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Vortex-induced vibration characteristics of an elastic square cylinder on fixed supports

机译:固定支架上弹性方筒的涡激振动特性

摘要

The vortex-induced structural vibration of an elastic square cylinder, on fixed supports at both ends, in a uniform cross flow was measured using fiber-optic Bragg grating sensors. The measurements are compared to those obtained for an elastic circular cylinder of the same hydraulic diameter in an effort to understand the effect of the nature (fixed or oscillating) of the flow separation point on the vortex-induced vibration. It is found that a violent vibration occurs at the third-mode resonance when the vortex-shedding frequency coincides with the third-mode natural frequency of the fluid-structure system, irrespective of the cross-sectional geometry of the cylinder. This is in distinct contrast to previous reports of flexibly supported rigid cylinders, where the first-mode vibration dominates, thus giving little information on the vibration of other modes. The resonance behavior is neither affected by the incidence angle (a) of the free stream, nor by the nature of the flow separation point. However, the vibration amplitude of the square cylinder is about twice that of the circular cylinder even though the flexural rigidity of the former is larger. This is ascribed to a difference in the nature of the flow separation point between the two types of structures. The characteristics of the effective modal damping ratios, defined as the sum of structural and fluid damping ratios, and the system natural frequencies are also investigated. The damping ratios and the system natural frequencies vary little with the reduced velocity at α=0 deg, but appreciable at α ≥15 deg; they further experience a sharp variation, dictated by the vortex-sheddine freauency, near resonance.
机译:使用光纤布拉格光栅传感器测量了在均匀固定的横向流动中,在两端固定支架上由弹性方筒产生的涡流引起的结构振动。将测量结果与从具有相同液压直径的弹性圆柱体获得的测量结果进行比较,以了解流动分离点的性质(固定或振荡)对涡流诱发的振动的影响。已经发现,当涡流脱落频率与流体结构系统的第三模式固有频率一致时,在第三模式共振时会发生剧烈振动,而与圆柱的横截面几何形状无关。这与以前报道的柔性支撑的刚性圆柱体形成鲜明对比,在以前的报道中,第一模式的振动占主导,因此几乎没有其他模式的振动信息。共振行为既不受自由流的入射角(α)的影响,也不受流动分离点的性质的影响。然而,即使前者的抗弯刚度较大,方筒的振动幅度也大约是圆筒的两倍。这归因于两种类型的结构之间的流动分离点的性质的差异。还研究了有效模态阻尼比(定义为结构阻尼比和流体阻尼比之和)以及系统固有频率的特性。阻尼比和系统固有频率在α= 0度时随速度降低而变化不大,但在α≥15度时可观。它们进一步经历了急剧的变化,这是由涡旋-雷西丁的柔韧性决定的,接近共振。

著录项

  • 作者

    Wang ZJ; Zhou Y;

  • 作者单位
  • 年度 2005
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  • 原文格式 PDF
  • 正文语种 eng
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