Influence analysis on grid scale limiter of XY-SAS model
-
摘要: XY-SAS(Xu & Yan Scale Adaptive Simulation)模型通过在SA(Spalart-Allmaras)模型耗散项的湍流尺度中引入基于平均涡量的冯卡门长度尺度,在不稳定流动区域具有类似LES(Large Eddy Simulation)的计算性能,且不存在DES(Detached Eddy Simulation)方法中RANS(Reynolds Averaged Navier-Stokes)与LES的交界面问题.由于SAS类模型预测的湍流能谱存在高波数衰减不足的缺陷,需要进一步在湍流尺度中引入网格尺度作为限制器.采用不同形式的网格尺度限制器构造了3种XY-SAS模型,对Re=3 900的圆柱绕流进行数值模拟,并与DES及实验数据进行比较.结果表明网格尺度限制器对XY-SAS模型的计算性能有较大影响,以最小网格间距作为高波数衰减限制器是较为合理的选择,此时模型对于大分离流动能够达到DES的模拟能力.Abstract: The Xu & Yan scale adaptive simulation (XY-SAS) model is based on the introduction of the von Karman length scale into the destruction term of spalart-allmaras (SA) turbulence model, which results in a large eddy simulation (LES)-like behavior in unsteady regions of the flowfield without explicit grid dependence. Because the SAS models could not provide sufficient damping of the smallest scales, the grid spacing was introduced as the high wave number damping limitation. Three different XY-SAS models were constructed by using various grid limiters and were tested by the numerical example of circular cylinder at Re=3 900. The numerical results were compared with detached eddy simulation (DES) and experimental data. It is concluded that, the grid limiter has a strong influence on the performance of the model and the minimum grid spacing is a good limitation, under which the XY-SAS model performs as well as DES method.
-
Key words:
- XY-SAS model /
- von Karman length scale /
- grid spacing /
- turbulence model /
- separation flow
-
[1] Fröhlich J,von Teryi D.Hybrid LES/RANS methods for the simulation of turbulent flows[J].Progress in Aerospace Sciences,2008,44(5):349-377 [2] 阎超,于剑,徐晶磊,等.CFD模拟方法的发展成就与展望[J].力学进展,2011,41(5):562-589 Yan Chao,Yu Jian,Xu Jinglei,et al.On the achievements and prospects for the methods of computational fluid dynamics[J].Advance in Mechanics,2011,41(5):562-589(in Chinese) [3] Menter F R,Kuntz M,Bender R.A scale-adaptive simulation model for turbulent flow predictions[C]//41st Aerospace Sciences Meeting and Exhibit.Reston,VA:American Institute of Aeronautics and Astronautics Inc,2003-0767 [4] Menter F R,Egorov Y.A scale-adaptive simulation model using two-equation models[C]//43rd AIAA Aerospace Sciences Meeting and Exhibit.Reston,VA:American Institute of Aeronautics and Astronautics Inc,2005:271-283 [5] Menter F R,Egorov Y.The scale-adaptive simulation method for unsteady turbulent flow predictions.Part 1:theory and model description[J].Flow,Turbulence and Combustion,2010,85(1):113-138 [6] Egorov Y,Menter F R,Lechner R,et al.The scale-adaptive simulation method for unsteady turbulent flow predictions.Part 2:application to complex flows[J].Flow,Turbulence and Combustion,2010,85(1):139-165 [7] Menter F R,Schütze J,Kurbatskii K A,et al.Scale-resolving simulation techniques in industrial CFD[C]//6th AIAA Theoretical Fluid Mechanics Conference.Reston,VA:American Institute of Aeronautics and Astronautics Inc,2011-3474 [8] Menter F R.Review of the shear-stress transport turbulence model experience from an industrial perspective[J].International Journal of Computational Fluid Dynamics,2009,23(4):305-316 [9] 徐晶磊,阎超.一个一方程Scale-Adaptive Simulation模型的构造[C]//第14届全国计算流体力学会议.贵阳:[s.n.],2009:113-117 Xu Jinglei,Yan Chao.A one-equation scale-adaptive simulation model[C]//14th National Conference on CFD.Guiyang:[s.n. ],2009:113-117(in Chinese) [10] Spalart P R,Allmaras S R.A one-equation turbulence model for aerodynamic flows[C]//30th AIAA Aerospace Sciences Meeting and Exhibit.Reno,NV:American Institute of Aeronautics and Astronautics Inc,1992-0439 [11] 高瑞泽,徐晶磊,赵瑞,等.XY-SAS模型对分离流动的性能分析[J].北京航空航天大学学报,2010,36(4):414-418 Gao Ruize,Xu Jinglei,Zhao Rui,et al.Evaluation of XY-SAS model for separated flows[J].Journal of Beijing University of Aeronautics and Astronautics,2010,36(4):414-418(in Chinese) [12] Xu J L,Hu N,Gao G.A high-fidelity turbulence length scale for flow simulation[C]//Progress in Hybrid RANS-LES Modelling.Berlin:Springer,2012:141-145 [13] Ong L,Wallace J.The velocity field of the turbulent very near wake of a circular cylinder[J].Exp Fluids,1996,20(6):441-453 [14] Kravchenko A G,Moin P.Numerical studies of flow over a circular cylinder at ReD=3 900[J].Phys Fluids,2000,12(12):403-417 [15] Shim Y M,Sharma R N,Richards P J.Numerical study of the flow over a circular cylinder in the near wake at Reynolds number 3 900[C]//39th AIAA Fluid Dynamics Conference.Reston,VA:American Institute of Aeronautics and Astronautics Inc,2009-4160
点击查看大图
计量
- 文章访问数: 1050
- HTML全文浏览量: 93
- PDF下载量: 627
- 被引次数: 0