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Comparison of 2D finite element modeling assumptions with results from 3D analysis for composite skin-stiffener debonding
Authors:Ronald Krueger  Isabelle L Paris  T Kevin O'Brien  Pierre J Minguet
Affiliation:

a ICASE, NASA Langley Research Center, Mail Stop 132C, Hampton, VA 23681-2199, USA

b National Research Council, NASA Langley Research Center, Mail Stop 188E, Hampton, VA 23681-2199, USA

c US Army Research Laboratory, Vehicle Technology Directorate, NASA Langley Research Center, Mail Stop 188E, Hampton, VA 23681-2199, USA

d The Boeing Company, PO BOX 16858, MS P38-13, Philadelphia, PA 19142-0858, USA

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.
Keywords:
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