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长方体充气膜结构设计简化计算方法研究
引用本文:江锡虎,袁敏,谢步瀛,朱保兵.长方体充气膜结构设计简化计算方法研究[J].合肥工业大学学报(自然科学版),2006,29(4):471-474.
作者姓名:江锡虎  袁敏  谢步瀛  朱保兵
作者单位:1. 同济大学,土木工程学院,上海,200092
2. 合肥工业大学,机械与汽车工程学院,安徽,合肥,230009
摘    要:文章以非线性有限元知识为基础,对非线性有限元迭代方法简化,对不同荷载工况下结构的膜面应力和顶点最大位移等基本结构变化特性进行分析,得出模型的荷载-变形关系;并与ANSYS分析软件的分析结果进行比较,二者结果较为接近,证明了该文充气膜结构的简化有限元迭代方法正确性与可靠性。

关 键 词:充气膜结构  几何大变形  非线性  荷载  变形  模态
文章编号:1003-5060(2006)04-0471-04
修稿时间:2005年5月20日

Simplified calculation for air-supported membrane construction design
JIANG Xi-hu,YUAN Min,XIE Bu-ying,ZHU Bao-bing.Simplified calculation for air-supported membrane construction design[J].Journal of Hefei University of Technology(Natural Science),2006,29(4):471-474.
Authors:JIANG Xi-hu  YUAN Min  XIE Bu-ying  ZHU Bao-bing
Abstract:In light of the geometrical large deformation and small strain of the air-supported structure and on the basis of the non-linear finite element iteration method,different loading conditions including snow load and wind load are simplified,the membrane stress and the largest displacement of the chosen membrane with certain interior pressure are analyzed,and the load-deformation relations of the structure are obtained.The relevant calculation formulas are also given.The results of analysis by using the ANSYS software with the triangle finite element are compared with those by using the simplified calculation method,which turns out to be very close.It is thought that the presented simplification method based on the non-linear finite element iteration method is right and feasible.
Keywords:air-supported membrane structure  geometrical large distortion  non-linearity  loading  deforming  mode
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