期刊文献+
共找到2篇文章
< 1 >
每页显示 20 50 100
考虑充气压力的气梁结构变形性能
1
作者 舒浙锋 张安琪 +1 位作者 刘平 付功义 《空间结构》 CSCD 北大核心 2023年第4期35-41,共7页
研究了充气压力的改变对充气梁变形性能的影响.考虑气梁的褶皱,通过数据拟合得到褶皱后惯性矩比与弯矩比的简化关系.同时,假设充气气体符合理想气体压力规律,对气梁结构的变形进行了理论推导,得到考虑充气梁内压影响的位移与弯矩的解析... 研究了充气压力的改变对充气梁变形性能的影响.考虑气梁的褶皱,通过数据拟合得到褶皱后惯性矩比与弯矩比的简化关系.同时,假设充气气体符合理想气体压力规律,对气梁结构的变形进行了理论推导,得到考虑充气梁内压影响的位移与弯矩的解析解.为验证理论的正确性,制作了一个长3.0m、直径0.3m的圆形充气梁,固定其一端从而形成悬臂梁结构.在不同长度、不同充气压力以及不同加载方式下进行了加载试验,得到位移与荷载曲线,同时还测得相应的内压数据.与本文的解析解进行对比,数据符合良好.结果表明,气梁的气压对充气梁结构性能有显著影响.加载方式对气梁位移影响较小,气梁位移与截面弯矩成函数关系.相同位移下,考虑内压时比不考虑内压情况下截面弯矩增加近28%. 展开更多
关键词 气梁结构 褶皱 气压 膜结构 结构稳定
原文传递
Pseudo-beam method for compressive buckling characteristics analysis of space inflatable load-carrying structures 被引量:1
2
作者 Changguo Wang Huifeng Tan Xingwen Du Center for Composite Materials,Harbin Institute of Technology, 150001 Harbin, China 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2009年第5期659-668,共10页
This paper extends Le van's work to the case of nonlinear problem and the complicated configuration. The wrinkling stress distribution and the pressure effects are also included in our analysis. Pseudo-beam method is... This paper extends Le van's work to the case of nonlinear problem and the complicated configuration. The wrinkling stress distribution and the pressure effects are also included in our analysis. Pseudo-beam method is presented based on the inflatable beam theory to model the inflatable structures as a set of inflatable beam elements with a prestressed state. In this method, the discretized nonlinear equations are given based upon the virtual work principle with a 3-node Timoshenko's beam model. Finite element simulation is performed by using a 3-node BEAM189 element incorporating ANSYS nonlinear program. The pressure effect is equivalent included in our method by modifying beam element cross-section parameters related to pressure. A benchmark example, the bending case of an inflatable cantilever beam, is performed to verify the accuracy of our proposed method. The comparisons reveal that the numerical results obtained with our method are close to open published analytical and membrane finite element results. The method is then used to evaluate the whole buckling and the loadcarrying characteristics of an inflatable support frame subjected to a compression force. The wrinkling stress and region characteristics are also shown in the end. This method gives better convergence characteristics, and requires much less computation time. It is very effective to deal with the whole load-carrying ability analytical problems for large scale inflatable structures with complex configuration. 展开更多
关键词 inflatable structure - Pseudo-beam method inflatable beam theory Nonlinear buckling finite element
下载PDF
上一页 1 下一页 到第
使用帮助 返回顶部