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APPLICATION OF A HYBRID RANS-LES METHOD TO FREE SHEAR LAYERS

机译:混合RANS-LES方法在自由剪切层中的应用

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This paper presents the application of the XLES (eXtra Large Eddy Simulation) method to relevant test-cases. The mixing between two boundary layers and between a wake and a boundary layer are discussed. The first test case considers the mixing layer that forms at the end of a splitting plate. Two boundary layers with different free-stream velocities flow on the upper and lower side of a flat plate and join at the trailing edge forming a free shear layer. The second test case represents a mixing between the 2-D wake originating downstream an airfoil and the 2-D boundary layer developing over a flat plate placed beneath the airfoil. This application is representative of flows over multi-element configurations where the wake coming from the slat merges with the boundary layer of the main component. The method has shown to be effective reducing the modelled turbulence and providing resolved turbulence in the regions of the field treated in LES mode. The "grey-area" issue has been highlighted. This is likely connected to the stochastic character of the model.
机译:本文介绍了XLES(超大型涡模拟)方法在相关测试用例中的应用。讨论了两个边界层之间以及尾流和边界层之间的混合。第一个测试案例考虑了在分隔板末端形成的混合层。具有不同自由流速度的两个边界层在平板的上侧和下侧流动,并在后缘汇合,形成一个自由剪切层。第二个测试案例代表了在机翼下游产生的2-D尾流与在机翼下方放置的平板上方展开的2-D边界层之间的混合。此应用程序代表多元素配置上的流,其中来自板条的尾波与主要组件的边界层合并。该方法已显示出有效地减少了建模的湍流并在以LES模式处理的场的区域中提供了解析的湍流。 “灰色区域”问题已突出显示。这很可能与模型的随机性有关。

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