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