A methodology is presented for measuring interface fracture properties of c
omposite materials. A bimaterial Brazilian disk specimen with a crack along
the interface is employed. The specimen is analyzed by means of the finite
element method and a conservative integral to determine stress intensity f
actors as a function of loading angle and crack length. A weight function i
s employed to determine the effect of residual curing stresses on the stres
s intensity factors. These are combined to determine the critical interface
energy release rate g(ic) as a function of stress intensity phase angle Ps
i for tests carried out on a glass/epoxy material pair.