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In this paper, the classical solution of the opening mode crack in the 90° layer of 0/90/0 laminates has been determined by
means of Fourier transformations and the procedure of Copson for a pair of dual integral equations. The fracture behavior
and the in situ transverse strength of the 90° layer have been quantitatively studied in graphite/epoxy laminates, based on
the solution obtained above.
The results show that the stress intensity factor of this kind of laminates, which is different from that of a single unidirectional
90° layer, decreases with the increase in thicknessb, or modulusE
L orG
LT of the 0° layer and also decreases with the decrease in the thickness of the 90° layer. So the lamination effect manifests
itself and thein situ transverse strength of the 90° layer is thereby enchanced. The theoretical calculations agree with the experimental data
presented by D.L. Flaggs.
Supported by National Natural Science Fundation of China. 相似文献