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contributor authorH. Saghizadeh
contributor authorC. K. H. Dharan
date accessioned2017-05-08T23:22:35Z
date available2017-05-08T23:22:35Z
date copyrightOctober, 1986
date issued1986
identifier issn0094-4289
identifier otherJEMTA8-26912#290_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/101196
description abstractThe delamination fracture toughness of graphite and aramid-epoxy composite laminates was determined as a function of loading rate for unidirectional and woven reinforcements. In addition, the in-situ fracture toughness of the epoxy matrix was obtained by determining the crack energy release rate during the delamination fracture of thin epoxy films. The fracture surfaces were investigated using scanning electron microscopy. The results show that increasing the loading rate and the use of woven reinforcements increase the fracture toughness. A model was used to estimate the relative contributions from the fiber-matrix interface and the matrix to the overall delamination crack energy release rate.
publisherThe American Society of Mechanical Engineers (ASME)
titleDelamination Fracture Toughness of Graphite and Aramid Epoxy Composites
typeJournal Paper
journal volume108
journal issue4
journal titleJournal of Engineering Materials and Technology
identifier doi10.1115/1.3225885
journal fristpage290
journal lastpage295
identifier eissn1528-8889
keywordsComposite materials
keywordsEpoxy adhesives
keywordsFracture toughness
keywordsGraphite
keywordsDelamination
keywordsFracture (Process)
keywordsScanning electron microscopy
keywordsFibers AND Laminates
treeJournal of Engineering Materials and Technology:;1986:;volume( 108 ):;issue: 004
contenttypeFulltext


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