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Spatial-temporal patterns of three-dimensional subsonic turbulent cavity flow

机译:三维亚音速湍流腔流的时空分布

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摘要

Three-dimensional, high Reynolds number cavity flow is investigated. The cavity was exposed to a free-stream Mach number of 0.40 and a Reynolds number (based on cavity depth) of 1.6 x 10(6) with a thick incoming turbulent boundary-layer. Dominant modes and structures were studied by conducting unsteady numerical flow simulations (CFD), and applying Proper-Orthogonal-Decomposition (POD) in both two and three-dimensions. Fully three-dimensional POD analysis of cavity flow has been rarely conducted in other studies, and it is demonstrated that two-dimensional POD analysis is valid in order to emphasize patterns which are limited in space, but could be misleading without the comparison with the three-dimensional POD analysis. The analysis sheds new light on three-dimensional cavity flow by disclosing novel non-intuitive dominant structures and modes. Stretched streamwise vortices were found to be dominant, at least as the spanwise structures that originate from the classical two-dimensional shear-layer instability. Furthermore, the effect of symmetry plane assumption, which is usually disregarded, was studied rigorously for the first time. POD decomposition of symmetric and anti-symmetric flow modes revealed that anti-symmetric modes contain a significant portion of the total energy; however, they only interact weakly with the symmetric modes.
机译:研究了三维高雷诺数腔流动。空腔暴露于自由流的马赫数为0.40,雷诺数(基于空腔深度)为1.6 x 10(6),且进入的湍流边界层较厚。通过进行非稳态数值流模拟(CFD),并在二维和三维中应用适当的正交分解(POD),研究了主导模式和结构。在其他研究中,很少对空腔流动进行全三维POD分析,并且证明了二维POD分析对于强调空间受限的模式是有效的,但如果不与这三个模型进行比较,可能会产生误导POD分析。通过揭示新颖的非直觉主导结构和模式,该分析为三维空腔流动提供了新的思路。已发现拉伸流向涡流是主要的,至少是因为源自经典二维剪切层不稳定性的翼展向结构。此外,首次严格地研究了通常忽略的对称平面假设的影响。对称和反对称流动模式的POD分解表明,反对称模式包含了总能量的很大一部分;但是,它们仅与对称模式相互作用。

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