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The effects of damping on the amplitude and frequency response of a freely vibrating cylinder in cross-flow

机译:阻尼对横流中自由振动圆柱体的振幅和频率响应的影响

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We have studied the effects of controlled damping on the amplitude and frequency response profiles of an elastically mounted cylinder in cross-flow. The dimensionless damping parameter, b{sup}* = 2b/ρLDU, which is closely related to the traditional "mass-damping" parameter, m{sup}*ξ, was varied over a wide range of values through the use of a variable magnetic eddy current damping system. For low damping and sufficiently high Reynolds number we observe the previously described large-amplitude, three-branch (initial, upper, lower) response profile, and for high damping or low Reynolds number we observe the small-amplitude, two-branch (initial and lower) response profile. However we find that, because of the influence of Reynolds number, the traditional labels of "high mass-damping" and "low mass-damping" are incomplete with regard to predicting a large or small-amplitude response profile. In our experiments, as damping is systematically increased, we observe a transition between these two profiles characterized by a gradual "erosion" and eventual disappearance of the large-amplitude section (upper branch) and the scaling down of the lower branch region. We find that jumps from the upper to the initial branch originate on the 2S/2P boundary in the Williamson-Roshko plane. Another new finding is a hysteresis between the lower branch and the desynchronized region, which only appears at low Reynolds numbers. We also explore changes in the frequency response profile, which are connected with the changes in the amplitude profile, for our upper branch cases. We observe that analogous to the three amplitude branches, there are three distinct branches for the frequency response.
机译:我们研究了受控阻尼对错流的弹性安装气缸的振幅和频率响应曲线的影响。与传统的“质量阻尼”参数m {sup} *ξ密切相关的无量纲阻尼参数b {sup} * = 2b /ρLDU,通过使用变量在很大的范围内变化磁涡流阻尼系统。对于低阻尼和足够高的雷诺数,我们观察到了先前描述的大振幅三分支(初始,上,下)响应曲线,对于高阻尼或低雷诺数,我们观察了小振幅,两分支(初始及以下)的响应配置文件。但是,我们发现,由于雷诺数的影响,“大质量阻尼”和“低质量阻尼”的传统标签在预测大振幅或小振幅响应曲线方面并不完整。在我们的实验中,随着阻尼的系统增加,我们观察到这两个曲线之间的过渡,其特征是逐渐出现“侵蚀”,并最终使大振幅部分(上部分支)消失,下部分支区域按比例缩小。我们发现,从上部分支到初始分支的跳跃起源于Williamson-Roshko飞机的2S / 2P边界。另一个新发现是下部分支与失步区域之间的磁滞现象,仅在低雷诺数时出现。对于上分支情况,我们还探索了频率响应曲线的变化,该变化与幅度曲线的变化有关。我们观察到,类似于三个幅度分支,对于频率响应有三个不同的分支。

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