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Usefulness of passive non-linear energy sinks in controlling galloping vibrations

机译:被动非线性能量吸收器在控制舞动振动中的有用性

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摘要

The suppression of vibration amplitudes of an elastically-mounted square prism subjected to galloping oscillations by using a non-linear energy sink is investigated. The non-linear energy sink consists of a secondary system with linear damping and non-linear stiffness. A representative model that couples the transverse displacement of the square prism and the non-linear energy sink is constructed. A linear analysis is performed to determine the impacts of the non-linear energy sink parameters (mass, damping, and stiffness) on the coupled frequency and onset speed of galloping. It is demonstrated that increasing the damping of the non-linear energy sink can result in a significant increase in the onset speed of galloping. Then, the normal form of the Hopf bifurcation is derived to identify the type of instability and to determine the effects of the non-linear energy sink stiffness on the performance of the aeroelastic system near the bifurcation. The results show that the non-linear energy sink can be efficiently implemented to significantly reduce the galloping amplitude of the square prism. It is also shown that the multiple stable responses of the coupled aeroelastic system are obtained as well as the periodic responses, which are dependent on the considered non-linear energy sink parameters. (C) 2016 Elsevier Ltd. All rights reserved.
机译:研究了通过使用非线性能量吸收器来抑制弹性安装的方棱镜受到驰豫振荡的振幅的问题。非线性能量吸收器由具有线性阻尼和非线性刚度的辅助系统组成。建立了一个将方形棱镜和非线性能量吸收器的横向位移耦合的代表性模型。执行线性分析以确定非线性能量吸收器参数(质量,阻尼和刚度)对舞动的耦合频率和起始速度的影响。已经证明,增加非线性能量吸收器的阻尼可以导致奔腾的开始速度显着增加。然后,得出霍普夫分叉的范式,以识别不稳定性的类型,并确定非线性能量宿刚度对分叉附近气动弹性系统性能的影响。结果表明,可以有效地实现非线性能量吸收器,以显着减小方形棱镜的驰豫幅度。还表明,获得了耦合气动弹性系统的多个稳定响应以及周期响应,这些响应取决于所考虑的非线性能量宿参数。 (C)2016 Elsevier Ltd.保留所有权利。

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