Finite element procedure for stress amplification factor recovering in a representative volume of composite materials
Finite element models are proposed to the micromechanical analysis of a representative volume of composite materials. A detailed description of the meshes, boundary conditions, and loadings are presented. An illustrative application is given to evaluate stress amplification factors within a represen...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
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Departamento de Ciência e Tecnologia Aeroespacial
2011-09-01
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| Series: | Journal of Aerospace Technology and Management |
| Subjects: | |
| Online Access: | http://www.jatm.com.br/papers/vol3_n3/JATMv3n3_p239-250_Finite_element_procedure_for_stress_amplification_factor_recovering_in_a_representative_volume_of_composite_materials.pdf |
| Summary: | Finite element models are proposed to the micromechanical analysis of a representative volume of composite materials. A detailed description of the meshes, boundary conditions, and loadings are presented. An illustrative application is given to evaluate stress amplification factors within a representative volume of the unidirectional carbon fiber composite plate. The results are discussed and compared to the numerical findings. |
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| ISSN: | 1984-9648 2175-9146 |