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Variable structure control of vortex-induced vibration.

机译:涡激振动的可变结构控制。

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摘要

The fundamentals of actively controlling vortex-induced vibration of flexible cylinders using the theory of robust controls are presented. A variable structure robust controller is devised to reject the persistent disturbances produced by the periodic shedding of vortices. In addition, the controller is capable of accommodating changes in the structural parameters of the cylinders and the non-linearities resulting from fluid-structure interactions.;Finite element-based model of the vortex-induced vibrations of flexible cylinders is presented using the wake-oscillator approach. The model is coupled with the time dependent flow-induced forcing function and integrated with the variable structure-sliding mode control strategy. The mathematical model developed is validated experimentally by testing various prototypes of flexible cylinders in a low-speed wind tunnel under various flow conditions. The effect of varying the design parameters of the controller and the cylinders on the attenuation of the vortex-induced vibrations is monitored. Emphasis is placed in this research effort on demonstrating the effectiveness of the variable structure-sliding mode controller in suppressing vortex-induced vibration of flexible cylinders.
机译:提出了使用鲁棒控制理论主动控制柔性缸涡旋振动的基本原理。设计了一种可变结构的鲁棒控制器,以抑制由于周期性涡旋脱落而产生的持续干扰。此外,该控制器还能够适应气缸结构参数的变化以及由于流体-结构相互作用而引起的非线性。;基于有限元模型,利用尾流模型建立了柔性气缸涡旋振动的模型振荡器方法。该模型与时间相关的流致强迫函数耦合,并与可变结构滑模控制策略集成。通过在各种流量条件下在低速风洞中测试柔性气缸的各种原型,通过实验验证了开发的数学模型。监测控制器和气缸设计参数的变化对涡流引起的振动衰减的影响。这项研究的重点是证明可变结构滑模控制器在抑制涡流引起的柔性气缸振动方面的有效性。

著录项

  • 作者

    Hussein, Nagy Mohamed.;

  • 作者单位

    The Catholic University of America.;

  • 授予单位 The Catholic University of America.;
  • 学科 Engineering Aerospace.;Engineering Mechanical.;Engineering Marine and Ocean.
  • 学位 Ph.D.
  • 年度 1994
  • 页码 114 p.
  • 总页数 114
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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