Flow field characteristics and vibration response of ortho-hexagonal air-supported membrane structures

IF 3.9 2区 工程技术 Q1 ENGINEERING, CIVIL
Dong Li , Ziming Wang , Mingxuan Lin , Hongwei Huang , Hongguang Xu , Jie Zhao , Feng Zhang
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引用次数: 0

Abstract

The fluid-structure interaction (FSI) effects existing in air-supported membrane roofs subjected to wind loading are significant, which would result in the vortex-induced resonance. This study employs the particle image velocimetry (PIV) technique to systematically explore the FSI mechanism of open-typed hexagonal inflatable membrane structures, with different Reynolds numbers and angles of attack considered. The PIV system is utilized to visualize and capture the surrounding flow field characteristics, including vortex separation, turbulence intensity, and eddy structures. Simultaneously, the aeroelastic responses of the membrane structure are comprehensively analyzed in both time and frequency domains, such as the displacement statistic, vibration frequency, damping ratio, and vibration mode. By integrating the fluid spatiotemporal evolution and structural dynamics, it is indicated that the angle of attack plays a pivotal role in FSI effects. It is indicated that as the angle of attack increases, the position of vortex separation shifts from the trailing edge to the leading edge of the membrane surface. This trend would enhance the FSI effect and trigger the vortex-induced vibration (VIV). In the case of large angle of attack (20°) and Reynolds number (4.55 ×105), the vortex structure develops more sufficiently, with its diameter enlarged and quantity increased significantly. The VIV phenomenon can be observed on the leeward side of the membrane when the reduced wind speed is close to 1.95, characterized by an obvious amplitude jump, a sharp reduction of damping ratios, and frequency lock-in.
正六边形空气支撑膜结构的流场特性和振动响应
空气支撑膜屋盖在风荷载作用下存在显著的流固耦合效应,会导致涡激共振。本研究采用粒子图像测速(PIV)技术,系统探讨了考虑不同雷诺数和攻角的开型六方充气膜结构的FSI机理。PIV系统用于可视化和捕获周围流场特征,包括旋涡分离、湍流强度和涡流结构。同时,从位移统计量、振动频率、阻尼比、振型等时域和频域对膜结构的气弹性响应进行了综合分析。通过对流体时空演化和结构动力学的综合分析,表明攻角在FSI效应中起着关键作用。结果表明,随着迎角的增大,涡分离的位置由尾缘向膜面前缘转移。在大迎角(20°)和雷诺数(4.55 ×105)情况下,涡结构发展更加充分,涡直径增大,涡量显著增加。当减小风速接近1.95时,膜背风侧出现了涡激振荡现象,表现为振幅跳变明显,阻尼比急剧减小,频率锁定。
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来源期刊
Structures
Structures Engineering-Architecture
CiteScore
5.70
自引率
17.10%
发文量
1187
期刊介绍: Structures aims to publish internationally-leading research across the full breadth of structural engineering. Papers for Structures are particularly welcome in which high-quality research will benefit from wide readership of academics and practitioners such that not only high citation rates but also tangible industrial-related pathways to impact are achieved.
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