物理
层流
湍流模型
边界层
统计物理学
大涡模拟
机械
层流下层
比例模型
明渠流量
直接数值模拟
流动分离
比例(比率)
湍流
雷诺数
流量(数学)
航空航天工程
工程类
量子力学
作者
Massimo Germano,Ugo Piomelli,Parviz Moin,W. Cabot
出处
期刊:Physics of fluids
[American Institute of Physics]
日期:1991-07-01
卷期号:3 (7): 1760-1765
被引量:6952
摘要
One major drawback of the eddy viscosity subgrid-scale stress models used in large-eddy simulations is their inability to represent correctly with a single universal constant different turbulent fields in rotating or sheared flows, near solid walls, or in transitional regimes. In the present work a new eddy viscosity model is presented which alleviates many of these drawbacks. The model coefficient is computed dynamically as the calculation progresses rather than input a priori. The model is based on an algebraic identity between the subgrid-scale stresses at two different filtered levels and the resolved turbulent stresses. The subgrid-scale stresses obtained using the proposed model vanish in laminar flow and at a solid boundary, and have the correct asymptotic behavior in the near-wall region of a turbulent boundary layer. The results of large-eddy simulations of transitional and turbulent channel flow that use the proposed model are in good agreement with the direct simulation data.
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