International Journal of Aerospace Engineering (Jan 2009)

A Three-Dimensional Ply Failure Model for Composite Structures

  • Maurício V. Donadon,
  • Sérgio Frascino M. de Almeida,
  • Mariano A. Arbelo,
  • Alfredo R. de Faria

DOI
https://doi.org/10.1155/2009/486063
Journal volume & issue
Vol. 2009

Abstract

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A fully 3D failure model to predict damage in composite structures subjected to multiaxial loading is presented in this paper. The formulation incorporates shear nonlinearities effects, irreversible strains, damage and strain rate effects by using a viscoplastic damageable constitutive law. The proposed formulation enables the prediction of failure initiation and failure propagation by combining stress-based, damage mechanics and fracture mechanics approaches within an unified energy based context. An objectivity algorithm has been embedded into the formulation to avoid problems associated with strain localization and mesh dependence. The proposed model has been implemented into ABAQUS/Explicit FE code within brick elements as a userdefined material model. Numerical predictions for standard uniaxial tests at element and coupon levels are presented and discussed.