用于可压缩壁面湍流LES及DNS入口边界条件的“回收-调节”方法综述

刘卫东; 陈逖; 孙明波; 范晓樯; 梁剑寒

用于可压缩壁面湍流LES及DNS入口边界条件的“回收-调节”方法综述

国防科学技术大学航天与材料工程学院,长沙 410073

基金项目: 国家自然科学基金(10802096)

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- 文章访问数: 1928
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- 被引次数: 0
出版历程
- 收稿日期: 2010-02-14
- 修回日期: 2010-04-22
- 刊出日期: 2011-03-28

Overview of recycling-rescaling method for inflow boundary conditions of LES and DNS of compressible wall bounded turbulent flows

College of Aerospace and Materials Engineering, National University of Defense Technology,Changsha 410073,China

摘要

摘要: 为了减小湍流流动问题的大涡模拟和直接数值模拟的入口湍流脉动边界条件对计算结果的影响,叙述了用于可压缩壁面湍流入口脉动生成的一种方法——“回收-调节”方法(recycling-rescaling method),叙述了这种方法的理论基础及简要推导过程,介绍了几种常用的“回收-调节”方法并指出了实现中的几个关键问题,分析了这种方法中存在的不足并对其应用进行了总结评述.该方法可为湍流、燃烧问题的大涡模拟和直接数值模拟方法的发展提供参考.
- 大涡模拟 /
- 直接数值模拟 /
- 可压缩壁面湍流 /
- 入口脉动生成 /
- “回收-调节”方法
Abstract: The inflow turbulent fluctuating boundary conditions play a key role in large eddy or direct numerical simulations of many turbulent problems.This paper introduced a method — recycling-rescaling method for inflow fluctuation generation of compressible wall bounded turbulent flows.The theory foundation and deduction of the method were given in the paper.Several recycling-rescaling methods were introduced and some key points in the implementation were indicated.Applications were summarized and limitations were discussed.This paper can be a reference for further investigation in LES (large eddy simulation) and DNS (direct numerical simulation) of turbulent flow and combustion problems.
- large eddy simulation /
- direct numerical simulation /

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参考文献(21)

[1]	Klein M,Sadiki A,Janicka J.Influence of the boundary conditions on the direct numerical simulation of a plane turbulent jet //The 2nd International Symposium on Turbulence and Shear Flow Phenomena,TSFP2.Stockholm,Sweden: ,2001,1:401-406.
[2]	Stanley S A,Sarkar S.Influence of nozzle conditions and discrete forcing on turbulent plane jets[J].AIAA Journal,2000,38(9):1615-1623.
[3]	Klein M,Sadiki A,Janicka J.Influence of the inflow conditions of primary breakup of liquid jets //ILASS-Europe,Annual Conference on Liquid Atomization and Spray System.Zurich,Switzerland: ,2001:475-480.
[4]	Lund T S,Squires K D,Wu X H.Turbulent inflow boundary conditions for LES .AIAA Paper 2003-0067,2003.
[5]	Sagaut P,Garnier E,Tromeur E,et al.Turbulent inflow conditions for large-eddy simulation of compressible wall-bounded flows[J].AIAA Journal,2004,42(3):469-477.
[6]	Lee S,Lele S K,Moin P.Simulation of spatially evolving turbulence and the applicability of Taylor's hypothesis in compressible flow[J].Physics of Fluids,1992,4(7):1521-1530.
[7]	Le H,Moin P,Kim J.Direct numerical simulation of turbulent flow over a backward-facing step[J].Journal of Fluid Mechanics,1997,330:349-374.
[8]	Smits A J,Dussauge J P.Turbulent shear layers in supersonic flow[M].New York:American Institute of Physics,1996.
[9]	Van Driest E R.Turbulent boundary layers in compressible fluids[J].Journal of the Aeronautical Sciences,1951,18(3):145-160,216.
[10]	Walz A.Boundary layers of flow and temperature[M].Massachusetts:MIT Press,1969.
[11]	Dassauge J P,Gaviglio J.The rapid expansion of a supersonic turbulent flow:role of bulk dilatation[J].Journal of Fluid Mechanics,1987,174:81-112.
[12]	Bradshaw P.Compressible turbulent shear layers[J].Annual Review of Fluid Mechanics,1977,9:33-54.
[13]	Lund T S,Wu X H,Squires K D.Generation of turbulent inflow data for spatially-developing boundary layer simulations[J].Journal of Computational Physics,1998,140(2):233-258.
[14]	Urbin G,Knight D.Large eddy simulation of a supersonic boundary layer using an unstructured grid[J].AIAA Journal,2001,39(7):1288-1295.
[15]	Stolz S,Adams N A.Large-eddy simulation of high-Reynolds-number supersonic boundary layers using the approximate deconvolution model and a rescaling and recycling technique[J].Physics of Fluids,2003,15(8):2398-2412.
[16]	Xiao X D,Edwards J R,Hassan H A,et al.Inflow boundary conditions for hybrid large-eddy/Reynolds-averaged Navier-Stokes simulations[J].AIAA Journal,2003,41(8):1481-1489.
[17]	Fan C C,Xiao X,Edwards J R,et al.Hybrid large-eddy/Reynolds-averaged Navier-Stokes simulations of shock-separated flows[J].Journal of Spacecraft and Rockets,2004,41(6):897-906.
[18]	Norris J W,Edwards J R.Large-eddy simulation of high-speed,turbulent diffusion flames with detailed chemistry .AIAA Paper 1997-0370,1997.
[19]	Xu S,Martin M P.Assessment of inflow boundary conditions for compressible turbulent layers[J].Physics of Fluids,2004,16(7):2623-2639.
[20]	Edwards J R,Choi J,Boles J A.Large-eddy/Reynolds-averaged Navier-Stokes simulation of a Mach 5 compression corner interaction[J].AIAA Journal,2008,46(4):977-991.
[21]	Bohr E,Bailon-Cuba J,Jansen K,et al.Inflow generation technique of large eddy simulation using equilibrium similarity analysis .AIAA Paper 2005-4672,2005.