In carbon fibre composite laminated plates, impact of a small mass at
subordnance velocities resulted in three types of initial fractures: y
arn splitting, fibre breakage and delamination. An elastic analysis fo
r stresses developed due to impact against the composite plate has bee
n correlated with observations of fracture initiation in impact experi
ments. Fractures due to yam splitting developed near the periphery of
the contact area due to a tensile radial stress perpendicular to the f
ibres; this type of fracture also occurred near the distal surface as
a result of combined transverse tension and shear on fibres. Under the
striker there was fibre breakage and delamination as well. Criteria w
ere obtained for initiation of yarn splitting in composite plates defo
rmed at high rates.