Non-local theory for composite is applied to solve the Mode III crack probl
em under impact loading. The composite is a laminate made up of two differe
nt orthotropic layers. Based on the classical boundary conditions, all quan
tities are expressed in terms of a single unknown function. Integral transf
orm is used to reduce the problem to a system of dual integral equations. T
he solution is obtained by using the Copson's method [1], which can be gene
ralized to include arbitrary loading applied to the crack. (C) 2000 Elsevie
r Science Ltd. All rights reserved.