Data di Pubblicazione:
2013
Abstract:
In the present paper a three-dimensional Progressive Damage Approach
(PDA) for laminated composites will be presented. This approach is based on the
use of a progressive damage finite element with the geometrically non-linear finite
element formulation for stress calculation. The FEM element has been integrated
with Hashin's failure criteria to split fibre and matrix failure modes and to simulate
stiffness degradation within each ply by means of the Ply Discount Method
(PDM). FEM code previsions, in the case of complex structures with different mesh
densities and element types, were compared with the results obtained using embedded
global-local approach to prove the effectiveness of the implemented code. As
experimental test-case, the structural behaviour of a notched panel, under tensile
load has been investigated. Obtained numerical results have been compared with
both numerical and experimental data, available from the literature. Finally, a comparison
between a full 3D model and a global-local model has been performed in
order to evaluate the effectiveness of the developed progressive damage approach
in global-local analyses..
Tipologia CRIS:
01.01 Articolo in rivista
Keywords:
composites; delamination
Elenco autori:
Zarrelli, Mauro
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