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Large-eddy simulations of flow past a square cylinder using structured and unstructured grids

机译:使用结构化和非结构化网格的流经方圆柱体的大涡模拟

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The flow past a square cylinder at Re = 2.2 x 10(4) is analyzed by large-eddy simulation (LES) using the fine grids in order to represent details of near-cylinder flows. The accuracy of LES on structured and unstructured grids is assessed from the engineering viewpoint, compared with previous studies. The finite differencing method code with 4th order central scheme for the convective term is used for structured LES, while the open-source finite volume method code (OpenFOAM 2.3.0) with 1st-2nd order schemes is applied for unstructured LES. Typical schemes in OpenFOAM are tested, i.e., "LUST" (blending of linear and linear upwind schemes), "limitedLinear" (TVD) and "linearUpwind" (linear upwind). In this study, three effects are emphasized: numerical schemes for convective terms, meshing strategies, and spanwise resolution and length. On the whole, OpenFOAM can obtain fairly accurate prediction of the time-averaged and r.m.s quantities no matter which numerical scheme is used. "LUST" and "linearUpwind" are suggested. Meshing refinement in wake can be a solution to improve the far-wake velocity distribution and to overcome the earlier energy decay of turbulent motions in the inertial subrange caused by artificial dissipation. Different degrees of instantaneous flow reattachment near the trailing edges are found in the results obtained by OpenFOAM. Flow reattachment is closely associated with the roll-up of shear layer, and the flow topology between the shear layer and the side wall featured by the frontal and leeward secondary vortex. In this regard, the refinement of hexahedra cells near cylinder gives a best solution among all present cases tested compared with the previous DNS result. Generally the Kelvin-Helmholtz instability can be accurately predicted by OpenFOAM under the present numerical conditions. In addition, the spanwise resolution seems no big effect in predicted results when less than 0.05D. By contrast, the increase in spanwise length to 14D from 4D plays an important role in obtaining reasonable spanwise correlation of pressure and consequently the overall fluctuating lifts. (C) 2016 Elsevier Ltd. All rights reserved.
机译:通过大涡流仿真(LES)使用细网格对流经Re = 2.2 x 10(4)的方筒的流动进行分析,以表示近筒流动的细节。与以前的研究相比,从工程角度评估了结构化和非结构化网格上LES的准确性。对流项具有四阶中心方案的有限差分方法代码用于结构化LES,而具有一阶至二阶方案的开源有限体积方法代码(OpenFOAM 2.3.0)适用于非结构化LES。测试了OpenFOAM中的典型方案,即“ LUST”(线性和线性迎风方案的混合),“ limitedLinear”(TVD)和“ linearUpwind”(线性迎风)。在这项研究中,强调了三种影响:对流项的数值方案,网格划分策略以及翼展方向的分辨率和长度。总体而言,无论使用哪种数值方式,OpenFOAM都能获得相当准确的时间平均量和均方根量预测。建议使用“ LUST”和“ linearUpwind”。尾流中的网格细化可以是一种改善远尾速度分布并克服由人工耗散引起的惯性子范围内湍流运动的早期能量衰减的解决方案。在OpenFOAM获得的结果中,发现后缘附近有不同程度的瞬时流量重新附着。流动的重新附着与剪切层的卷起以及剪切层与侧壁之间的流动拓扑密切相关,其特征在于前涡流和背风次涡。在这方面,与以前的DNS结果相比,在圆柱体附近对六面体细胞的细化提供了所有当前测试案例中的最佳解决方案。通常,在当前数值条件下,OpenFOAM可以准确预测开尔文-亥姆霍兹不稳定性。此外,当小于0.05D时,跨度分辨率似乎对预测结果没有太大影响。相比之下,将翼展方向长度从4D增加到14D在获得合理的翼展方向相关压力以及因此总体波动升程方面起着重要作用。 (C)2016 Elsevier Ltd.保留所有权利。

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