2.2. Analysis of a laminated composite plate The classical lamination theory is used to analyze the mechan-ical behavior of the composite laminate. We assume that plane stress condition is valid for each ply. Accordingly, out-of-plane stress components are taken as zero. With respect to the coordi-

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creating 11 cross-ply composite laminate plates with [0,90,0,90] s orientation. Delaminated regions were placed at one inch increments, horizontally along the specimen. During testing, one side of each composite laminate plates were clamped using a custom fabricated fixture, cantilevered leaving the remaining edges free.

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