桥梁主梁弯扭耦合滞回颤振稳定状态评估

STABILITY STATE EVALUATION OF HYSTERESIS FLUTTER OF A BRIDGE GIRDER

  • 摘要: 对于大跨桥梁主梁断面,当来流风速抵达颤振临界点,主梁可能呈现持幅振动现象,即“滞回颤振”(软颤振)。与振幅快速发散的硬颤振不同,滞回颤振时运动与气动力存在非线性效应,结构会出现阶跃、分岔等多种动力学行为。既有针对滞回颤振的研究多是经典线性理论的直接推广,仅关注颤振临界状态之后可能存在的平衡位置,极少讨论系统在到达平衡位置后能否继续维持振幅稳定的滞回振荡。本文结合颤振能量演化方程及一阶快变近似方法,从非线性动力学的角度探究了滞回颤振持幅稳定的内在数学原理,推导了描述滞回颤振状态振幅演化趋势的量化指标——滞回颤振稳定指数,并结合某大跨度桥梁流线型箱梁断面的非线性结构、气动力参数及自由振动试验,验证了该分析方法可以有效评估滞回颤振维持稳定振荡的能力,并阐明了量化指标的物理意义。最后,根据该理论指出了当滞回颤振稳定指数小于零时,即便气动力和结构力在周期内可以平衡,在实际环境中也不会发生稳定的滞回颤振。

     

    Abstract: For girders of large-span bridges, when the incoming wind speed is equal to or surpasses the flutter critical point, the bridge deck exhibits persistent amplitude vibrations, termed "hysteresis flutter" (or soft flutter). Different from hard flutter with rapid increasing amplitudes, soft flutter entails a more intricate coupling with nonlinear effects between motion and aerodynamic forces, resulting in various dynamic states, including step through and bifurcations. Present research comes from the practical extension of classical theories, focusing primarily on the potential equilibrium states which may exist after the flutter critical condition. However, there is little discussion on whether the system can maintain stable amplitude oscillations once it reaches the equilibrium position. This study combines the flutter energy evolution equation with the first-order quasi-static approximation method to explore the intrinsic mathematical principles underlying amplitude stability in hysteretic flutter from a nonlinear perspective of dynamics. It also derives a quantitative indicator, the Hysteretic Flutter Stability Index, which characterizes the amplitude evolution trend of the hysteretic flutter state. By combining the nonlinear structural and aerodynamic characteristics of a streamlined box girder section of a large-span bridge, this study verifies that the analytical method proposed can effectively assess the ability of hysteretic flutter to maintain stable oscillations. Finally, demonstrating by the theory that, even when aerodynamic and structural forces balance within a cycle, stable hysteretic flutter will not occur with an index less than zero in practical environments.

     

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