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contributor authorAssimina A. Pelegri
date accessioned2017-05-08T23:59:44Z
date available2017-05-08T23:59:44Z
date copyrightOctober, 1999
date issued1999
identifier issn0094-4289
identifier otherJEMTA8-27002#430_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/122199
description abstractAn investigation into the growth behavior of interlayer and intralayer cracks in delaminated cross-ply laminates subjected to fatigue compression is presented. Experimental data indicate different fatigue growth patterns for the two cases. The effects of mode mixity and position of the delamination in the formation of the cracks are studied. A mode-dependent fatigue growth law is applied in order to predict the behavior of the intralayer and interlayer cracks. Successful correlation of the analytical and test data is conducted for the interlayer cracks. For the intralayer cracks, addition of contact effects and local geometrical parameters in the model are suggested.
publisherThe American Society of Mechanical Engineers (ASME)
titleEvolution of Interlayer and Intralayer Cracks Under Compressive Fatigue in Composites
typeJournal Paper
journal volume121
journal issue4
journal titleJournal of Engineering Materials and Technology
identifier doi10.1115/1.2812398
journal fristpage430
journal lastpage435
identifier eissn1528-8889
keywordsFatigue
keywordsComposite materials
keywordsFracture (Materials)
keywordsCompression
keywordsDelamination AND Laminates
treeJournal of Engineering Materials and Technology:;1999:;volume( 121 ):;issue: 004
contenttypeFulltext


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