methods for strong shocks II: high-order finite-volume schemes

Weijie Ren, Wenjia Xie, Ye Zhang, Hang Yu, Zhengyu Tian

AI总结:

本文首次建立五阶有限体积 WENO 格式的矩阵稳定性分析方法,揭示高空间精度导致激波不稳定,并指出横向耗散和激波结构内点数对稳定捕捉强激波的关键作用。

摘要:

激波不稳定问题通常出现在涉及强激波的流动模拟中,尤其是在采用高阶格式时,这限制了它们在超声速/高超声速流动模拟中的应用。本研究重点探索五阶有限体积 WENO 格式中激波不稳定性的数值特性和内在机制。为此,我们首次建立了适用于五阶格式的矩阵稳定性分析方法。通过预测指数增长阶段扰动误差的演化,该方法为激波捕捉行为提供了定量认识,并有助于阐明导致激波不稳定的机制。结果表明,即使是有耗散的求解器,当空间精度提高到五阶时也会遭受激波不稳定问题。进一步研究表明,这是由于 WENO 格式在数值激波结构附近具有过高的空间精度所致。此外,五阶格式的激波不稳定问题被证明是一个多维耦合问题。为了稳定地捕捉强激波,关键在于横向面上具有足够的耗散,并确保在垂直于激波方向的数值激波结构内至少有两个点。矩阵稳定性分析方法还明确了不稳定性的来源位置,揭示不稳定性源于数值激波结构。另外,稳定性分析表明,局部特征分解有助于缓解高阶格式中的激波不稳定性,尽管不稳定性仍然存在。这些结论为更好地理解五阶格式中的激波不稳定性铺平了道路,并为发展适用于高马赫数可压缩流动的更可靠的高阶激波捕捉方法提供了指导。

英文摘要:

The shock instability problem commonly arises in flow simulations involving strong shocks, particularly when employing high-order schemes, limiting their applications in hypersonic flow simulations. This study focuses on exploring the numerical characteristics and underlying mechanisms of shock instabilities in fifth-order finite-volume WENO schemes. To this end, for the first time, we have established the matrix stability analysis method for the fifth-order scheme. By predicting the evolution of perturbation errors in the exponential growth stage, this method provides quantitative insights into the behavior of shock-capturing and helps elucidate the mechanisms that cause shock instabilities. Results reveal that even dissipative solvers also suffer from shock instabilities when the spatial accuracy is increased to fifth-order. Further investigation indicates that this is due to the excessively high spatial accuracy of the WENO scheme near the numerical shock structure. Moreover, the shock instability problem of fifth-order schemes is demonstrated to be a multidimensional coupling problem. To stably capture strong shocks, it is crucial to have sufficient dissipation on transverse faces and ensure at least two points within the numerical shock structure in the direction perpendicular to the shock. The source location of instability is also clarified by the matrix stability analysis method, revealing that the instability arises from the numerical shock structure. Additionally, stability analysis demonstrates that local characteristic decomposition helps mitigate shock instabilities in high-order schemes, although the instability still persists. These conclusions pave the way for a better understanding of the shock instability in fifth-order schemes and provide guidance for the development of more reliable high-order shock-capturing methods for compressible flows with high Mach numbers.

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