摘要
为确定充气膜结构找形分析时,在内压已知情况下膜面张力的大小,根据多元函数泰勒展开公式推导了该类结构充气膨胀的体积微分方程,并由基于U.L.格式的非线性有限单元法,建立了以节点位移和膜面初始张力为未知量的平衡方程,编制了在给定内部气压及膨胀体积情况下的找形分析程序。对球面及圆柱面充气膜结构进行了找形计算,得到的数值结果与由球面及圆柱面的矢高、内压、初始张力相互关系得到的理论解进行比较并得到了验证。计算结果表明,提出的基于有限元的体积微分法可有效的用于充气膜结构的找形分析。
In order to determine the initial stress of pneumatic membrane structures in form-finding analysis in the condition that the internal pressure is given, the Taylor Expansion of a multi-variable function is used to establish the volume differential equation. With the nonlinear finite element method based on Updated Lagranglan formulations, this paper presents a new approach to calculate the nodal displacements and initial stress in pneumatic membrane structures form-finding analysis. A numerical procedure has been developed and two air supported membrane structures are selected as the analytical models. By comparing the numerical results with the corresponding theoretical results, the validity of the presented approach is shown.
出处
《四川大学学报(工程科学版)》
EI
CAS
CSCD
北大核心
2007年第5期49-52,共4页
Journal of Sichuan University (Engineering Science Edition)
基金
上海市科委浦江人才计划资助项目(05PJ14091)
关键词
泰勒展开
充气膜结构
体积微分
找形分析
Taylor Expansion
volume differential
pneumatic membrane structures
form-finding analysis