Article
2011
Finite element procedure for stress amplification factor recovering in a representative volume of composite materials
Authors
Journal of Aerospace Technology and Management , vol. 3 , no. 3 , pp. 239-250
ISSN: 19849648
8
Citations
3
Authors
Abstract
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.
Keywords
Composites
Finite element analysis
Micromechanics
Microstress distribution
Stress amplification factor
Aerospace Engineering
(ENGI)
Engineering (all)
(ENGI)
: Scopus
Last Update: 2026-06-25
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