In this study, it is shown that a computational procedure, termed "discrete
damage space homogenization method" (DDSHM), can accurately predict the co
nstitutive response of layered composite materials containing growing crack
s. The effective constitutive law for a specific layered composite architec
ture, as defined by the DDSHM, was integrated into the ABAQUS commercial fi
nite element program using the user-defined material feature. Calculations
were performed to show correlation with experimental data on flat laminates
and curved beam elements and to illustrate the computational efficiency of
the method for general analysis of composite materials with growing cracks
. Results show that given the basic information about the fracture toughnes
s of the material, the DDSHM is able to predict important material paramete
rs, including the load at initiation of cracking, damage growth rate, and t
he resulting effect on the macroscopic stiffness. (C) 2001 Elsevier Science
Ltd. All rights reserved.