The region around a terminated ply is modeled as several elastic layer
s separated by shear regions. A shear-lag analysis is then performed a
llowing for the thickness of the elastic and shear layers to vary. Bou
ndary conditions, away from the ply drop, are based on the deflections
determined by a finite element model. The interlaminar stresses are c
ompared against those generated by the finite element model for tapere
d laminates under pure extension, pure bending, and extension-bending
coupling. The shear-lag analysis predicts the interlaminar shear at an
d near the ply drop for pure extension and in cases involving bending
if the deflections due to bending are removed. The interlaminar shear
stress and force equilibrium are used to determine the interlaminar no
rmal stress. The trends in the interlaminar normal stress shown by the
finite element model are partially captured by the shear-lag analysis
. This simple analysis indicates that the mechanism for load transfer
about a ply drop is primarily due to shear transfer through the resin-
rich areas.