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contributor authorHyoungseock Seo
contributor authorH. T. Hahn
contributor authorJenn-Ming Yang
date accessioned2017-05-09T00:28:09Z
date available2017-05-09T00:28:09Z
date copyrightOctober, 2008
date issued2008
identifier issn0094-4289
identifier otherJEMTA8-27111#041002_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/138049
description abstractThe fatigue behavior and residual strength of postimpacted GLARE 4-3/2, GLARE 5-2/1, and monolithic aluminum 2024-T3 alloy were investigated experimentally. Drop-weight impact was applied at a variety of energy levels to inflict a barely visible impact damage, a clearly visible impact damage, and a penetration damage. After the impact test, constant-amplitude tension-tension fatigue was done to delineate the modes of damage initiation and growth and the effect of damage on fatigue life and residual strength. The results showed that GLARE laminates exhibit superior postimpact fatigue durability when compared with the monolithic 2024-T3 aluminum alloy.
publisherThe American Society of Mechanical Engineers (ASME)
titleImpact Damage Tolerance and Fatigue Durability of GLARE Laminates
typeJournal Paper
journal volume130
journal issue4
journal titleJournal of Engineering Materials and Technology
identifier doi10.1115/1.2969253
journal fristpage41002
identifier eissn1528-8889
keywordsFatigue
keywordsAluminum
keywordsLaminates
keywordsDurability
keywordsFracture (Materials)
keywordsStress
keywordsFatigue testing AND Impact testing
treeJournal of Engineering Materials and Technology:;2008:;volume( 130 ):;issue: 004
contenttypeFulltext


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