For composite laminates,how to accurately analyze the interlayer stress(especially the transverse shear stress)is of great significance in practical engineering applications.The research purpose of this paper is to propose a relatively simple and accurate finite element numerical method that can accurately analyze the transverse stresses between composite layers.The main work is as follows:Combining layerwise theory and symplectic finite element theory,based on the principle of minimum potential energy and the modified H-R variational principle,a multilayer symplectic formula is established.The main characteristics of multi-layer symplectic include: the diagonal of the element's coefficient matrix has no zero elements,so the corresponding finite element linear system equations have stable solutions;because the multilayer symplectic contains out-of-plane stress variables,it meets the layer The continuous requirements of transverse shear stress and normal stress;support for the introduction of stress boundary conditions of the structure.At the same time,there is no need to apply special post-processing techniques to calculate the out-of-plane stress results.Based on the multi-layer symplectic finite element model,several examples are analyzed.The numerical results are compared with the exact or analytical solutions.The results show that: on the boundary,the accuracy of multi-layer symplectic stress results is better than non-coordinated displacement elements;the finite element model can significantly improve the accuracy of numerical results after introducing out-of-plane stress boundary conditions;The transverse stress analysis results of common composite laminates show that the results of multi-layer symplectic elements are more accurate than those of noncoordinated displacement elements and hybrid stress elements.For different boundary conditions,multi-layer symplectic elements can give ideal stress results.The establishment of multi-layer symplectic element proposed an effective new method for stress analysis of composite laminates. |