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Effects of Boundary Conditions on Postbuckling Strengths of Composite Laminate with Various Shaped Cutouts under In Plane Shear

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Figure

Table 1. Material Properties of T300/5208 (pre-peg) graph- ite-epoxy.
Table 3. Convergence study.
Figure 2. Meshing of a square laminate without cutout showing element- and node-numbering scheme
Figure 4. Meshing of square laminate with: (a) Diamond; (b) Square; (c) Elliptical-horizontal; and (d) Elliptical-vertical cutouts
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