Model of composite laminated thin plate based on modified couple stress theory and buckling analysis of scale effects

被引：0
作者：
Li, Li [1 ,3 ]
Chen, Wan-Ji [1 ,2 ]
Zheng, Nan [2 ]
机构：
[1] State Key Laboratory for Structural Analysis of Industrial Equipment, Dalian University of Technology
[2] Key Laboratory of Liaoning Province for Composite Structural Analysis of Aerocraft and Simulation, Shenyang Aerospace University
[3] Physics and Biophysics Department, China Medical University
来源：
Gongcheng Lixue/Engineering Mechanics | 2013年 / 30卷 / 05期
关键词：
Anisotropic constitute relations; Buckling; Composite laminated thin plate; Modified couple stress theory; Scale effects;
D O I：
10.6052/j.issn.1000-4750.2011.11.0750
中图分类号：
学科分类号：
摘要：
The modified couple stress theory (C1 theory) in the isotropic elasticity is extended to anisotropic composite laminated plate. Based on virtual principle, a new model is established for a single layer of composite laminated thin plate involving two material characteristic length constants. In the theory the form of new curvature tensor is asymmetric, however it can result in the same symmetric curvature tensor as in the isotropic elasticity. More simplified model for cross-ply composite laminated thin plate involving one material length constant is applied to the buckling analysis. Numerical results show that the present plate model can capture the scale effects of buckling analysis in microstructures.
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页码：1 / 7
页数：6
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