A low Reynolds number variant of partially-averaged Navier-Stokes model for turbulence

被引:49
|
作者
Ma, J. M. [1 ,2 ]
Peng, S. -H. [1 ,3 ]
Davidson, L. [1 ]
Wang, F. J. [2 ]
机构
[1] Chalmers, Dept Appl Mech, SE-41296 Gothenburg, Sweden
[2] China Agr Univ, Coll Water Conservancy & Civil Engn, Beijing 100094, Peoples R China
[3] Swedish Def Res Agcy FOI, Dept Aeronaut & Syst Technol, SE-16940 Stockholm, Sweden
基金
中国国家自然科学基金;
关键词
Low Reynolds number model; Near-wall behavior; Turbulent flow; BOUNDARY-LAYER FLOWS; HEAT-TRANSFER; SIMULATION; CHANNEL;
D O I
10.1016/j.ijheatfluidflow.2011.02.001
中图分类号
O414.1 [热力学];
学科分类号
摘要
A low Reynolds number (LRN) formulation based on the Partially Averaged Navier-Stokes (PANS) modelling method is presented, which incorporates improved asymptotic representation in near-wall turbulence modelling. The effect of near-wall viscous damping can thus be better accounted for in simulations of wall-bounded turbulent flows. The proposed LRN PANS model uses an LRN k-epsilon model as the base model and introduces directly its model functions into the PANS formulation. As a result, the inappropriate wall-limiting behavior inherent in the original PANS model is corrected. An interesting feature of the PANS model is that the turbulent Prandtl numbers in the k and epsilon equations are modified compared to the base model. It is found that this modification has a significant effect on the modelled turbulence. The proposed LRN PANS model is scrutinized in computations of decaying grid turbulence, turbulent channel flow and periodic hill flow, of which the latter has been computed at two different Reynolds numbers of Re = 10,600 and 37,000. In comparison with available DNS, LES or experimental data, the LRN PANS model produces improved predictions over the standard PANS model, particularly in the near-wall region and for resolved turbulence statistics. Furthermore, the LRN PANS model gives similar or better results - at a reduced CPU time - as compared to the Dynamic Smagorinsky model. (C) 2011 Elsevier Inc. All rights reserved.
引用
收藏
页码:652 / 669
页数:18
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