文章基本信息

标题：Effects of Ply Orientation on Nonlinear Buckling of Aircraft Stiffened Composite Panel
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作者：Ouadia Mouhat ; Abdellatif Khamlichi ; Hasnae Boubel 等
期刊名称：Research Journal of Applied Sciences
印刷版ISSN：1815-932X
电子版ISSN：1993-6079
出版年度：2020
卷号：15
期号：4
页码：139-149
DOI：10.36478/rjasci.2020.139.149
语种：English
出版社：Medwell Journals
摘要：In this study, gradual demand for curved,stiffened panels composite emerged from Carbon FiberReinforced Plastics (CFRP) these are structures that arefrequently used in aerospace engineering. Up to 50% ofthe primary structure of the Boeing 787 is made up ofwoven graphite-epoxy. This research emphasizes thebuckling analysis of stiffened composite panels using thenonlinear, finite element modeling. The stiffened panel isassumed to be subjected to a uniform axial compressionload of 10 kN. For the nonlinear buckling analysis, astiffened composite panel is made of Carbon FibreComposite (CFC) in epoxy, Kevlar in epoxy and E-Glass(EG) in epoxy. Due to the fact that there are numerousstiffened composite panels materials this study, thereforeuses a numerical approach to present the study and resultsof the nonlinear static buckling analysis of i-stiffened ondifferent composite panels. This research also presentedthe effect of the different ply orientations using AbaqusFinite Element Analysis (FEA).
关键词：Stiffened composite panels;nonlinear buckling analysis;ply orientations;FEM;CFC;FEA