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首页> 外文期刊>International Journal for Numerical Methods in Fluids >RESEARCH PAPER PRESENTED AT ANADE 2013: ADVANCES IN NUMERICAL AND ANALYTICAL TOOLS FOR DETACHED FLOW PREDICTION
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RESEARCH PAPER PRESENTED AT ANADE 2013: ADVANCES IN NUMERICAL AND ANALYTICAL TOOLS FOR DETACHED FLOW PREDICTION

机译:于2013年ANADE上发表的研究论文:分离流动预测的数值和分析工具的发展

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摘要

In this paper, we investigate the accuracy and efficiency of discontinuous Galerkin spectral method simulations of under-resolved transitional and turbulent flows at moderate Reynolds numbers, where the accurate prediction of closely coupled laminar regions, transition and developed turbulence presents a great challenge to large eddy simulation modelling. We take full advantage of the low numerical errors and associated superior scale resolving capabilities of high-order spectral methods by using high-order ansatz functions up to 12th order. We employ polynomial de-aliasing techniques to prevent instabilities arising from inexact quadrature of nonlinearities. Without the need for any additional filtering, explicit or implicit modelling, or artificial dissipation, our high-order schemes capture the turbulent flow at the considered Reynolds number range very well. Three classical large eddy simulation benchmark problems are considered: a circular cylinder flow at Re-D=3900, a confined periodic hill flow at Re-h=2800 and the transitional flow over a SD7003 airfoil at Re-c=60,000. For all computations, the total number of degrees of freedom used for the discontinuous Galerkin spectral method simulations is chosen to be equal or considerably less than the reported data in literature. In all three cases, we achieve an equal or better match to direct numerical simulation results, compared with other schemes of lower order with explicitly or implicitly added subgrid scale models. Copyright (c) 2014 John Wiley & Sons, Ltd.
机译:在本文中,我们研究了在中等雷诺数下欠解析的过渡流和湍流的不连续Galerkin谱方法模拟的准确性和效率,其中紧密耦合的层流区域,过渡和发展湍流的精确预测对大涡流提出了巨大挑战仿真建模。通过使用高达12阶的高阶ansatz函数,我们充分利用了高阶谱方法的低数值误差和相关的出色的尺度解析能力。我们采用多项式去混叠技术来防止由于非线性的不精确正交引起的不稳定性。不需要任何额外的滤波,显式或隐式建模或人工耗散,我们的高阶方案可以很好地捕获在考虑的雷诺数范围内的湍流。考虑了三个经典的大涡模拟基准问题:在Re-D = 3900时的圆柱流,在Re-h = 2800时的受限周期性坡面流以及在Re-c = 60,000时通过SD7003机翼的过渡流。对于所有计算,用于不连续Galerkin光谱方法模拟的自由度总数选择为等于或大大小于文献中报道的数据。与使用显式或隐式添加子网格比例模型的其他低阶方案相比,在这三种情况下,我们都能获得与直接数值模拟结果相同或更好的匹配。版权所有(c)2014 John Wiley&Sons,Ltd.

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