上游双扰动对圆柱气动特性影响的数值模拟

张攀峰; 王晋军; 武哲

上游双扰动对圆柱气动特性影响的数值模拟

北京航空航天大学航空科学与工程学院, 北京 100083

基金项目: 国家自然科学基金资助项目(10272016)

详细信息

作者简介:
张攀峰(1978-),男,湖北武汉人,博士后,pfzhang@ase.buaa.edu.cn.

中图分类号: O 357.5; V 211.3
计量
- 文章访问数: 2904
- HTML全文浏览量: 43
- PDF下载量: 1024
- 被引次数: 0
出版历程
- 收稿日期: 2005-12-13
- 网络出版日期: 2006-10-31

Numerical simulation on upstream dual rods′ effect on aerodynamic characteristics of cylinder

School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

摘要

摘要: 通过用商用计算流体力学软件FLUENT 6.0中的SIMPLE方法求解二维非定常层流模型,对雷诺数Re=200时上游双扰动体对下游圆柱气动特性影响进行了数值模拟研究.计算结果表明当双扰动体相隔较近(H/d=1.1,1.33)时,其后形成单一的Karman涡街,它们对下游圆柱的干扰作用类似于单扰动体时的情况,但是流动结构发生变化的临界间距Lcri较之有效宽度相同的单扰动体的要大,因此可以推断出在该种布置下双扰动体和圆柱绕流会出现2种流动模式.在空穴流动模式下面,下游圆柱的阻力和升力脉动最多减小94%和79%,系统阻力(包括圆柱和扰动体)也能减小33%.而当双扰动体尾流为双Karman涡街时(双扰动体相隔较远H/d=3.33,5.0),圆柱迎风面部分区域仍受到来流的冲击作用,气动力减小有限.
- 双扰动体 /
- 圆柱 /
- 减阻 /
- 层流 /
- 数值模拟
Abstract: Numerical simulation was constructed to investigate the upstream dual rods′ effect on the characteristics of the cylinder at Reynolds number 200. The unsteady laminar model was solved by SIMPLE method with CFD(computational fluid dynamics) commercial software package FLUENT 6.0. When the dual rods have small vertical interval (H/d=1.1, 1.33), there is only one Karman vortex street formed behind the rods. This case is much more similar to that of a single rod, but the critical spacing ratio for the flow pattern transition is larger than that of the single one. That means there are two different flow patterns with the spacing ratio increase, the cavity flow mode and the wake impinging mode. In the cavity flow mode, the maximum drag and RMS (root mean square) value of lift were reduced by 94% and 79%, respectively. The system drag (including the rod and the cylinder drag) was reduced by 33%. If there are two vortex streets behind the rods with large vertical interval (H/d=3.33, 5.0), the upwind surface of the cylinder is also impinged by the gap flow between the rods, which results in the drag and RMS value of lift reduction is limited.
- perturbation techniques /
- cylinders /
- drag reduction /
- laminar /
- numerical simulation

HTML全文

参考文献(1)

[1] Zdravkovich M M. Flow around circular cylinders[M]. Oxford:Oxford University Press, 1997 [2] Lesage F, Gartshore I S. A method of reducing drag and fluctuating side force on bluff bodies[J]. J of Wind Engineering and Industrial Aerodynamics, 1987,25:229-245 [3] Igarashi T. Drag reduction of a square prism by flow control using a small rod[J]. J of Wind Engineering and Industrial Aerodynamics, 1997, 69-71:141-153 [4] Igarashi T, Terachi N. Drag reduction of flat plate normal to airstream by flow control using a rod [J]. J of Wind Engineering and Industrial Aerodynamics, 2002, 90:359-376 [5] Prasad A, Williamson C H K. A method for the reduction of bluff body drag[J]. J of Wind Engineering and Industrial Aerodynamics, 1997, 69-71:155-167 [6] Sakamoto H, Tan K, Takeuchi N, et al. Suppression of fluid forces acting on a square prism by passive control[J]. J Fluid Engineering, Trans of the ASME, 1997, 119:506-511 [7] Zhang P F, Wang J J, Lu S F, et al. Aerodynamic characteristics of a square cylinder with a rod in a staggered arrangement[J]. Experiments in Fluids, 2005, 38:494-502 [8] Wang J J, Zhang P F, Lu S F, et al. Drag reduction of a circular cylinder using an upstream rod[J]. Flow, Turbulence and Combustion, 2006, 76(1):83-101 [9] Norberg C. Flow around a circular cylinder:aspects of fluctuating lift [J]. Journal of Fluids and Structures, 2001,15:459-469 [10] Slaoutiand A, Stansby P K. Flow around two circular cylinders by the random-vortex method[J]. Journal of Fluids and Structures, 1992, 6:641-670 [11] Mittal S, Kumar V, Raghuvanshi A. Unsteady incompressible flows past two cylinders in tandem and staggered arrangements [J]. International Journal for Numerical Methods in Fluids, 1997, 25(11):1315-1344 [12] 张攀峰.上游扰动体减低钝体阻力机理研究 .北京:北京航空航天大学航空科学与工程学院,2005 Zhang Panfeng. Drag reduction of the bluff bodies by using an upstream interference . Beijing:School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics,2005(in Chinese) [13] Zhou Y, Zhang H J, Yiu M W. The turbulent wake of two side-by-side circular cylinders[J]. J Fluid Mech, 2002, 458:303-332 [14] Meneghini J R, Saltara F, Siqueira C L R, et al. Numerical simulation of flow interference between two circular cylinders in tandem and side-by-side arrangements[J]. J of Fluids and Structures, 2001, 15(2):327-350

施引文献

资源附件(0)

访问统计