In this study, a method of finite element analysis is presented to examine
the three-dimensional inelastic behaviour of fibre-reinforced composite lam
inates with damage. The constitutive model for the characterization of mech
anical responses of non-linear composite materials to damage that was propo
sed recently by the authors is employed. The formulation of the elastic dam
age stress-strain relationship in incremental form is first developed and t
hen incorporated within the context of the displacement-based finite elemen
t procedure. Solution of the non-linear equilibrium equations is obtained w
ith the modified Newton-Raphson iteration technique. Numerical implementati
on of the stress calculation is discussed in detail. Results predicted usin
g the present finite element program for uniaxial off-axis tensile loading
of unidirectional graphite/epoxy composite laminates show satisfactory agre
ement with those obtained from experiments. Other results describing the de
velopment of damage zones, the inelastic effect on stress distributions and
material property variations due to damage in cross-ply laminated composit
e structures are also examined and discussed.