作者: S. Zheng , C.T. Sun
DOI: 10.1016/S0013-7944(97)00120-3
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摘要: Abstract A triple plate finite element model was proposed to analyze delamination interaction in laminated structures. This verified by comparison with an axisymmetric solution on a double delaminated structure. With this model, the results of three-point bending composite laminate and circular were obtained. In case laminate, both crack induced shear crack-induced delaminations will grow at same time eventually, while plate, vertical distance between these two has significant effect their interaction. Depending distance, one may have shielding other, other negligible former.