Journal of Aerospace Technology and Management (Sep 2011)

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

  • Paulo Cesar Plaisant Junior,
  • Flávio Luiz de Silva Bussamra,
  • Francisco Kioshi Arakaki

Journal volume & issue
Vol. 3, no. 3
pp. 239 – 250

Abstract

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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