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The results show that our model cannot only be used for loading cases with small strains but also with large strains.
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It is reminded that these results are obtained only for loading case (b).
Interlaminar normal stress along the 90°/90° interface of [0°/0°/90°/90°] laminate for loading case (a) is displayed in Fig. 6.
Through the thickness distribution of the interlaminar normal stress σ z for [90°/90°/0°/0°] layup is displayed in Fig. 7 for loading case (a).
Figure 4 shows the numerical value of σ z at exactly y = b versus p value for both [0°/90°/0°/90°] and [0°/90°/90°/0°] laminates for loading case (a).
For these load cases, M1/M2 ratio was equal to −0.5 for load cases 1 and 2 (fix-ended) and zero for load cases 3 and 4 (pin-ended).
However, in almost all cases, lower one-percentile strength ratios were produced for load cases 5 6 than for load cases 1 4.
The same conclusion can be drawn by comparing Fig. 10d for load cases 5 6 with Fig. 10b for load cases 1 4.
These conclusions also appear valid when Fig. 10c, d plotted for load cases 5 6 are compared.
More compact statistics and tighter histograms were produced for load cases 5 6 ploted in Fig. 10c as opposed to those produced for load cases 1 4 and shown in Fig. 10a.
For an isotropic plate the degree of localization is found to increase with the increase in the aspect ratio for load cases (i)–(iii) but is found to be moderate for load cases (iv) and (v).
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