Numerical simulation of Reynolds number effects on velocity shear flow around a circular cylinder

被引:66
|
作者
Cao, Shuyang [1 ]
Ozono, Shigehira [2 ]
Tamura, Yukio [3 ]
Ge, Yaojun [1 ]
Kikugawa, Hironori [4 ]
机构
[1] Tongji Univ, State Key Lab Disaster Reduct Civil Engn, Shanghai 200092, Peoples R China
[2] Miyazaki Univ, Fac Engn, Miyazaki 8892192, Japan
[3] Tokyo Polytech Univ, Kanagawa 2430297, Japan
[4] Oita Natl Coll Technol, Dept Mech Engn, Oita 8700152, Japan
关键词
Aerodynamic force; Direct numerical simulation; Large eddy simulation; Shear parameter; Vortex shedding; Wake dynamics; NAVIER-STOKES EQUATIONS; FRACTIONAL-STEP METHOD; WAKE; TRANSITION; TURBULENT; DYNAMICS;
D O I
10.1016/j.jfluidstructs.2010.03.003
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Three-dimensional Direct Numerical Simulation (DNS) and Large Eddy Simulation (LES) are performed to investigate the shear effects on flow around a circular cylinder at Reynolds numbers of Re = 60-1000. The shear parameter, beta, which is based on the velocity gradient, cylinder diameter and upstream mean velocity at the center plane of the cylinder, varies from 0 to 0.30. Variations of Strouhal number, drag and lift coefficients, and unsteady wake structures with shear parameter are studied, along with their dependence on Reynolds number. The presented simulation provides detailed information for the flow field around a circular cylinder in shear flow. This study shows that the Strouhal number exhibits no significant variation with shear parameter. The stagnation point moves to the high-velocity side almost linearly with shear parameter, and this result mainly influences the aerodynamic forces acting on a circular cylinder in shear flow. Both the Reynolds number and shear parameter influence the movement of the stagnation point and separation point. Mode A wake instability is suppressed into parallel vortex shedding mode at a certain shear parameter. The lift force increases with increasing shear parameter and acts from the high-velocity side to the low-velocity side. In addition, a simple method to estimate the lift force coefficient in shear flow is provided. (C) 2010 Elsevier Ltd. All rights reserved.
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页码:685 / 702
页数:18
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