通过阻抗准则预测涡激振动

D. Sabino, D. Fabre, J. Leontini, D. L. Jacono
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引用次数: 12

摘要

我们使用不可压缩的线性化纳维-斯托克斯方程,研究了一个浸没在牛顿粘性流中并能沿未扰动流的正交方向运动的安装有弹簧的阻尼刚性圆柱体在雷诺数 $Re$ 在不稳定性开始附近($15\leqslant Re\leqslant 60$)的涡旋诱导振动。首先,我们考虑了气缸的强加谐波运动来解决线性问题。结果用机械阻抗来解释,即垂直力系数与气缸速度之间的比率,它是雷诺数和驱动频率的函数。考虑到圆柱体和流体之间的能量传递,我们发现阻抗结果提供了一个简单的标准,可以预测流体-弹性耦合结构的不稳定性。然后,我们对完全耦合的流体/气缸系统进行了全局稳定性分析。通过第二种方法获得的不稳定性阈值与基于阻抗准则的预测结果完全一致。然后,基于渐近发展的理论论证给出了耦合问题特征值的预测,并根据减速度 $U^{\ast }$、无量纲质量 $m^{\ast }$ 和雷诺数的函数描述了阈值以外不稳定区域的特征。此外,还探讨了阻尼参数 $unicode[STIX]{x1D6FE}$ 对不稳定区域的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Vortex-induced vibration prediction via an impedance criterion
The vortex-induced vibration of a spring-mounted, damped, rigid circular cylinder, immersed in a Newtonian viscous flow and capable of moving in the direction orthogonal to the unperturbed flow is investigated for Reynolds numbers $Re$ in the vicinity of the onset of unsteadiness ($15\leqslant Re\leqslant 60$) using the incompressible linearised Navier–Stokes equations. In a first step, we solve the linear problem considering an imposed harmonic motion of the cylinder. Results are interpreted in terms of the mechanical impedance, i.e. the ratio between the vertical force coefficient and the cylinder velocity, which is represented as function of the Reynolds number and the driving frequency. Considering the energy transfer between the cylinder and the fluid, we show that impedance results provide a simple criterion allowing the prediction of the onset of instability of the coupled fluid-elastic structure case. A global stability analysis of the fully coupled fluid/cylinder system is then performed. The instability thresholds obtained by this second approach are found to be in perfect agreement with the predictions of the impedance-based criterion. A theoretical argument, based on asymptotic developments, is then provided to give a prediction of eigenvalues of the coupled problem, as well as to characterise the region of instability beyond the threshold as function of the reduced velocity $U^{\ast }$, the dimensionless mass $m^{\ast }$ and the Reynolds number. The influence of the damping parameter $\unicode[STIX]{x1D6FE}$ on the instability region is also explored.
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