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闭口箱梁桥气动性能几何参数的灵敏度分析。

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

机构信息

State Key Lab for Disaster Reduction in Civil Engineering, Tongji University, Shanghai 200092, China.

Institute of Urban Smart Transportation & Safety Maintenance, Shenzheng University, Shenzhen 518060, China.

出版信息

Sensors (Basel). 2018 Jun 27;18(7):2053. doi: 10.3390/s18072053.

Abstract

In this study, the influence of two critical geometrical parameters (i.e., angles of wind fairing, α; and lower inclined web, β) 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 β, a closed-box girder with a sharper wind fairing angle of α = 50° has better flutter and vortex-induced vibration (VIV) performance than that with α = 60°, while an inclined web angle of β = 14° produces the best VIV performance. In addition, the results from particle image velocimetry (PIV) tests indicate that a wind fairing angle of α = 50° 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 ₂) and Part D (with a reference of ₁₃) generally decrease with the increase of β, 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 β.

摘要

在这项研究中,通过理论分析和使用激光位移传感器进行风洞试验,系统研究了两个关键几何参数(即挡风罩角度 α 和下斜腹板 β)对闭口箱梁桥空气动力性能的影响。结果表明,对于特定的斜腹板角度 β,挡风罩角度 α = 50°的闭口箱梁具有比 α = 60°更好的颤振和涡激振动(VIV)性能,而 β = 14°的斜腹板产生最佳的 VIV 性能。此外,粒子图像测速(PIV)测试结果表明,α = 50°的挡风罩角度通过诱导单个涡结构和尾流区域上下部分的涡度强度的平衡分布产生更好的颤振性能。此外,二维三自由度(2D-3DOF)分析结果表明,绝对值 Part A(以颤振导数 ₂为参考)和 Part D(以 ₁₃为参考)通常随 β的增加而减小,而扭转为主的耦合颤振中俯仰自由度(DOF)的参与水平的变化最初增加,达到峰值,然后随 β的增加而减小。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/71da/6069057/6aa0fa8d0b70/sensors-18-02053-g001.jpg

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