4∶1矩形断面运动诱导涡型扭转涡振的LES研究
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国家重点研发计划资助项目(2023YFC3805201),教育部111引智基地资助项目(B18062)


A LES Study of Torsional Motion-Induced Vortex Vibration of 4∶1 Rectangular Section
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    摘要:

    涡激振动是大跨度桥梁典型的风致振动现象之一,主要包括卡门涡型涡振和运动诱导涡型涡振.尽管已有大量研究对第一类振动进行了深入探讨,但对第二类振动的研究仍相对不足.为此,本研究以4∶1矩形断面为研究对象,采用大涡模拟方法再现了运动诱导涡型扭转涡振的完整过程,提出一种去均值的条件平均技术以提取关键旋涡的演化特征,系统分析了流场结构与气动力矩的内在作用机制.研究结果表明:前缘分离涡沿结构表面向下游的漂移及其与尾缘涡的融合过程,是结构发生运动诱导涡型涡振动态激励的主要来源.同时,研究发现涡旋运动特征与力矩密度分布在时空演化上高度一致.流场结构的动态变化不仅改变了作用在结构上的激励力矩幅值,还调控了气动力矩和扭转响应之间的相位关系.

    Abstract:

    Vortex-induced vibration is a representative wind-induced response of long-span bridges, comprising Karman vortex type vortex-induced vibration and motion-induced vortex vibration. Although the former has been extensively investigated, research on the latter remains comparatively limited. To address this gap, this study investigates the torsional mode of motion-induced vortex vibration in a 4:1 rectangular section using large-eddy simulation (LES). A mean-subtracted conditional averaging technique is proposed to elucidate the evolution of key vortices, and the underlying mechanism governing the flow field and aerodynamic moment are systematically analyzed. The results show that the downstream drift of leading-edge separation vortices along the section surface, together with their subsequent merger with trailing-edge vortices, constitutes the primary source of dynamic excitation that triggers motion-induced vortex vibration. Furthermore, the kinematics of the vortex structures exhibits strong spatiotemporal coherence with the distribution of aerodynamic moment density. The dynamic evolution of the flow field structures not only alters the amplitude of the aerodynamic excitation moment acting on the section but also modulates the phase relationship between the aerodynamic moment and the torsional response.

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回忆,陈海伟.4∶1矩形断面运动诱导涡型扭转涡振的LES研究[J].动力学与控制学报,2026,24(3):58~67; Hui Yi, Chen Haiwei. A LES Study of Torsional Motion-Induced Vortex Vibration of 4∶1 Rectangular Section[J]. Journal of Dynamics and Control,2026,24(3):58-67.

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  • 收稿日期:2025-11-06
  • 最后修改日期:2025-11-17
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  • 在线发布日期: 2026-03-30
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