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Civil-Comp Proceedings
ISSN 1759-3433
CCP: 41
ADVANCES IN THE ANALYSIS AND DESIGN OF COMPOSITES
Edited by: B.H.V. Topping
Paper III.1

Delamination Analysis of Thin Composite Structures using a Multi-Director Formulation

F. Gruttmann and W. Wagner

Institute of Statics, University of Karlsruhe (TH), Karlsruhe, Germany

Full Bibliographic Reference for this paper
F. Gruttmann, W. Wagner, "Delamination Analysis of Thin Composite Structures using a Multi-Director Formulation", in B.H.V. Topping, (Editor), "Advances in the Analysis and Design of Composites", Civil-Comp Press, Edinburgh, UK, pp 51-59, 1996. doi:10.4203/ccp.41.3.1
Abstract
A numerical model for the nonlinear analysis of laminated shells is presented. The developed isoparametric layered shell element is based on a multi-director formulation. Piecewise polynomial functions are used to interpolate the displacement field through the thickness. Thus the developed element is able to predict the complete stress state. Within a nonlinear static analysis onset of delamination is described by exploiting a stress based fracture criterion between adjacent layers. Additional nodal variables are introduced to describe the vector of crack opening displacement. Crack propagation and the final delamination zone for a prescribed load level is achieved by fulfilment of the weak form of equilibrium and of the fracture criterion.

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