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Implicit Large Eddy Simulation of weakly-compressible turbulent channel flow

机译:弱压缩湍流通道的隐式大涡模拟

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This paper concerns the accuracy of several high-resolution and high-order finite volume schemes in Implicit Large Eddy Simulation of weakly-compressible turbulent channel flow. The main objective is to investigate the properties of numerical schemes, originally designed for compressible flows, in low Mach compressible, near-wall turbulent flows. Variants of the Monotone Upstream-centred Scheme for Conservation Laws and Weighted Essentially Non-Oscillatory schemes for orders of accuracy ranging from second to ninth order, as well as with and without low Mach corrections, have been investigated. The performance of the schemes has been assessed against incompressible Direct Numerical Simulations. Detailed comparisons of the velocity profiles, turbulent shear stresses and higher-order turbulent statistics reveal that the low Mach correction can significantly reduce the numerical dissipation of the methods in low Mach boundary layer flows. The effects of the low Mach correction have more profound impact on second and third-order schemes, but they also improve the accuracy of fifth order schemes. The ninth-order Weighted Essentially Non-Oscillatory scheme is the least dissipative scheme and it is shown that the implementation of the low Mach correction in conjunction with this scheme has a significant anti-dissipative effect that adversely affects the accuracy. Finally, the computational cost required for obtaining the improved accuracy using increasingly higher order schemes is also discussed. (C) 2015 Elsevier B.V. All rights reserved.
机译:本文涉及弱压缩湍流通道隐式大涡模拟中几种高分辨率和高阶有限体积方案的准确性。主要目的是研究低马赫数可压缩近壁湍流中最初为可压缩流设计的数值格式的性质。研究了单调上游定律的定律方案和加权基本非振荡方案的精度,其精度范围从二阶到九阶,以及有无低马赫校正。已针对不可压缩的直接数值模拟对方案的性能进行了评估。速度剖面,湍流剪切应力和高阶湍流统计数据的详细比较表明,低马赫数校正可以显着减少低马赫数边界层流中方法的数值耗散。低马赫校正的效果对二阶和三阶方案有更深远的影响,但它们也提高了五阶方案的准确性。九阶加权基本非振荡方案是耗散最少的方案,并且表明与该方案结合使用低马赫校正具有显着的消散效果,对精度产生不利影响。最后,还讨论了使用越来越高阶的方案获得提高的精度所需的计算成本。 (C)2015 Elsevier B.V.保留所有权利。

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