Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
754124 | Acta Mechanica Solida Sinica | 2008 | 14 Pages |
Abstract
ABSTRACTA constitutive model for composite laminated plates with the damage effect of the intra-layers and inter-laminar interface is presented. The model is based on the general six-degreesof-freedom plate theory, the discontinuity of displacement on the interfaces are depicted by three shape functions, which are formulated according to solutions satisfying three equilibrium equations. By using the variation principle, the three-dimensional non-linear equilibrium differential equations of the laminated plates with two different damage models are derived. Then, considering a simply supported laminated plate with damage, an analytical solution is presented using finite difference method to obtain the inter-laminar stresses.
Related Topics
Physical Sciences and Engineering
Engineering
Mechanical Engineering