首页> 外文期刊>International Journal for Numerical Methods in Fluids >An algebraic variational multiscale-multigrid method for large-eddy simulation of turbulent pulsatile flows in complex geometries with detailed insight into pulmonary airway flow
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An algebraic variational multiscale-multigrid method for large-eddy simulation of turbulent pulsatile flows in complex geometries with detailed insight into pulmonary airway flow

机译:代数变分多尺度多网格方法,用于复杂几何中湍流脉动流的大涡模拟,并深入了解肺气道流

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摘要

The algebraic variational multiscale-multigrid method, an advanced computational approach recently proposed for large-eddy simulation of turbulent flow, is further developed in this study for turbulent flow simulations in complex geometries. In particular, it is applied to the complex case of pulsatile turbulent flow dynamics of the upper and lower pulmonary airways up to generation 7 and carefully investigated for this important application. Among other things, the results obtained with the proposed method are compared with the results obtained with a rather traditional stabilized finite element method. As opposed to previous large-eddy simulations of pulmonary airways, we consider a pulsatile inflow condition, allowing the development of turbulence over a pulse cycle to be investigated, which obviously makes these results more physiologically realistic. Our results suggest that turbulent effects in the bronchial airways are rather weak and can completely decay as early as the third generation, depending on geometry and flow distribution. Both methods utilized in this study are able to adequately capture all flow stages from laminar via transitional to turbulent regimes without any modifications. However, the algebraic variational multiscale-multigrid method provides superior results as soon as the flow enters the most challenging, turbulent flow regime. Furthermore, the robustness of the scale-separation approach based on plain aggregation algebraic multigrid inherent to the algebraic variational multiscale-multigrid method is demonstrated for the present complex geometry.
机译:代数变分多尺度多重网格方法是最近提出的用于湍流大涡模拟的一种先进的计算方法,它在本研究中被进一步开发用于复杂几何形状的湍流模拟。特别是,它适用于直到第7代的上,下肺气道脉动湍流动力学的复杂情况,并针对这一重要应用进行了仔细研究。除其他事项外,将通过拟议方法获得的结果与通过相当传统的稳定有限元方法获得的结果进行比较。与以前的肺气道大涡模拟相反,我们考虑了脉动性流入情况,可以研究脉动周期内湍流的发展,这显然使这些结果在生理上更加现实。我们的结果表明,支气管气道中的湍流效应相当弱,并可能在第三代之前完全衰减,具体取决于几何形状和流量分布。在这项研究中使用的两种方法都能够在不做任何修改的情况下,充分捕获从层流到过渡状态到湍流状态的所有流动阶段。但是,一旦流体进入最具挑战性的湍流状态,代数变分多尺度多重网格方法将提供优异的结果。此外,对于当前的复杂几何,证明了基于代数变分多尺度-多重网格方法固有的平原聚合代数多重网格的尺度分离方法的鲁棒性。

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