1.College of Civil Engineering and Architecture, Zhejiang University, Hangzhou 310058, China;
2.Electric Power Design Institute of Zhejiang Province, Hangzhou 310007, China
In order to study the aerodynamic coefficients and flow characteristics of a smooth circular cylinder, wind pressures on the cylinder were measured at different wind speeds in a uniform flow simulated in a wind tunnel.The variation of the drag coefficient, lift coefficient, surface wind pressure distribution, wind pressure correlation coefficient and Strouhal number of the cylinder with respect to the Reynolds number were obtained.And the above results were compared with those of the previous researches.The results show that the fluctuation of the lift coefficients is larger than that of the drag coefficients, indicating that the vortex shedding induced by cross-wind excitation is more significant than that induced by along-wind turbulence.When the Reynolds number is in the critical flow region, the wind distribution around the cylinder experiences a symmetry-asymmetry-symmetry transition, revealing a whole changing process from laminar flow separation to turbulent flow separation.When the Reynolds number equals 352 000, a critical flow with laminar flow separation on one side and turbulent flow separation on the other side occurs and the wind pressures around the cylinder present a unilaterally asymmetrical bubble form.The characteristics of wind pressure correlation during laminar flow separation and turbulent flow separation were obtained.The wind pressures on the same side of the cylinder are highly correlated in the laminar flow separation case.Whereas, the wind pressures in the flow region before the separation point are highly correlated and those in the flow region after the separation point are weakly correlated in the turbulent flow separation case.The spectrum of lift coefficient has an obvious peak in the turbulent flow separation case, indicating that the fluctuation of the wind pressures is induced by the periodical vortex.The spectrum of lift coefficient has no obvious peak in the turbulent flow separation case, indicating that the fluctuation of the wind pressures is induced by the random vortex.
[1] Simiu E, Scanlan R H. Wind effects on structures: fundamentals and applications to design[M], New York, John Wiley & Sons Inc, 1996.
[2] Homes J D. Wind loading of structures[M]. New York, CRC Press, 2015.
[3] Michael B. A challenging test case for large eddy simulation: high Reynolds number circular cylinder flow[J]. Heat and Fluid Flow, 2000, 21(5): 648-654.
[4] 詹昊, 李万平, 方秦汉, 等. 不同雷诺数下圆柱绕流仿真计算[J]. 武汉理工大学学报, 2008(12):129-132.
Zhan Hao, Li Wanping, Fang Qinhan, et al. Numerical simulation of the flow around a circular cylinder at various Reynolds number[J]. Journal of Wuhan University of Technology, 2008(12):129-132.
[5] 秦其伟, 刘小兵, 刘庆宽. 高超临界雷诺数下圆柱绕流的数值计算[J]. 工程力学, 2016, 33(suppl):18-22.
Qin qiwei, Liu Xiaobing, Liu Qingkuan. Numerical calculation of flow over circular cylinder at high supercritical Reynolds number[J]. Engineering Mechanics, 2016, 33(suppl):18-22.
[6] 李寿英, 顾明. 斜、直圆柱绕流的CFD模拟[J]. 空气动力学学报, 2005, 23(2):222-227.
Li Shouying, Gu Ming. Numerical simulation for flow around perpendicular and oblique circular cylinders[J]. Acta Aerodynamica Sinica, 2005, 23(2):222-227.
[7] Delany N K, Sorensen N E. Low-speed drag of cylinders of various shapes[R]. National Advisory Committee for Aeronautics, Technical note 3038, 1953.
[8] Achenbach E. Influence of surface roughness on the cross-flow around a circular cylinder[J], Journal of Fluid Mechanics, 1971, 46(2):321-335.
[9] Cheung C K, Melboure W H. Wind tunnel blockage effect on a circular cylinder in turbulent flows[J], 7th Australasian hydraulics and fluid mechanics conference, Brisbane, 18-22, August, 1980.
[10] Norberg C. Experimental investigation of the flow around a circular cylinder: influence of aspect ratio[J]. Journal of Fluid Mechanics, 2006, 258:287-316.
[11] Grove A S, Shair F H, Petersen E E, et al. An experimental investigation of the steady separated flow past a circular cylinder[J]. Journal of Fluid Mechanics, 2006,19(1):60-80.
[12] 李会知, 樊友景, 吴义章, 等. 不同粗糙表面的圆柱风压分布试验研究[J]. 工程力学, 2002, 19(2):129-132.
Li huizhi, Fan youjing, Wu Yizhang, et al. Wind tunnel testof pressure distribution on cylinders with warious surface roughness[J]. Engineering Mechanics, 2002, 19(2):129-132.
[13] 刘庆宽, 邵奇, 郑云飞, 等. 雷诺数对圆柱气动力和流场影响的试验研究[J]. 实验流体力学, 2016, 30(4):7-13.
Liu qingkuan, Shao qi, Zheng yunfei, et al. Experimental study on Reynolds number effect on aerodynamic pressure and forces of cylinder [J]. Journal of Experiments in Fluid Mechanics, 2016, 30(4):7-13.
[14] 马文勇, 袁欣欣, 张晓斌, 等. 圆形断面在35k~330k雷诺数范围的气动力特性研究[J]. 工程力学, 2015, 32(suppl):348-352.
Ma Wenyong, Yuan Xinxin, Zhang Xiaobing, et al. Charactertistics of aerodynamcis forces on a circular cylinder at Reynolds numbers from 35k to 330k[J]. Engineering Mechanics, 2015, 32(suppl):348-352.
[15] 郑云飞, 刘庆宽, 马文勇, 等. 端板对二维矩形风洞试验模型气动特性的研究[J]. 实验流体力学, 2017, 31(3):38-45.
Liu qingkuan, Shao qi, Zheng yunfei, et al. Experimental study on Reynolds number effect on aerodynamic pressure and forces of cylinder [J]. Journal of Experiments in Fluid Mechanics, 2017, 31(3):38-45.
[16] 建筑工程风洞试验方法标准JGJ/T 338-2014[S]. 中国建筑工业出版社, 2015.
Standard for wind tunnel test of buildings and structures: JGJ/T 338-2014[S]. Beijing: China Architecture and Building Press, 2015.