This paper deals with the numerical modeling of delaminated composite plates by applying the differential quadrature method. A semi-layerwise modeling technique developed by the author including the first-, second- and third-order shear deformation plate theories is utilized. The proposed model captures separately the delaminated and the intact parts of the plates with straight delamination front. Firstly, the governing differential equations are presented and then it is shown how these were discretized by using a recommended grid structure and the required boundary and continuity conditions. Some plate problems with simply supported and rigidly fixed edges are solved including some variations of the size and the thicknesswise position of the material defect. One of the non-trivial aspects of the differential quadrature solution is how the continuity between the different regions can be imposed. It will be shown that at the mutual grid points of the neighboring regions it is not possible to satisfy each continuity condition against the stress resultants, and thus although some conditions are violated, the problems can be solved accurately by properly choosing the actual conditions. Once, the differential quadrature solution became available the mechanical fields were determined, too. Moreover, the J-integral can be determined and together with a simple mode separation technique even the mode-II and mode-III components became available. The comparison of results to those by spatial finite element models shows very good accuracy and the effectiveness of the proposed differential quadrature solution.
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