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Conference paper

Finite elements modeling of delaminations in composite laminates

In Advances in Marine Structures — 2011, pp. 133-139

Edited by Fricke, W.

From

University of Genoa1

Wind Turbines, Wind Energy Division, Risø National Laboratory for Sustainable Energy, Technical University of Denmark2

Wind Energy Division, Risø National Laboratory for Sustainable Energy, Technical University of Denmark3

Risø National Laboratory for Sustainable Energy, Technical University of Denmark4

The application of composite materials in many structures poses to engineers the problem to create reliable and relatively simple methods, able to estimate the strength of multilayer composite structures. Multilayer composites, like other laminated materials, suffer from layer separation, i.e., delaminations, which may affect the stiffness and stability of structural components.

Especially deep delaminations in the mid surface of laminates are expected to reduce the effective flexural stiffness and lead to collapse, often due to buckling behaviour. This paper deals with the numerical modelling of the buckling strength of composite laminates containing delaminations. Namely, non-linear buckling and post-buckling analyses are carried out to predict the critical buckling load of elementary composite laminates affected by rectangular delaminations of different sizes and locations, which are modelled by finite elements using different techniques.

Results obtained with different finite element models are compared and discussed.

Language: English
Publisher: Taylor & Francis
Year: 2011
Pages: 133-139
Proceedings: 3rd International Conference on Marine Structures
ISBN: 0203808118 , 0415677718 , 0429212836 , 1322627150 , 9780203808115 , 9780415677714 , 9780429212833 and 9781322627151
Types: Conference paper
DOI: 10.1201/b10771-1
ORCIDs: Branner, Kim

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