Application of a new empirical model of nonlinear self-excited force to torsional vortex-induced vibration and nonlinear flutter of bluff bridge sections

被引:41
作者
Gao, Guangzhong [1 ,2 ]
Zhu, Ledong [2 ,3 ,4 ]
Li, Jiawu [1 ]
Han, Wanshui [1 ]
机构
[1] Changan Univ, Highway Coll, Xian 710064, Shaanxi, Peoples R China
[2] Tongji Univ, Dept Bridge Engn, Shanghai 200092, Peoples R China
[3] Tongji Univ, State Key Lab Disaster Reduct Civil Engn, Shanghai 200092, Peoples R China
[4] Tongji Univ, Key Lab Transport Ind Bridge Wind Resistance Tech, Shanghai 200092, Peoples R China
基金
中国国家自然科学基金; 国家重点研发计划;
关键词
Soft flutter; Vortex-induced vibration; Universal self-excited force model; Aerodynamic nonlinearity; Two-edge-box girder; OSCILLATING SQUARE PRISM; FLUCTUATING PRESSURES;
D O I
10.1016/j.jweia.2020.104313
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
Long-span bridges are susceptible to vortex-induced vibration (VIV) and flutter in different reduced wind range. Currently, VIV and flutter are considered as two different types of wind-induced vibration and different empirical models were proposed. The possibility of building a universal empirical model for both torsional VIV and nonlinear flutter was explored. In the previous study, a new empirical model was proposed for describing aerodynamic nonlinearities during soft flutter of a bluff bridge section with a medium side ratio. In this study, the empirical model was refined and extended to both torsional VIV and nonlinear flutter for a general bluff body, especially for a flat bridge deck, which is more common in long-span bridges. In the empirical model, aerodynamic nonlinear damping effect was modeled by a cubic velocity term and its applicability was validated by a series of elastically-mounted sectional model tests of a flat twin-side-girder bridge deck. The results indicated that the proposed empirical model was suitable for predicting the stable amplitude of torsional VIV and nonlinear flutter, although the motion-induced "pure force" varies with side ratios. It was found that torsional VIV and soft flutter share the same nonlinear damping mechanism during the development of LCO.
引用
收藏
页数:15
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