Abstract

More and more air-supported structures are used. However,the current wind load shape coefficient can not match engineering design. The CFD technology is utilized to simulate the wind load pressure distribution of rigid half cylindrical shape used for air-supported structures frequently. The shape is found by finite element software ANSYS, and then put into the flow field. RNG ĸ-ε turbulence model based on the Reynolds averaging method and FLUENT software are chose to investigate wind load variation along different wind direction (0°, 30°, 60°, 90°). The results show that the distribution range of extreme negative pressure area is from - 0.9 to - 1.01 at different wind direction angles, and it is easy to separate and form extreme negative pressure area at the two corners close to the windward side. Therefore, enough attention should be paid to the extreme positive pressure area at the bottom of the windward side and the extreme negative pressure area at the top of the membrane face.

Highlights

  • More and more air-supported structures are used

  • The results show that the distribution range of extreme negative pressure area is from - 0.9 to - 1.01 at different wind direction angles, and it is easy to separate and form extreme negative pressure area at the two corners close to the windward side

  • [4] 杨庆山,刘瑞霞.薄膜结构气弹动力稳定性研究[J].工程力学, 2006, 23(9):18-24

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Summary

Introduction

More and more air-supported structures are used. ,the current wind load shape coefficient can not match engineering design. 摘要:近年来充气膜结构应用越来越多,然而现行荷载规范中的风荷载体形系数并不能满足工程设计应用的需要。本 文采用数值模拟方法,运用CFD技术对截圆柱形充气膜结构模型进行绕流风场的数值模拟,分析其表面风荷载分布规 律。通过有限元软件ANSYS对膜结构找形,然后将其导入到流场域中,从而建立起充气膜结构绕流问题的计算模型。 选用基于雷诺平均法(RANS)的RNG ĸ-ε湍流模型,分析不同风向角(0°,30°,60°,90°)时截圆柱形充气膜结构的风荷载 云图,得到不同风向角下,膜面极值负压区分布范围为-0.9~-1.01,在离迎风面最近的两个拐角处,容易发生分离现象, 形成极值负压区。因此在设计时,要对迎风面底端的极值正压区和膜面顶部的极值负压区给予足够重视。 感[1,2,3],风荷载在其设计中往往起到控制作用。而现行荷

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