PG-EAM - Graduate Program in Aeronautical and Mechanical Engineering
PT EN
Article 2011

Finite element procedure for stress amplification factor recovering in a representative volume of composite materials

Authors

Plaisant, Paulo Cesar
Arakaki, Francisco Kioshi

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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