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Mechanical properties of interlaminer Kevlar29 and Al2O3 powder/epoxy composite plates using an analytical approach


Citation

Abu Talib, Abd. Rahim and Abbud, L. H. and Ali, Aidy and Mustapha, Faizal (2011) Mechanical properties of interlaminer Kevlar29 and Al2O3 powder/epoxy composite plates using an analytical approach. Scientific Research and Essays, 6 (21). pp. 4455-4463. ISSN 1992-2248

Abstract / Synopsis

In this study, the behaviour of laminated composite plates, fiber Kevlar29, Al2O3powder/epoxy and the suggested analytical solution for static analysis of composite plates were presented using general classical laminated plate theory. The Navier solutions are limited to simply support rectangular plates using static analysis. The results show that the effect of the deflections and stresses on the plate thickness–to–length ratio, aspect ratio, modulus ratio, fiber orientation and the number of layers were observed. The deflection and stresses on laminated composite plate decreases with the increase in the number of layers, fiber orientation, and thickness of the laminated plates. These results indicate that the improvements in mechanical properties for aircraft body applications were achieved.


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Additional Metadata

Item Type: Article
Divisions: Faculty of Engineering
Publisher: Academic Journals
Keywords: Composite materials; Laminated plates; Mechanical properties; Navier solution; Deflection plate
Depositing User: Nabilah Mustapa
Date Deposited: 07 Dec 2015 02:42
Last Modified: 07 Dec 2015 02:42
URI: http://psasir.upm.edu.my/id/eprint/23107
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