Impact Properties of Parts Manufactured from Fiberglass and Kevlar Composite Panels

Emilian Ionut Croitoru; Gheorghe Oancea

doi:10.4028/www.scientific.net/AMM.809-810.938

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 809-810Impact Properties of Parts Manufactured from...

Impact Properties of Parts Manufactured from Fiberglass and Kevlar Composite Panels

Abstract:

This paper presents a method of finite element modelling used to study the effect of laminates orientation and thickness on impact properties of a composite sandwich panel made of glass and kevlar fibers in an epoxy resin matrix. In this research, the composite sandwich panel consists of a fuselage skin panel from an aircraft having two configurations: (0/90/0/90/core/90/0/90/0) and (0/90/45/-45/core/-45/45/90/0). This panel is loaded with one uniform distributed abuse loading case and the stress variation within the composite panel for each configuration is determined.

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Periodical:

Applied Mechanics and Materials (Volumes 809-810)

Pages:

938-943

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.809-810.938

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Online since:

November 2015

Authors:

Emilian Ionut Croitoru*, Gheorghe Oancea

Keywords:

Composite Panels, Fiberglass, Fibers, Finite Element Analysis, Finite Element Modelling, Kevlar, Resin Matrix

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