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中国博士后科学基金(200801290)

作品数:4 被引量:13H指数:2
相关作者:王长国杜星文赫晓东谭惠丰杜振勇更多>>
相关机构:哈尔滨工业大学更多>>
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受弯充气锥台的褶皱特性分析被引量:7
2011年
充气锥台是空间充气膜结构的主要承载力构件单元之一,膜面褶皱是导致其承载力降低的关键因素。该文基于薄膜理论分析了受弯充气锥台的褶皱特性。借助褶皱的应力判定准则对褶皱特征参数进行了预报,得到了初始起皱位置和起皱力随充气锥台两端半径比的变化规律,并得到了数值分析结果的验证。该文的结果为空间充气薄膜结构的承载能力预报提供重要依据。
杜振勇王长国谭惠丰
关键词:充气结构褶皱
A new model for wrinkling and collapse analysis of membrane inflated beam被引量:2
2010年
A new model is proposed to accurately predict the wrinkling and collapse loads of a membrane inflated beam.In this model,the pressure effects are considered and a modified factor is introduced to obtain an accurate prediction.The former is achieved by modifying the pressure-related structural parameters based on elastic small strain considerations,and the modified factor is determined by our test data.Compared with previous models and our test data,the present model,named as shell-membrane model,can accurately predict the wrinkling and collapse loads of membrane inflated beams.
Chang-Guo WangHui-Feng TanXing-Wen DuXiao-Dong He
关键词:充气梁起皱修正因子
充气薄膜管的弯皱行为分析被引量:8
2009年
基于Stein-Hedgepeth褶皱理论,并通过引入"收缩系数"表征了膜结构褶皱形变特性,联合褶皱时的应力平衡条件完成了充气膜结构褶皱分析。将方法拓展应用于充气薄膜管情况,分析了充气管结构的弯皱变形特性,得到了临界皱曲弯矩和失效弯矩,并分析了弯矩随管半径和气压的变化规律。通过弯皱试验与分析结果进行比较,验证了分析结果的准确性。
王长国杜星文赫晓东
关键词:充气结构充气管褶皱
Pseudo-beam method for compressive buckling characteristics analysis of space inflatable load-carrying structures被引量:1
2009年
This paper extends Le van's work to the case ofnonlinear problem and the complicated configuration. Thewrinkling stress distribution and the pressure effects are alsoincluded in our analysis. Pseudo-beam method is presentedbased on the inflatable beam theory to model the inflatablestructures as a set of inflatable beam elements with a pre-stressedstate. In this method, the discretized nonlinearequations are given based upon the virtual work principlewith a 3-node Timoshenko's beam model. Finite elementsimulation is performed by using a 3-node BEAM 189 elementincorporating ANS YS nonlinear program. The pressureeffect is equivalent included in our method by modifyingbeam element cross-section parameters related to pressure.A benchmark example, the bending case of an inflatable cantileverbeam, is performed to verify the accuracy of our proposedmethod. The comparisons reveal that the numericalresults obtained with our method are close to open publishedanalytical and membrane finite element results. The methodis then used to evaluate the whole buckling and the load-carryingcharacteristics of an inflatable support frame subjectedto a compression force. The wrinkling stress and regioncharacteristics are also shown in the end. This method givesbetter convergence characteristics, and requires much lesscomputation time. It is very effective to deal with the whole load-carrying ability analytical problems for large scaleinflatable structures with complex configuration.
Changguo Wang Huifeng Tan Xingwen Du Center for Composite Materials,Harbin Institute of Technology, 150001 Harbin, China
关键词:充气结构非线性方程组大型复杂结构
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