CORC  > 厦门大学  > 建筑土木-已发表论文
A pure bending exact nodal-averaged shear strain method for finite element plate analysis
Wu, C. T. ; Guo, Y. ; Wang, D. ; Wang DD(王东东)
刊名http://dx.doi.org/10.1007/s00466-013-0937-5
2014
关键词STABILIZED CONFORMING INTEGRATION MESH-FREE METHODS THIN PLATES LOCKING INTERPOLATION FORMULATION ELASTICITY MODEL
英文摘要National Natural Science Foundation of China [11222221]; An averaged shear strain method, based on a nodal integration approach, is presented for the finite element analysis of Reissner-Mindlin plates. In this work, we combine the shear interpolation method from the MITC4 plate element with an area-weighted averaging technique for the nodal integration of shear energy to relieve shear locking in the thin plate analysis as well as to pass the pure bending patch test. In order to resolve the numerical instability caused by the direct nodal integration, the bending strain field is computed by a sub-domain nodal integration approach based on the Sub-domain Stabilized Conforming Integration and a modified curvature smoothing scheme. The resulting nodally integrated smoothed strain formulation is shown to contain only the primitive variables and thus can be easily implemented in the existing displacement-based finite element plate formulation. Several numerical examples are presented to demonstrate the accuracy of the present method.
语种英语
出版者SPRINGER
内容类型期刊论文
源URL[http://dspace.xmu.edu.cn/handle/2288/90015]  
专题建筑土木-已发表论文
推荐引用方式
GB/T 7714
Wu, C. T.,Guo, Y.,Wang, D.,et al. A pure bending exact nodal-averaged shear strain method for finite element plate analysis[J]. http://dx.doi.org/10.1007/s00466-013-0937-5,2014.
APA Wu, C. T.,Guo, Y.,Wang, D.,&王东东.(2014).A pure bending exact nodal-averaged shear strain method for finite element plate analysis.http://dx.doi.org/10.1007/s00466-013-0937-5.
MLA Wu, C. T.,et al."A pure bending exact nodal-averaged shear strain method for finite element plate analysis".http://dx.doi.org/10.1007/s00466-013-0937-5 (2014).
个性服务
查看访问统计
相关权益政策
暂无数据
收藏/分享
所有评论 (0)
暂无评论
 

除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。


©版权所有 ©2017 CSpace - Powered by CSpace