Application of a new empirical model of nonlinear self-excited force to torsional vortex-induced vibration and nonlinear flutter of bluff bridge sections. Issue 205 (October 2020)

• Record Type: Journal Article
• Authors: Gao, Guangzhong; Zhu, Ledong; Li, Jiawu; Han, Wanshui
• Is Part Of: Journal of wind engineering and industrial aerodynamics. Issue 205(2020)
• Publication Date: 2020-10
• Subjects: Soft flutter -- Vortex-induced vibration -- Universal self-excited force model -- Aerodynamic nonlinearity -- Two-edge-box girder; Wind-pressure -- Periodicals; Buildings -- Aerodynamics -- Periodicals; Pression du vent -- Périodiques; Constructions -- Aérodynamique -- Périodiques; Buildings -- Aerodynamics; Wind-pressure; Periodicals
• DOI: 10.1016/j.jweia.2020.104313
• Languages: English
• ISSNs: 0167-6105

Abstract

Abstract: 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. Highlights: A universal empirical model of torsional VIV and nonlinear flutter is proposed. A novel measurement technique of aerodynamic force was employed to measure nonlinear self-excited torque. The nonlinear damping mechanism during torsional VIV and soft flutter is investigated.