首页> 外文期刊>Engineering Structures >Analysis of crosswind fatigue of wind-excited structures with nonlinear aerodynamic damping
【24h】

Analysis of crosswind fatigue of wind-excited structures with nonlinear aerodynamic damping

机译:非线性气动阻尼的风振结构侧风疲劳分析

获取原文
获取原文并翻译 | 示例
       

摘要

This study addresses crosswind fatigue analysis of wind-excited flexible structures at the vicinity of vortex lock-in speed where the nonlinear aerodynamic damping effect is significant. The nonlinear aerodynamic damping is modeled as a polynomial function of time-varying displacement or velocity of vibration. The crosswind response is a narrow-band hardening non-Gaussian process with a reduced peak factor and having a distribution of vibration amplitude different from Rayleigh distribution. Analytical solutions of cycle number and fatigue damage are derived and their accuracy is validated through comparison with rainflow cycle counting method using simulated response time histories. A correction factor as a function of response kurtosis is also introduced that facilitates the calculation of non-Gaussian fatigue damage from the Gaussian fatigue prediction. The effectiveness and accuracy of the proposed framework are illustrated by crosswind responses of a squared tall building and a two-dimensional structural section model, and by full-scale vibration measurement data of a traffic-signal-support-structure. This study provides an improved estimation of crosswind fatigue of wind-excited flexible structures with a consideration of hardening non-Gaussian response character.
机译:本文研究了在非线性气动阻尼效应显着的涡旋锁定速度附近的风激励柔性结构的侧风疲劳分析。非线性空气动力学阻尼建模为时变位移或振动速度的多项式函数。侧风响应是一种窄带硬化非高斯过程,具有降低的峰值因子,并且具有不同于瑞利分布的振动幅度分布。推导了循环次数和疲劳损伤的解析解,并通过使用模拟响应时间历史与雨流循环计数法进行比较,验证了其准确性。还引入了作为响应峰度的函数的校正因子,该校正因子有助于根据高斯疲劳预测来计算非高斯疲劳损伤。拟议框架的有效性和准确性通过方形高层建筑的侧风响应和二维结构截面模型以及交通信号支持结构的满量程振动测量数据进行了说明。这项研究考虑到硬化非高斯响应特性,提供了一种对风激励柔性结构的侧风疲劳的改进估计。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号