New higher order plate theory in modeling delamination buckling of composite laminates

AIAA Journal ◽  
1994 ◽  
Vol 32 (8) ◽  
pp. 1709-1716 ◽  
Author(s):  
Aditi Chattopadhyay ◽  
Haozhong Gu
2020 ◽  
Vol 12 (4) ◽  
pp. 168781402091536
Author(s):  
Zhaotian Wu ◽  
Chuwei Zhou

In this article, a finite element model of multi-layer composite laminates with delamination based on higher order zig-zag theory is studied for the progressive delamination analysis. The degrees of freedom are simplified by the continuity conditions of shear stress between layers and the free-surface conditions at the bottom and top of laminates. The numbers of degrees of freedom are not reduced with this method while the model can take the initiation of delamination into consideration in return. Static loading analysis is implemented to simulate the performance in delamination resistance with two different plies and under two different boundary conditions. The present model can present good performance in the prediction of delamination phenomenon.


2008 ◽  
Vol 39 (2) ◽  
pp. 414-427 ◽  
Author(s):  
J.R. Xiao ◽  
D.F. Gilhooley ◽  
R.C. Batra ◽  
J.W. Gillespie ◽  
M.A. McCarthy

2017 ◽  
Vol 168 ◽  
pp. 143-152 ◽  
Author(s):  
C. Thurnherr ◽  
R.M.J. Groh ◽  
P. Ermanni ◽  
P.M. Weaver

Author(s):  
S. Ramaswamy ◽  
Zahoor Ahmed Shariff ◽  
A. Abdul Munaf ◽  
I. Jerin Leno ◽  
S. Joe Patrick Gnanaraj ◽  
...  

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