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Nonlinear structural response in vortex-induced vibrations.

机译:涡激振动中的非线性结构响应。

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摘要

This study focuses on realistic structural response calculations under vortex-induced vibration. For calculating response associated with vortex-induced vibrations of a flexible cylinder a new model is used. This model considers the periodic wake as a nonlinear oscillator interacting nonlinearly with the body oscillator; parametric excitation is taken as the driving mechanism. This model represents the mechanism of' vortex-induced vibration that includes lock-in motion over a bandwidth, zones of instability for various frequency ratios, phase jump, hysteresis and bistability in structural response.;Numerical integration of the coupled model highlights the key characteristics of vortex-induced vibration due to nonlinear interaction between the body and the wake and is used to calculate the shortening of vortex formation length. The results show that the response is bistable and phase jump is observed.;Approximate analytical analysis using Method of Averaging of Krylov and Bogoliubov and Integral Equation Method and direct numerical integration provides the solution for the single degree of freedom model in order to get the structural response. Analysis of the model shows: there are two distinct levels of response, a significant phase jump during the mode transition, an amplification around the structural frequency, increase in resonance amplitude with decreasing structural mass and damping, a hysteretic behavior at both ends of the lock-in zone and high amplitude nonlinear damping. This is in accord with experimentally observed key characteristics for free vortex-induced vibration of cylinders.;This study suggests that the structural response due to vortex-induced vibration is nonlinear and parametric. This study is expected to have a substantial impact on the damping techniques for controlling tall building vibrations. Moreover, it is believed, the out come of the work will lead to consistent and realistic structural response calculations.
机译:这项研究的重点是在涡激振动下的实际结构响应计算。为了计算与挠性圆柱体的涡流引起的振动相关的响应,使用了新模型。该模型将周期唤醒视为与体振荡器非线性相互作用的非线性振荡器。参数激励被视为驱动机制。该模型代表了涡激振动的机制,包括在带宽上的锁定运动,各种频率比的不稳定性区域,相位跳变,磁滞和结构响应的双稳性。耦合模型的数字积分突出了关键特征体与尾流之间的非线性相互作用引起的涡流引起的振动的变化,并用于计算涡流形成长度的缩短。结果表明,该响应是双稳态的,并且观察到了相位跳变。;使用Krylov和Bogoliubov的平均方法和积分方程法以及直接数值积分的近似分析,为单自由度模型提供了解决方案,从而获得了结构响应。对模型的分析表明:有两个不同的响应级别,在模式转换期间出现明显的相跳,在结构频率附近放大,随着结构质量和阻尼的减小,共振幅度增加,在锁的两端都有滞后行为区域和高振幅非线性阻尼。这与实验观察到的圆柱自由涡流引起的振动的关键特征相一致。;本研究表明,涡流引起的振动引起的结构响应是非线性的并且是参数化的。预期该研究将对控制高层建筑物振动的阻尼技术产生重大影响。而且,可以相信,这项工作的结果将导致一致和现实的结构响应计算。

著录项

  • 作者

    Ahmad, Owais.;

  • 作者单位

    Stevens Institute of Technology.;

  • 授予单位 Stevens Institute of Technology.;
  • 学科 Engineering Civil.
  • 学位 Ph.D.
  • 年度 2004
  • 页码 221 p.
  • 总页数 221
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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