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Large eddy simulation of supersonic, compressible, turbulent mixing layers

机译:超音速,可压缩湍流混合层的大涡模拟

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Two and three dimensional large eddy simulations of a spatially developing supersonic mixing layer are performed using an in-house hybrid finite volume code that combines a fourth order non-dissipative MacCormack scheme for capturing turbulence and a second order SLAU2 upwind scheme for capturing shocks and other discontinuities in the flow. Three-dimensional predictions of growth rate and statistical moments in the self similar regime are consistent with past experimental and direct numerical simulation studies. The peak values of the transverse turbulence stresses are over predicted in two dimensional simulations. This may be attributed to the lack of vortex stretching and the lack of significant energy transfer to the smaller scales. This also leads to sustenance, pairing and overall growth of large coherent structures that result in an over-prediction of growth rate by about 20%. (C) 2019 Elsevier Masson SAS. All rights reserved.
机译:使用内部混合有限体积码对空间发展的超音速混合层进行二维和三维大涡模拟,该有限体积码结合了用于捕获湍流的四阶非耗散MacCormack方案和用于捕获冲击等的二阶SLAU2迎风方案。流中的不连续性。自相似状态下的增长率和统计矩的三维预测与过去的实验和直接数值模拟研究一致。横向湍流应力的峰值在二维模拟中被过度预测。这可能归因于缺乏涡旋拉伸以及缺乏向较小尺度的明显能量转移。这还会导致大型相干结构的维持,配对和整体增长,从而导致增长率高估约20%。 (C)2019 Elsevier Masson SAS。版权所有。

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