Prediction of vortex shedding from a circular cylinder using a volumetric Lattice-Boltzmann boundary approach

被引:0
作者
Y. Li
R. Zhang
R. Shock
H. Chen
机构
[1] Exa Corporation,
[2] 55 Network Drive,undefined
来源
The European Physical Journal Special Topics | 2009年 / 171卷
关键词
Vortex; Circular Cylinder; European Physical Journal Special Topic; Strouhal Number; Lattice Boltzmann Method;
D O I
暂无
中图分类号
学科分类号
摘要
An extended boundary scheme based on the generalized volumetric boundary algorithm for Lattice-Boltzmann method (LBM) is proposed in this paper. This approach applies a local non-equilibrium based scattering correction to the outgoing particle distributions that bounced-back from a solid surface. The correction reduces the near wall numerical smearing when enforcing the no-slip boundary condition and leads to accurate prediction of flow separations on a curved surface. A set of quantitative numerical studies of flow past a circular cylinder at low Reynolds numbers is conducted. Important flow quantities that characterize the vortex shedding phenomena behind cylinder are accurately predicted.
引用
收藏
页码:91 / 97
页数:6
相关论文
共 76 条
[1]  
Chen S.(1997)undefined Ann. Rev. Fluid Mech. 30 329-undefined
[2]  
Doolen G.(2006)undefined J. Fluid Mech. 550 413-undefined
[3]  
Shan X.(1992)undefined Phys. Rev. A 45 5339-undefined
[4]  
Yuan X.(1997)undefined Int. J. Mod. Phys. C 8 675-undefined
[5]  
Chen H.(1992)undefined Europhys. Lett. 17 479-undefined
[6]  
Chen H.(2006)undefined Phys. Rev. E 74 046703-undefined
[7]  
Chen S.(2003)undefined V. Yakhot, Science 301 633-undefined
[8]  
Matthaeus W.(2004)undefined J. Fluid Mech. 519 273-undefined
[9]  
Chen H.(2002)undefined AIAA J. Aircraft 39 434-undefined
[10]  
Teixeira C.(1998)undefined Int. J. Mod. Phys. C 9 1281-undefined