Sensitivity Analysis of Geometrical Parameters on the Aerodynamic Performance of Closed-Box Girder Bridges

被引:10
|
作者
Yang, Yongxin [1 ]
Zhou, Rui [2 ]
Ge, Yaojun [1 ]
Du, Yanliang [2 ]
Zhang, Lihai [3 ]
机构
[1] Tongji Univ, State Key Lab Disaster Reduct Civil Engn, Shanghai 200092, Peoples R China
[2] Shenzheng Univ, Inst Urban Smart Transportat & Safety Maintenance, Shenzhen 518060, Peoples R China
[3] Univ Melbourne, Dept Infrastruct Engn, Melbourne, Vic 3010, Australia
关键词
closed-box girder; wind fairing angle; lower inclined web angle; wind tunnel testing; particle image velocimetry; flutter performance; vortex-induced vibration performance; COUNTERMEASURES; SUSPENSION; FORCES;
D O I
10.3390/s18072053
中图分类号
O65 [分析化学];
学科分类号
070302 ; 081704 ;
摘要
In this study, the influence of two critical geometrical parameters (i.e., angles of wind fairing, a; and lower inclined web, beta) in the aerodynamic performance of closed-box girder bridges was systematically investigated through conducting a theoretical analysis and wind tunnel testing using laser displacement sensors. The results show that, for a particular inclined web angle beta, a closed-box girder with a sharper wind fairing angle of alpha = 50 degrees has better flutter and vortex-induced vibration (VIV) performance than that with alpha = 60 degrees, while an inclined web angle of beta = 14 degrees produces the best VIV performance. In addition, the results from particle image velocimetry (PIV) tests indicate that a wind fairing angle of alpha = 50 degrees produces a better flutter performance by inducing a single vortex structure and a balanced distribution of the strength of vorticity in both upper and lower parts of the wake region. Furthermore, two-dimensional three-degrees-of-freedom (2D-3DOF) analysis results demonstrate that the absolute values of Part A (with a reference of flutter derivative A(2)*) and Part D (with a reference of A(1) H-3*) generally decrease with the increase of beta, while the change of the participation level of heaving degrees of freedom (DOF) in torsion-dominated coupled flutter initially increases, reaches its peak, and then decreases with the increase of beta.
引用
收藏
页数:18
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