Effects Of Edge Distance, Hole Size Ratio And Hole Spacing On Peak Stresses Of Composite Laminate With Multiple Holes

dc.contributorKheradiya, Manishkumaren_US
dc.date.accessioned2009-09-16T18:20:02Z
dc.date.accessioned2011-08-24T21:42:45Z
dc.date.available2009-09-16T18:20:02Z
dc.date.available2011-08-24T21:42:45Z
dc.date.issued2009-09-16T18:20:02Z
dc.date.submittedJanuary 2008en_US
dc.description.abstractUnlike isotropic material, the stress distribution of laminate with a hole varies with its size, its material properties and fiber orientations of each layer. Moreover, presence of a hole in the neighborhood of another hole may also affect their stress distribution, too. The major objective of this study is to determine stress distribution of finite width laminated composite having multiple holes. The effect of stress concentration due to presence of holes in each angle ply of laminated composite is a focus of this study. Three dimensional finite element models are developed to determine the stress distribution in laminate using commercial software package ANSYS 10.0 classic. The material used for laminated composite is T300/977-2 grphite/epoxy with [03/±45/90]s laminate layup. The stress distribution of composite laminate with single, two and three holes is investigated. The effect of proximity of single hole to laminate edge is also discussed. The stress concentration for "two holes oriented in-line with load" and "two holes oriented side by side transverse to load" are discussed. The effects of "hole size ratio" and "edge distance between two holes" on stress distribution are also investigated. The patterns of three holes placed at three vertices of a triangle with different edge distance between holes are also been included in this study. The maximum stress concentration found at the point on hole periphery where fibers are tangent to the hole. The patterns of the hole orientation and holes size ratio as well as the edge distance between holes play important role on the magnitude of stress concentration of composite laminates.en_US
dc.identifier.urihttp://hdl.handle.net/10106/1812
dc.language.isoENen_US
dc.publisherMechanical Engineeringen_US
dc.titleEffects Of Edge Distance, Hole Size Ratio And Hole Spacing On Peak Stresses Of Composite Laminate With Multiple Holesen_US
dc.typeM.S.en_US

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