圆柱后丝的涡激振动与颤振

IF 2.2 3区 工程技术 Q2 MECHANICS Theoretical and Computational Fluid Dynamics Pub Date : 2023-03-13 DOI:10.1007/s00162-023-00644-3
Mohd Furquan, Sanjay Mittal
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引用次数: 0

摘要

流动通过柔性细丝,二维分裂板的厚度可忽略不计,附在一个圆柱体后面。基于来流自由流速度和柱体直径的雷诺数为\(\textrm{Re}=100\)。在此\(\textrm{Re}\),刚性灯丝的流动是稳定的。然而,柔性细丝在一定的减速范围内经历流动引起的振动,\(U^*\),定义为细丝的第一个无量纲化固有频率的倒数。在本工作(\(U^*\le 240\))中考虑的\(U^*\)的大范围内,它表现出颤振和涡激振动(VIV)。在VIV期间,观察到与灯丝弯曲相关的各种正常模式的锁定,每种模式都处于不同的减速状态。有趣的是,流体-结构系统不锁定在弯曲的第一模态,而是锁定在更高的模态。在第二种模式锁定之前和之后,在较长的减速范围内,流量都是稳定的。观察到两种旋涡脱落模式。\(\textsf{2P}\)模态与高频振动有关,而\(\mathsf {2\,S}\)模态是在相对低频振动期间观察到的。在第一个稳定状态下,一个破坏对称的干草叉分叉导致了灯丝的静态偏转。灯丝表现出颤振响应,在大幅度减速下,振幅和频率相对较低。在颤振过程中未观察到旋涡脱落。引起颤振的流体力是由于在圆柱体下游的再循环区域中灯丝两侧的不对称而产生的。通过对颤振和涡激振动时流丝界面能量传递的时空分布进行对比,发现颤振时的能量传递比涡激振动时小得多。颤振时,最大能量传递点位于纤丝根部附近,而在涡激时,最大能量传递点位于纤丝尖端附近。
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Vortex-induced vibration and flutter of a filament behind a circular cylinder

Flow past a flexible filament, a two-dimensional splitter plate with negligible thickness, attached behind a circular cylinder is investigated. The Reynolds number based on the free-stream speed of incoming flow and diameter of the cylinder is \(\textrm{Re}=100\). At this \(\textrm{Re}\), the flow for a rigid filament is steady. However, a flexible filament undergoes flow-induced vibration for a range of reduced speed, \(U^*\), defined as inverse of the first nondimensionalized natural frequency of the filament. Over the wide range of \(U^*\) considered in this work (\(U^*\le 240\)), it exhibits both flutter and vortex-induced vibration (VIV). Lock-in with various normal modes related to bending of the filament, each in a different regime of reduced speed, is observed during VIV. Interestingly, the fluid–structure system does not lock-in with the first normal mode of bending but with higher modes. The flow is steady for an extended range of reduced speed both before and after the lock-in with second mode. Two patterns of vortex shedding are observed. The \(\textsf{2P}\) mode is associated with high-frequency vibration, while the \(\mathsf {2\,S}\) mode is observed during relatively low-frequency oscillation. A symmetry-breaking pitchfork bifurcation leads to static deflection of the filament during the first steady regime. The filament exhibits flutter response, at large reduced speed, with relatively low amplitude and frequency. No vortex shedding is observed during flutter. The fluid forces that cause flutter arise from asymmetry across the two sides of the filament in the zones of recirculation downstream of the cylinder. Comparison of the space-time patterns of energy transfer at the fluid–filament interface for flutter and vortex-induced vibration reveals that the energy transfer is much smaller during flutter compared to VIV. The point of maximum energy transfer is located close to the root of the filament in case of flutter, while it is near the tip during VIV.

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来源期刊
CiteScore
5.80
自引率
2.90%
发文量
38
审稿时长
>12 weeks
期刊介绍: Theoretical and Computational Fluid Dynamics provides a forum for the cross fertilization of ideas, tools and techniques across all disciplines in which fluid flow plays a role. The focus is on aspects of fluid dynamics where theory and computation are used to provide insights and data upon which solid physical understanding is revealed. We seek research papers, invited review articles, brief communications, letters and comments addressing flow phenomena of relevance to aeronautical, geophysical, environmental, material, mechanical and life sciences. Papers of a purely algorithmic, experimental or engineering application nature, and papers without significant new physical insights, are outside the scope of this journal. For computational work, authors are responsible for ensuring that any artifacts of discretization and/or implementation are sufficiently controlled such that the numerical results unambiguously support the conclusions drawn. Where appropriate, and to the extent possible, such papers should either include or reference supporting documentation in the form of verification and validation studies.
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