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- W337389555 abstract "Abstract : The structural stiffness properties of composite laminated plates are experimental information needed in order to design aircraft components manufactured with composite materials. A common test used to obtain the necessary moduli is to apply a tension load on the ends of the specimen. Little study, if any, has been reported relating the application of the Saint Venant's principle within a multi-ply laminated plate. Previously, researchers have shown that routine application of Saint Venant's principle in problems involving a single composite lamina is not generally justified. This study offers justification for using Saint Venant's principle in commonly laid-up graphite epoxy plate specimens. The boundary conditions considered are attempts at modeling varying end supports for an in-plane loading. The analysis has been carried out using a finite element model considering three aspect ratios: 3, 5, and 10. (Author)" @default.
- W337389555 created "2016-06-24" @default.
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- W337389555 date "1978-12-01" @default.
- W337389555 modified "2023-09-27" @default.
- W337389555 title "Investigation of Saint Venant's Principle as Related to Laminated Composite Plates." @default.
- W337389555 hasPublicationYear "1978" @default.
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