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High Reynolds Number Large-Eddy Simulation of Free Shear Flows

机译:高雷诺数大涡流自由剪切流模拟

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Theoretical and numerical aspects of Large Eddy Simulation (LES) and Monotonically Integrated LES (MILES) are discussed in terms of the modified equations and quantified by comparing databases of homogeneous turbulence and transitional free jets. The MILES SGS models are found to be of tensorial eddy-viscosity. LES appears virtually independent of the SGS model if the resolution is fine enough to ensure that the cut-off wavenumber lies in the inertial sub-range, provided that the SGS model can adequately channel kinetic energy out of the wavenumbers close to the cut-off wavenumber to prevent aliasing.
机译:根据改进的方程,通过比较均匀湍流和过渡自由喷射的数据库来讨论大涡模拟(LES)和单调集成LES(MILGE)的理论和数值方面。发现Miles SGS模型具有姿态涡流粘度。如果分辨率足够精细,则LES几乎独立于SGS模型,以确保切断波数位于惯性子范围内,条件是SGS模型可以将动能充分地从截止截止的波兰音器Wavenumber防止别名。

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