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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 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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