The double cantilever beam (DCB) tests were executed for stitched CFRP laminates to evaluate the interlaminar fracture toughness (G
IC). The stitch parameters (stitch line spacing and pitch spacing) were changed and their effects on interlaminar fracture toughness were examined by means of DCB tests and FEM analysis. Different shape patterns in load-crack opening displacement (COD) curves were obtained at one level of equivalent stitch density for several specimens. It can be concluded that the difference in load-COD curve shape was affected by the stitch parameters. On the other hand, G
ICvalues themselves were not so seriously affected by the shape of load-COD curves. Interlaminar fracture toughness is mainly governed by the stitch density, in other words, increase in stitch density in laminates leads to the improvement in G
ICt. Simple FEM model tuned for unstitched and single stitch line DCB specimens was presented. FEM analysis results in linear relationship the between interlaminar fracture toughness of stitched CFRP laminates and the stitch density. Moreover, G
ICA of CFRP laminates with arbitrary stitched parameter can be predicted by the simple FEM model.
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