Large deformation dynamic finite element analysis of delaminated composite plates using contact-impact conditions

被引:8
作者
Chandrashekhar, M. [1 ]
Ganguli, Ranjan [2 ]
机构
[1] Indian Space Res Org, Ctr Space Applicat, Ahmadabad 380015, Gujarat, India
[2] Indian Inst Sci, Dept Aerosp Engn, Bangalore 560012, Karnataka, India
关键词
Nonlinear response; Finite element method; Composite plates; Delamination; Contact-impact; Augmented Lagrangian formulation; FREE-VIBRATION ANALYSIS; ORDER ZIGZAG THEORY; NONLINEAR DYNAMICS; BEAMS; FORMULATION;
D O I
10.1016/j.compstruc.2014.07.025
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
A new C-0 composite plate finite element based on Reddy's third order theory is used for large deformation dynamic analysis of delaminated composite plates. The inter-laminar contact is modeled with an augmented Lagrangian approach. Numerical results show that the widely used "unconditionally stable" beta-Newmark method presents instability problems in the transient simulation of delaminated composite plate structures with large deformation. To overcome this instability issue, an energy and momentum conserving composite implicit time integration scheme presented by Bathe and Baig is used. It is found that a proper selection of the penalty parameter is very crucial in the contact simulation. (C) 2014 Elsevier Ltd. All rights reserved.
引用
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页码:92 / 102
页数:11
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