基于表面吸气的矩形截面涡激振动抑制及机理研究
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长沙理工大学大学生创新创业训练计划项目(202210536048)


VIV Suppression and Mechanism Analysis Based on The Surface Aspiration of Rectangular Section
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    摘要:

    随着桥梁跨度的增加,其风致振动问题逐渐凸显,发展简单有效的风振控制措施对于保障桥梁结构的安全具有重要意义.将桥梁断面简化为矩形,通过数值模拟研究了侧表面双气孔吸气对矩形截面的涡激振动的抑制作用.研究表明:无量纲吸气流量是影响涡激振动抑制效果的决定性因素.当无量纲吸气流量Qs=0.01时,表面吸气对涡激振动的抑制效果达到最佳,矩形断面的振动幅值减小了99.73%,升力系数均方根值减小了90.37%,阻力系数平均值减小了32.55%.当Qs>0.01时,矩形截面的振动幅值仍然被有效地抑制,但由于吸气流量过大,侧表面上的边界层厚度变小,边界层内的剪切效应变强,引起背风面尾流旋涡的增强,最终导致矩形截面升、阻力系数的增加.

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    With the increase of bridge span, the problem of wind-induced vibration becomes more and more prominent. The development of simple and effective wind-induced vibration control measures is of great significance to ensure the safety of bridge structure. The section of the bridge is simplified as a rectangle and the suppression of VIV of the rectangular section by suction with double holes on the side surface is studied by numerical simulation. The results show that the inspiratory flow rate is the decisive factor affecting the suppression effect of VIV. When the dimensionless suction flow rate Qs=0.01, the surface suction has the best suppression effect on VIV. The vibration amplitude of the rectangular section is reduced by 99.73%, the root mean square value of lift coefficient is reduced by 90.73%, and the average drag coefficient is reduced by 32.55%. When Qs>0.01, the vibration amplitude of the rectangular section is still effectively suppressed. However, due to the excessive inspiratory flow, the thickness of the boundary layer on the side surface becomes smaller, and the shear effect in the boundary layer becomes stronger, which leads to the enhancement of the wake vortex on the leewards, and finally leads to the increase of the lift and drag coefficient of the rectangular section.

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罗楚钰,曾梦竹,王响军,韩艳.基于表面吸气的矩形截面涡激振动抑制及机理研究[J].动力学与控制学报,2023,21(6):72~80; . VIV Suppression and Mechanism Analysis Based on The Surface Aspiration of Rectangular Section[J]. Journal of Dynamics and Control,2023,21(6):72-80.

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  • 收稿日期:2023-04-11
  • 最后修改日期:2023-05-31
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  • 在线发布日期: 2023-07-04
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