PG-EAM - Programa de Pós-Graduação em Engenharia Aeronáutica e Mecânica
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Dissertação de Mestrado 2020

Three dimensional hybrid-mixed finite elements for analysis of laminated composite plates

Autor

Fernando Carlos Magalhães Carneiro da Silva

Orientador

Área de Concentração

Projeto Aeronáutico, Estruturas e Sistemas Aeroespaciais

Data de Defesa

16/12/2020

Número da Tese

77689

Resumo

In this thesis, three-dimensional hybrid-mixed stress elements are used for structural analysis of laminates. In the formulation of the hybrid-mixed finite elements, stress and displacement fields are simultaneously and independently approximated in the domain as well as the displacement on the boundary. Legendre polynomials are used as approximation functions. These approximations are free of any constraint a priori. The orthotropic material has been considered in the element implementation and numerical results for some selected problems have been compared with those from conventional compatibility finite element method. The numerical tests have showed good convergence of results both for displacement and stress. Results for stress converged faster than those for displacement, i.e., convergence has been observed for the lowest levels of refinement. In general, results for p-refinement were better than those for h-refinement.

Palavras-chave

Método de elementos finitos Laminados Placas Funções de Legendre Engenharia de materiais