Buckling and vibration analyses of composite laminates with weak interfaces by a coupled meshfree and finite element method
Source abstract
Abstract
Abstract Buckling and free vibration analyses for composite laminates with weak interfaces were performed based on a three-dimensional hybrid semianalytical model. The model was established by coupling the radial point interpolation method and finite element method (FEM) in a Hamilton system. A direct coupling approach was developed based on the FEM background cell algorithm, and a modified Hamiltonian function for buckling analysis of rectangular laminated plates was given. The governing equations were deduced with the transfer matrix technique and a general linear spring layer model based on the modified Hellinger-Reissner variational principle. Several numerical examples are also presented to validate the efficiency and accuracy of the present method.
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Research context
OpenAlex topics: Composite Structure Analysis and Optimization · Numerical methods in engineering · Structural Load-Bearing Analysis
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
School of Aeronautics and Astronautics, Shanghai Jiao Tong University, 200240 Shanghai, China
Shanghai Aircraft Design and Research Institute, 201210 Shanghai, China
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