Experimental investigation on wake characteristics behind a yawed square cylinder

被引:11
|
作者
Lou, X. [1 ]
Zhou, T. [1 ]
Zhou, Y. [2 ]
Wang, H. [3 ]
Cheng, L. [1 ]
机构
[1] Univ Western Australia, Sch Civil Environm & Min Engn, 35 Stirling Highway, Crawley, WA 6009, Australia
[2] Harbin Inst Technol, Shen Zhen Postgrad Sch, Harbin, Peoples R China
[3] Cent S Univ, Sch Civil Engn & Architecture, Changsha, Hunan, Peoples R China
基金
澳大利亚研究理事会;
关键词
Yawed square cylinder; Vortex shedding; Phase-average method; TAYLOR HYPOTHESIS; STROUHAL NUMBERS; TURBULENT WAKE; HEAT-TRANSPORT; FLOW STRUCTURE; VORTICITY; SIMULATION; MOMENTUM; REGION;
D O I
10.1016/j.jfluidstructs.2015.11.017
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The wake vortical structures of a square cylinder at different yaw angles to the incoming flow (alpha = 0 degrees, 15 degrees, 30 degrees and 45 degrees) are studied using a one-dimensional (1D) hot-wire vorticity probe at a Reynolds number (Re) of about 3600. The results are compared with those obtained in a yawed circular cylinder wake. The Strouhal number (St(N)) as well as the mean drag coefficient (C-DN), normalized by the velocity component normal to the cylinder axis, follow the independent principle (IP) satisfactorily up to alpha = 40 degrees. Using the phase averaging analysis, both the coherent and the remaining contributions of velocity and vorticity are quantified. The flow patterns of the coherent spanwise vorticity (omega(z))display obvious Karman vortex streets and their maximum concentrations decrease as a increases. Similar phenomena are also shown in the coherent contours of the streamwise (u) and transverse (v) velocities as well as the Reynolds shear stress (uv). The contours of the spanwise velocity (w) and Reynolds shear stress (uw), however, experience an increasing trend for the maximum concentrations with increasing yaw angle. These results indicate an enhancement of the three-dimensionality of the wake and the reduction of vortex shedding strength as a increases. While general similarities to the wake behind a yawed circular cylinder are found in terms of flow features, some differences between the two wakes at different yaw angles are highlighted. (C) 2015 Elsevier Ltd. All rights reserved.
引用
收藏
页码:274 / 294
页数:21
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