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Wind and Structures
  Volume 39, Number 5, November 2024 , pages 313-327
DOI: https://doi.org/10.12989/was.2024.39.4.313
 


Aeroelastic wind tunnel tests and numerical simulations on umbrella-shaped tensioned membrane structures in typhoons
Dong Li, Zhou Zhang, Yi Qiu, Zhiwei Chen and Zhichao Lai

 
Abstract
    This paper presents the wind tunnel test and numerical simulation on umbrella-shaped tensioned membrane structures to investigate the effects of both high wind velocity and various wind direction of typhoon on their aerodynamic behavior. Finite element models are also developed and benchmarked to further investigate the effects on rise-to-span ratio, wind attack angle, and pretension. Results from the experimental tests and finite element analyses show that: (i) the turbulence buffeting in the leeward surface is significant with large displacement responses, especially with the 0° wind direction, large wind attack angle and high rise-to-span ratio; (ii) Non-Gaussian characteristics become remarkable with increasing skewness and kurtosis, which may be contributed by the high-level turbulence intensity in typhoons; and (iii) the effects of rise-to-span ratio, wind attack angle and pretension are proved more significant, which should be considered in the wind-resistance design of membrane structures in typhoons.
 
Key Words
    aerodynamic behavior; coupled FSI simulation; typhoons; umbrella-shaped membrane structures; wind tunnel test
 
Address
Dong Li:1)College of Civil Engineering, Fuzhou University, Fuzhou 350116, China
2)Key Laboratory of Fluid and Power Machinery (Xihua University), Ministry of Education, Chengdu 610039, China
3)School of Advanced Manufacturing, Fuzhou University, Jinjiang 362251, China

Zhou Zhang:School of Advanced Manufacturing, Fuzhou University, Jinjiang 362251, China

Yi Qiu:College of Civil Engineering, Fuzhou University, Fuzhou 350116, China

Zhiwei Chen:Kaihui Group Co., Ltd, Putian 351100, China

Zhichao Lai:College of Civil Engineering, Fuzhou University, Fuzhou 350116, China
 

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