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DETACHED-EDDY SIMULATION: CURRENT STATUS AND PERSPECTIVES

机译:Detached-Eddy Simulation:当前状态和透视

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Detached-Eddy Simulation (DES) is a hybrid technique proposed in 1997 as a numerically feasible and plausibly accurate approach for predicting massively separated flows. Since its inception the method has been applied to a range of configurations including simple shapes such as cylinders, spheres and aircraft forebodies, in addition to complex geometries including fighter aircraft. The accuracy of DES predictions has typically been far superior to that of steady or unsteady Reynolds-averaged Navier-Stokes methods while at the same time avoiding the Reynolds-number limitations that plague Large-Eddy Simulation. Based on research performed to date, the method appears sound and responds well to the type of boundary layer separation (i.e., laminar or turbulent), and to grid refinement. However, it is possible to degrade predictions using a grid density that is both too fine for RANS and too coarse for LES. Examples of applications of the technique are presented, along with a summary of some of the important findings and directions for future research.
机译:分离涡流仿真(DES)是一种1997年提出的混合技术,作为预测大规模分离流的数值可行和合理的准确方法。由于其成立,该方法已经应用于一系列配置,包括简单的形状,例如汽缸,球体和飞机的前缘,除了包括战斗机的复杂几何形状之外。 DES预测的准确性通常远远优于稳定或不稳定的雷诺斯平均天维的Navier-Stokes方法,同时避免扰乱大涡模拟的雷诺数限制。基于迄今为止执行的研究,该方法出现了声音并响应边界层分离的类型(即,层流或湍流),以及网格精制。然而,可以使用栅格密度来降低预测,该网格密度对于Rans而言过于良好并且对于LES而言过于粗糙。提出了该技术的应用的示例,以及一些重要研究结果和未来研究的方向的摘要。

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