A 2D equivalent single-layer formulation for the effect of transverse shear on laminated plates with curvilinear fibres

R. M. J. Groh*, P. M. Weaver, S. White, G. Raju, Z. Wu

*Corresponding author for this work

Research output: Contribution to journalArticle (Academic Journal)peer-review

27 Citations (Scopus)

Abstract

The Hellinger-Reissner mixed variational principle in conjunction with Lagrange multipliers is used to model transverse shear stresses, in bending of variable stiffness laminated plates, using a reduced two-dimensional formulation. The effect of transverse shear stresses on the bending deflection of variable angle tow (VAT) laminates is assessed. The novel formulation features multiple shear correction factors that are functions of the bending rigidity terms D-ij, their first and second derivatives and the Timoshenko shear factor chi. The new set of governing equations are solved, in their strong form, using the Differential Quadrature Method (DQM) and the accuracy and robustness of the solution technique verified using a 2D "thick" shell and 3D high-fidelity finite element model. The derived theory is superior to the "thick" 2D shell model in capturing transverse shear effects and shows good accuracy compared to the full 3D solution for thicknesses within the range of practical engineering laminates. The derived equations degenerate to Classical Laminate Analysis for very thin configurations but discrepancies as large as 43% are observed for span-to-thickness ratios of 10:1. Finally, the specific VAT panels under investigation are affected more by transverse shear deformation than a corresponding homogeneous quasi-isotropic laminate. (C) 2013 Elsevier Ltd. All rights reserved.

Original languageEnglish
Pages (from-to)464-478
Number of pages15
JournalComposite Structures
Volume100
DOIs
Publication statusPublished - 1 Jun 2013

Keywords

  • INPLANE
  • COMPOSITE PLATES
  • Differential Quadrature Method
  • FORMAT
  • Transverse shear deformation
  • Tow steering
  • SHELLS

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