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Influence of micromechanics in composite panels buckling loads


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Opened Access Influence of micromechanics in composite panels buckling loads
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Author: Martín, Alberto
Ibiza Granados, Carlos
Rodríguez de Tembleque Solano, Luis
Department: Universidad de Sevilla. Departamento de Mecánica de Medios Continuos y Teoría de Estructuras
Date: 2015
Published in: 3rd International Conference on Mechanical Models in Structural Engineering, 267-280. Sevilla, España : CMMoST 2015
ISBN/ISSN: 978-84-606-9356-7
Document type: Presentation
Abstract: In-plane compression loads may cause buckling of fiber-reinforced composite panels. An accurate knowledge of these critical buckling loads is essential for structural design. In all cases of buckling of panels, critical loads increases with the increase in the thickness of the panel, however, more economical solutions can be obtained by keeping the thickness of the plate as small as possible and increasing the stability by considering micromechanical aspect such as: fiber orientation relative to axial direction, fiber aspect ratio or fiber volume fraction. This paper presents some parametric studies to study the influence of micromechanics in the critical buckling load of fiber-reinforced plates and curved panels.
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