This paper investigates the low-velocity impact behaviour and impact-induce
d damages in graphite/epoxy composite laminates. A three-dimensional finite
element and transient dynamic analysis is performed to calculate the time-
varying displacements, forces, strains and stresses throughout the laminate
resulting from transverse impact. A layered version of an eight-noded isop
arametric brick element with incompatible modes is used to model the lamina
te. Transient dynamic equilibrium equation is integrated step-by-step with
respect to time using Newmark direct time integration method. Modified Hert
zian contact law is used to model the local contact behaviour. Appropriate
three-dimensional failure criteria are used for predicting the occurrence o
f matrix cracking and the extent of delamination after impact.