Ponencia
Influence of micromechanics in composite panels buckling loads
Autor/es | Martín, Alberto
Ibiza Granados, Carlos Rodríguez de Tembleque Solano, Luis |
Departamento | Universidad de Sevilla. Departamento de Mecánica de Medios Continuos y Teoría de Estructuras |
Fecha de publicación | 2015 |
Fecha de depósito | 2016-02-19 |
Publicado en |
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ISBN/ISSN | 978-84-606-9356-7 |
Resumen | 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 ... 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. |
Ficheros | Tamaño | Formato | Ver | Descripción |
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CMMoST 2015_Martin_Influence.pdf | 1.782Mb | [PDF] | Ver/ | |