首页> 外文会议>International Conference on Structural Dynamics >Limit Cycles in Vortex-Induced Vibrations: a Critical Analysis
【24h】

Limit Cycles in Vortex-Induced Vibrations: a Critical Analysis

机译:涡旋诱导的振动中限制循环:一个关键分析

获取原文

摘要

The fluid-structure interaction in vortex-induced vibrations of circular structures is modelled as a non-linear damping force. The Van der Pol and Rayleigh oscillators are classic examples of physical systems, which attain a limit cycle under self-induced vibrations. Their application for the case of vortex-induced vibrations has a theoretical justification in Marris, who found an analogy with the Magnus effect for a rotating cylinder, because the lift force on a vibrating cylinder is produced by the non-symmetric boundary layer separation from the top and bottom surfaces. In accordance with the Rayleigh formulation, Vickery&Basu propose for the aerodynamic damping a parabolic relationship function of the rms oscillation. This approach is recommended in many international codes (e.g. Eurocode) for the design of circular structures with regard to cross-wind vibrations, even though the predictions result extremely conservative. Recent wind tunnel experiments performed at WISt (Ruhr-Universitat Bochum, Germany) on a circular cylinder in forced-oscillations evidenced a behaviour of the aerodynamic damping with positive curvature, which is in contrast with the negative curvature in Rayleigh oscillator. These experimental results require a critical analysis of the Vickery formulation and its theoretical background.
机译:涡旋诱导的圆形结构振动中的流体结构相互作用被建模为非线性阻尼力。 van der POL和Rayleigh振荡器是物理系统的经典示例,其在自诱导的振动下获得极限循环。他们对涡旋诱导的振动的申请具有在Marris中的理论典范化,他们发现了一种与旋转圆筒的大马效果的类比,因为振动缸上的提升力由非对称边界层分离产生顶部和底表面。根据Rayleigh配方,Vickery&Basu提出了空气动力学阻尼RMS振荡的抛物关系功能。这种方法建议在许多国际代码(例如Eurocode)中,用于在横向振动方面设计循环结构,即使预测结果极为保守。在强制 - 振动中的圆柱体上进行的最近在诸如诸如圆柱体的圆柱体进行的风洞实验证明了具有阳性曲率的空气动力学阻尼的行为,这与瑞利振荡器中的负曲率相反。这些实验结果需要对Vickery制剂及其理论背景的关键分析。

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