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LES/RANS方法混合函数特性研究 被引量:1

PARAMETRIC STUDY ON THE BLENDING FUNCTION IN TRANSITION ZONE OF THE LES/RANS METHOD
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摘要 将两方程k-ωSST湍流模型和Sagaut的混合尺度亚格子模型通过一个混合函数相结合,构造出一种混合大涡/雷诺平均N-S方程模拟方法(hybird large eddy simulation/reynolds-averaged navier-stokes,HybridLES/RANS),采用这种混合模拟方法结合5阶WENO格式对Ma=2.8平板湍流边界层进行了数值模拟,并在计算区域上游入口处采用"回收/调节"方法生成湍流脉动边界条件,通过考查RANS区域向LES区域的过渡参数及网格分辨率对这种混合模拟方法进行了评价.计算结果表明:该文采用的混合模拟方法可以捕捉到湍流边界层中的大尺度结构且入口边界层平均参数不会发生漂移,混合函数应当将RANS区域和LES区域的过渡点设置在对数律层和尾迹律层的交界处,而过渡应当迅速以获得正确的雷诺剪切应力分布,在该文采用的模型及数值方法的条件下,流向及展向的网格小至与Escudier混合长相当时,能够获得可以接受的脉动速度的单点-二阶统计值. Two-equation k-ω SST turbulence model was combined with Sagaut's mixed-length subgrid-scale model with a blending function to construct a hybrid large-eddy/Reynolds-averaged Navier-Stokes method. The method was used to compute a plate turbulent boundary layer at Mach number 2.8 with fifth-order WENO scheme. A recycling/rescaling method was used to generate and sustain turbulent fluctuations at the inlet. The RANS to LES transition parameters and mesh resolution were considered in order to assess the method. The results showed that the hybrid method could capture the large-scale structure in the turbulent boundary-layer and no shift of the inlet mean parameters was observed. The blending function should be designed to transition to LES toward the outer part of the logarithmic region and the transition should be sharp to obtain the correct Reynolds shear stress. Single point-second order velocity fluctuations statistics might be obtained and accepted on streamwise and spanwise meshes scaled by Escudier mixing length.
出处 《力学学报》 EI CSCD 北大核心 2012年第3期487-493,共7页 Chinese Journal of Theoretical and Applied Mechanics
基金 国家自然科学基金资助项目(10802096)~~
关键词 混合大涡/雷诺平均N-S方程模拟方法 WENO格式 湍流边界层 “回收/调节”方法 混合函数 hybird large-eddy/Reynolds-averaged Navier-Stokes method, WENO scheme, turbulent boundarylayer, "recycling/rescaling" method, blending function
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参考文献21

  • 1Georgiadis N J, Rizzetta DP, Fureby C. Large eddy sim- ulation: current capabilities, recommended practices and future research. AIAA Journal, 2010, 48(8): 1772-1784.
  • 2Georgiadis N J, Iwan J, Alexander D, et al. Hybrid Reynolds-averaged Navier-Stokes/Large eddy simulation simulations of supersonic turbulent mixing. AIAA Jour- nal, 2003, 41(2): 218-229.
  • 3Schluter JU, Pitsch H, Moin P. Large eddy simulation in- flow conditions for coupling with Reynolds-averaged flow solvers. AIAA Journal, 2004, 42(3): 478-484.
  • 4Spalart PR, Jou WH, Strelets M, et al. Comments on the feasibility for wings and on a hybrid RANS/LES ap- proach. In: Proceeding of First AFOSR International Conf on DNS/LES, 1997.
  • 5Strelets M. Detached eddy simulation of massively sepa- rated flows. AIAA 2001-2306, 2001.
  • 6Fan CC, Xiao XD, Edwards JR, et al. Hybrid Large eddy/ Reynolds-averaged Navier-Stokes simulation of shock- separated flows. Journal of Spacecraft and Rockets, 2004, 41(6): 897-906.
  • 7孙明波,梁剑寒,王振国.二维凹腔超声速流动的混合RANS/LES模拟[J].推进技术,2006,27(2):119-123. 被引量:10
  • 8孙明波,梁剑寒,王振国.超声速来流横向狭缝喷流标量输运的混合RANS/LES模拟[J].力学季刊,2007,28(3):395-399. 被引量:4
  • 9范周琴,孙明波,刘卫东.支板喷射超声速燃烧流场三维大涡模拟[J].国防科技大学学报,2011,33(1):1-6. 被引量:7
  • 10Choi JI, Edwards JR, Baurle RA. Compressible boundary- layer predictions at high-reynolds number using hybrid LES/RANS method. AIAA Journal, 2009, 47(9): 2179- 2193.

二级参考文献31

  • 1杨武兵,张会强,王希麟,郭印诚,林文漪.空间发展平板混和层流动的大涡模拟-3D与2D模拟的比较[J].工程热物理学报,2004,25(6):1046-1048. 被引量:3
  • 2Swaminathan N, Bilger R W. Assessment of Combustion Submodels for Turbulent Nonprenixed Hydrocarbon names [J]. Combustion and Flame, 1998, 116 (4):519-545.
  • 3Swaminathan N, Bilger R W. Comment and Reply on the "Assessment of Computation Submodels for Turbulent Non-premixed Hydrocarbon flames" [J]. Combustion and Flame, 1999, 116:675 - 677.
  • 4Waidmann W, Alff F, Bǒam M, et al. Supersonic Combustion of Hydrogen/air in a SCRAMJET Combustion Chamber [ J ]. Space Technology, 1995, 15 (6): 421-429.
  • 5Oevermann M. Numerical Investigation of Turbulent Hydrogen Combustion in Ascramjet Using Flame-let Modeling [J]. Aerospace Science and Technology,2004,4:463 - 480.
  • 6Shu C W. High Order ENO and WENO Schemes for Computational Fluid Dynamics [ C ]//High-Order Methods for Computational Physics, 1999.
  • 7Shu C W.High order ENO and WENO schemes for computational fluid dynamics [ A ].In Barth T J,Deconinck H,editors,High-Order Methods for Computational Physics[ M].Springer-Verlag,1999:439 ~ 582.
  • 8Shu C W,Osher S.Efficient implementation of essentially non-oscillatory shock-capturing schemes Ⅱ[J].Journal of Computational Physics,1989,83 (1):32 ~ 87.
  • 9Gruber M R,Baurle R A.Fundamental studies of cavitybased flameholder concepts for supersonic combustors[ J].Journal of Propulsion and Power,2001,17 (1):146~ 153.
  • 10Settles G S,Williams D R.Reattachment of a compressible turbulent free shear layer[ J].AIAA Journal,1982,20(1):60 ~67.

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