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contributor authorA. R. Khamseh
contributor authorA. M. Waas
date accessioned2017-05-08T23:53:40Z
date available2017-05-08T23:53:40Z
date copyrightJanuary, 1997
date issued1997
identifier issn0094-4289
identifier otherJEMTA8-26982#56_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/118816
description abstractWe report the results of an experimental investigation carried out for the analysis of failure mechanisms in fibrous laminated composite plates containing stress raisers, in the form of circular cutouts, under static biaxial planar compressive loading (i.e., compression in the two inplane orthogonal directions). A series of biaxial tests were carried out with 48 ply graphite/epoxy composites of varying fiber orientation. In all cases, the hole diameter to plate width aspect ratio remained in a range suitable for infinite plate assumptions. Fiber microbuckling, fiber kink banding, and fiber/matrix debonding are identified as the dominant failure mechanisms.
publisherThe American Society of Mechanical Engineers (ASME)
titleFailure Mechanisms of Composite Plates With a Circular Hole Under Remote Biaxial Planar Compressive Loads
typeJournal Paper
journal volume119
journal issue1
journal titleJournal of Engineering Materials and Technology
identifier doi10.1115/1.2805974
journal fristpage56
journal lastpage64
identifier eissn1528-8889
keywordsComposite materials
keywordsStress
keywordsFailure mechanisms
keywordsPlates (structures)
keywordsFibers
keywordsEpoxy adhesives
keywordsCompression
keywordsFailure analysis
keywordsGraphite AND Mechanisms
treeJournal of Engineering Materials and Technology:;1997:;volume( 119 ):;issue: 001
contenttypeFulltext


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