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Extended layerwise method for laminated composite plates with multiple delaminations and transverse cracks

Published: 01 October 2016 Publication History

Abstract

In this paper, the extended layerwise method (XLWM), which was developed for laminated composite beams with multiple delaminations and transverse cracks (Li et al. in Int J Numer Methods Eng 101:407---434, 2015), is extended to laminated composite plates. The strong and weak discontinuous functions along the thickness direction are adopted to simulate multiple delaminations and interlaminar interfaces, respectively, whilst transverse cracks are modeled by the extended finite element method (XFEM). The interaction integral method and maximum circumferential tensile criterion are used to calculate the stress intensity factor (SIF) and crack growth angle, respectively. The XLWM for laminated composite plates can accurately predicts the displacement and stress fields near the crack tips and delamination fronts. The thickness distribution of SIF and thus the crack growth angles in different layers can be obtained. These information cannot be predicted by using other existing shell elements enriched by XFEM. Several numerical examples are studied to demonstrate the capabilities of the XLWM in static response analyses, SIF calculations and crack growth predictions.

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Cited By

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  • (2019)Geometrically nonlinear analysis of matrix cracking and delamination in composites with floating node methodComputational Mechanics10.1007/s00466-018-1591-863:2(201-217)Online publication date: 1-Feb-2019

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Published In

cover image Computational Mechanics
Computational Mechanics  Volume 58, Issue 4
October 2016
162 pages

Publisher

Springer-Verlag

Berlin, Heidelberg

Publication History

Published: 01 October 2016

Author Tags

  1. Composite laminated plates
  2. Delamination
  3. Layerwise theory
  4. Transverse crack

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  • (2019)Geometrically nonlinear analysis of matrix cracking and delamination in composites with floating node methodComputational Mechanics10.1007/s00466-018-1591-863:2(201-217)Online publication date: 1-Feb-2019

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