首页> 外文期刊>Journal of Wind Engineering and Industrial Aerodynamics: The Journal of the International Association for Wind Engineering >Vortex-induced vibration and its effect on torsional flutter instability in the case of B/D=4 rectangular cylinder
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Vortex-induced vibration and its effect on torsional flutter instability in the case of B/D=4 rectangular cylinder

机译:B / D = 4矩形圆柱体时涡激振动及其对扭振不稳定性的影响

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摘要

For two-dimensional rectangular cylinder with the side-ratio of 4 (B/D = 4, B: along-wind length, D: cross-wind length), two different types of vortex-induced excitation, which are motion-induced vortex excitation, i.e. shear layer instability related-vortex excitation, and Karman vortex excitation, were observed in both heaving and torsional motion. Also, the role of vortex-generation on the torsional flutter instability was experimentally investigated by changing the rotation axis in the state without/with a splitter plate in the wake. The two different kinds of vortex-induced excitations was confirmed in the close reduced wind speed region, and the vortex-induced excitations could play an important role as triggering of torsional flutter instability when Scruton number is small enough. Furthermore, the flow pattern around the cylinder during torsional motion drastically changes between the low and high-reduced velocity.
机译:对于侧面比为4的二维矩形圆柱体(B / D = 4,B:顺风长度,D:横风长度),两种不同类型的涡旋激发是运动涡旋在升沉运动和扭转运动中都观察到了激振,即剪切层失稳相关的激振和Karman激振。另外,通过在尾流不带隔板的情况下改变旋转轴,实验研究了涡旋产生对扭转颤振不稳定性的作用。在接近减小的风速区域确认了两种不同类型的涡旋激振,当Scruton数足够小时,涡旋激振可能在触发扭振不稳定性中起重要作用。此外,在扭转运动期间,圆柱体周围的流动模式在低和高降低速度之间急剧变化。

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