Journal of Aerospace Technology and Management (Jan 2012)

FINITE ELEMENT PROCEDURE FOR STRESS AMPLIFICATION FACTOR RECOVERING IN A REPRESENTATIVE VOLUME OF COMPOSITES MATERIALS. DOI: 10.5028/jatm.2011.03033911

  • Paulo Cesar Plaisant Junior,
  • Flávio Luiz de Paula Bussamra,
  • Francisco Kioshi Araki

Journal volume & issue
Vol. 3, no. 3

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.

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