Through-the-thickness stitching dramatically improves the interlaminar frac
ture toughness of laminated composites. Currently the Double Cantilever Bea
m (DCB) test is being used for determining the Mode I interlaminar fracture
toughness of unstitched and lightly stitched composite laminates. But the
standard DCB test method is not suitable for laminates with medium to high
density s titches. Due t o the high bending moment at the crack-tip, the sp
ecimens fail due to compressive stresses before the delamination could prop
agate. In order to overcome this limitation, a new fixture has been develop
ed and used to perform Mode I fracture toughness tests on laminates with hi
gh density stitches. An analysis method has been developed to determine the
load-deflection and the load-energy release rate relationships in the new
test. The new test method has been found to be successful in testing graphi
te/epoxy laminates containing Kevlar stitches with a density of 64 stitches
per square inch. The apparent fracture toughness of these specimens is abo
ut 45 times that of unstitched specimens.