Numerical analysis of intralaminar failure mechanisms in composite structures. Part I: FE implementation

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154 Citations (Scopus)

Abstract

This paper presents a three-dimensional continuum damage mechanics-based material model which was implemented in an implicit finite element code to simulate the progressive intralaminar degradation of fibre reinforced laminates. The damage model is based on ply failure mechanisms and uses seven damage variables assigned to tensile, compressive and shear damage at a ply level. Non-linear behaviour and irreversibility were taken into account and modelled. Some issues on the numerical implementation of the damage model are discussed and solutions proposed. Applications of the methodology are presented in Part II [1].
Original languageEnglish
Pages (from-to)1039-1046
Number of pages8
JournalComposite Structures
Volume93
Issue number2
DOIs
Publication statusPublished - 2011
Externally publishedYes

Keywords

  • Damage mechanics Finite element analysis (FEA) Modelling Non-linear behaviour Continuum damage mechanics Mechanics Paper laminates Quality assurance Structure (composition) Three dimensional Damage model Damage variables Failure mechanism Fibre reinforced Finite element codes Material models Nonlinear behaviours Numerical implementation Shear damage Finite element method

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