应用改进的低雷诺数湍流模型预测转捩流动
Prediction of transitional flows using an improved low-Reynolds-number turbulence model with transition sensitivity
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摘要: 基于Launder-Sharma(LS)低雷诺数k-ε两方程湍流模型发展了一种改进的具有转捩敏感性的低雷诺数湍流模型.针对LS模型的可实现性(realizability)问题和前缘滞止点湍动能预测过大的不足,模型进行了改进.改进模型只使用当地物理量,不需要求解壁面距离、y+和边界层积分参数.改进模型能够适用于广泛的流动,且容易应用到通用的计算流体动力学(CFD)程序中.对具有详细数据的零压力梯度平板转捩边界层T3A实验的模拟结果显示,改进模型能够预测转捩流动,并能对自由湍流变化给出合理的响应.Abstract: The paper presented the initial development of an improved two-equation low-Reynolds-number(LRN) turbulence model with transition sensitivity,based on the Launder-Sharma(LS) turbulence model.Several modifications were made for LS model's disadvantage on realizablity and stagnation point anomaly.The improved model only uses local variables.No need of calculating wall distance,y+ and boundary layer integral parameters makes it can be used for a wide range of flows,and this feature also makes it more easily implemented into general-purpose computational fluid dynamics(CFD) codes.The numerical simulation results of T3A test,a zero pressure gradient transitional flat plate boundary layer flow experiment,with detailed experimental data shows that the improved model can predict transitional flow,including an appropriate response to freestream turbulence intensity variety.
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Key words:
- transition models /
- transitional flows /
- numerical simulation
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[1] Savill A M.Evaluating turbulence model p redictions of transition[J].Applied Scientific Research,1993,51:555-562. [2] Launder B E,Sharma B I.Application of the energy dissi-pation model of turbulence to calculation of flow near a spinning disc[J].Letters in Heat and Mass T ran sfer,1974,1:131-138. [3] Patel V C,Rodi W,Scheuerer G.Turbulence models for near-wall and low Reynolds number flows—A review[J].AIAA Journal,1984,23:1308-1319. [4] Schmidt R C,Patankar S V.Simulating boundary layer transition with low2Reynolds-number k-turbulence mod-els:Part 1—An evaluation of p rediction characteristics[J].ASME J.Turbo mach.,1991,113:10-26. [5] Suzen Y B,Huang P G.Numerical simulation of unsteady wake/blade interactions in low-pressure turbine flows u-sing an intermittency transport equation[J].ASM E J.Turbomach.,2005,127:431-444. [6] Kato M,Launder B E.The modeling of turbulent flow a-round stationary and vibrating square cylinders[C]//Proc.9t h Sympo sium on Turbulent Shear Flows.Kyoto,Japan:[s.n.],1993. [7] Moore J G,Moore J.Realizability in two-equation t urbu-lence models[C]//30th AIAA Fluid Dynamics Confer-ence.Norfolk,VA:AIAA,1999. [8] Shih T H,Liou W W,Shabbir A,et al.A new k-epsilon eddy visco sit y model for high Reynolds number turbulent flows[J].Computers Fluids,1995,24:227-238. [9] Radmehr A,Patankar S V.Computation of boundary lay-er transition using low2Reynolds-number turbulence mod-els[J].Numerical Heat Transfer,Part B:Fundamentals,2001,39:525-543. [10] Jones W P,Launder B E.The calculation of low2Reyn-olds-number phenomena with a two-equation model of turbulence[J].International Journal of Heat and Fluid Flow,1973,16:1119-1130. [11] Craft T J,Launder B E.Prediction of turbulent transi-tional phenomena with a nonlinear eddy-viscosity model[J].International Journal of Heat and Fluid Flow,1997,18:15-28. [12] 赵秋颍.叶轮机械高、低速流动的数值模拟[D].北京:北京航空航天大学,2005.ZHAO Qiuying.The numerical simulation for the high speed and the low speed flow field in turbomachinery[D].Beijing:Beijing Universit y of Aeronautics and Ast ronau-tics,2005.(in Chinese)
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