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Comparison of 2D finite element modeling assumptions with results from 3D analysis for composite skin-stiffener debonding

Authors :
T. Kevin O'Brien
Ronald Krueger
Pierre J. Minguet
Isabelle Paris
Source :
Composite Structures. 57:161-168
Publication Year :
2002
Publisher :
Elsevier BV, 2002.

Abstract

The influence of two-dimensional finite element modeling assumptions on the debonding prediction for skin-stiffener specimens was investigated. Geometrically nonlinear finite element analyses using two-dimensional plane-stress and plane-strain elements as well as three different generalized plane-strain type approaches were performed. The computed skin and flange strains, transverse tensile stresses and energy release rates were compared to results obtained from three-dimensional simulations. The study showed that for strains and energy release rate computations the generalized plane-strain assumptions yielded results closest to the full three-dimensional analysis. For computed transverse tensile stresses the plane-stress assumption gave the best agreement. Based on this study it is recommended that results from plane-stress and plane-strain models be used as upper and lower bounds. The results from generalized plane-strain models fall between the results obtained from plane-stress and plane-strain models. Two-dimensional models may also be used to qualitatively evaluate the stress distribution in a ply and the variation of energy release rates and mixed mode ratios with delamination length. For more accurate predictions, however, a three-dimensional analysis is required.

Details

ISSN :
02638223
Volume :
57
Database :
OpenAIRE
Journal :
Composite Structures
Accession number :
edsair.doi...........6c66924c90a594f8bf6a53b23a61badf
Full Text :
https://doi.org/10.1016/s0263-8223(02)00079-x