【24h】

UNST EADY AERODYNAMIC MODELING AND FLUTTER ANALYSIS OF LONG-SPAN SUSPENSION BRIDGES

机译:大跨度悬索桥的不稳定气动建模与颤振分析

获取原文

摘要

A parametric one-dimensional model of suspension bridges is employed to investigate their static and dynamic aeroelastic behavior in response to a gust load and at the onset of flutter. The equilibrium equations are obtained via a direct total Lagrangian formulation where the kinematics for the deck, assumed to be linear, feature the vertical and the chord-wise displacements of the deck mean axis and the torsional rotations of the deck cross sections, while preserving their shape during rotation. The cables elasto-geometric stiffness contribution is obtained by condensing the equilibrium in the longitudinal direction assuming small horizontal displacements and neglecting the cable kinematics along the bridge chord-wise direction. The equations of motion are linearized about the prestressed static aeroelastic configuration and are obtained via an updated Lagrangian formulation.The equations of motion governing the structural dynamics of the bridge are coupled with the incompressible unsteady aerodynamic model obtained by a set of reduced-order indicial functions developed for the cross section of a suspension bridge, here represented by a rectangular cross-section. The space dependence of the governing equations is treated using the Galerkin approach borrowing as set of trial functions, the eigenbasis of the modal space. The time integration is subsequently performed by using a numerical scheme that includes the modal reduced dynamic aeroelastic Ordinary Differential Equations (ODEs) and the added aerodynamic states also represented in ODE form, the latter being associated with the lag-state formulation pertinent to the unsteady wind-induced loads.The model is suitable to analyze the effect of a time and space non uniform gust load distributed on the bridge span. The obtained aeroelastic system is also suitable to study the onset of flutter and to investigate the sensitivity of the flutter condition on geometrical and aerodynamic parameters. The flutter instability is evaluated using appropriate frequency and time domain characteristics. The parametric continuum model is exploited to perform dynamic aeroelastic flutter analysis and gust response of the Runyang Suspension Bridge over the Yangtze river in China.
机译:悬索桥的参数一维模型用于研究其响应阵风载荷和颤振开始时的静态和动态气动弹性行为。平衡方程是通过直接的总拉格朗日公式获得的,假设甲板的运动学假定为线性,则以甲板平均轴的垂直和弦向位移以及甲板横截面的扭转旋转为特征。旋转过程中的形状。缆索的弹性刚度贡献是通过在假定水平方向位移较小的情况下沿纵向方向压缩平衡并忽略沿桥弦方向的缆索运动学来获得的。通过更新的拉格朗日公式将运动方程线性化,并通过更新的拉格朗日公式获得。将控制桥梁结构动力学的运动方程与通过一组降阶的局部函数获得的不可压缩的非定常空气动力学模型相结合为悬索桥的横截面而开发,此处以矩形横截面表示。控制方程的空间依赖性使用Galerkin方法作为试验函数集(模态空间的本征基)进行借用。随后,通过使用一种数值方案来执行时间积分,该方案包括模态简化的动态气动弹性常微分方程(ODE)和以ODE形式表示的附加空气动力学状态,后者与与非稳定风有关的滞后状态公式相关联感应荷载:该模型适合分析时空不均匀阵风荷载对桥梁跨度的影响。所获得的气动弹性系统还适合于研究颤振的发生以及研究颤振条件对几何和空气动力学参数的敏感性。使用适当的频域和时域特性评估颤振的不稳定性。利用参数连续体模型对中国长江上游润扬大桥进行了动态气动弹性颤振分析和阵风响应。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号