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dc.contributor.authorShen, M.
dc.contributor.authorAkanda, Sajedur R.
dc.date.accessioned2017-05-09T01:18:33Z
dc.date.available2017-05-09T01:18:33Z
dc.date.issued2015
dc.identifier.issn0094-4289
dc.identifier.othermats_137_02_021008.pdf
dc.identifier.urihttp://yetl.yabesh.ir/yetl/handle/yetl/158135
dc.description.abstractA previously developed energy based high cycle fatigue (HCF) life assessment framework is modified to predict the low cycle fatigue (LCF) life of aluminum 6061T6. The fatigue life assessment model of this modified framework is formulated in a closed form expression by incorporating the Ramberg–Osgood constitutive relationship. The modified framework is composed of the following entities: (1) assessment of the average strain energy density and the average plastic strain range developed in aluminum 6061T6 during a fatigue test conducting at the ideal frequency for optimum energy calculation, and (2) determination of the Ramberg–Osgood cyclic parameters for aluminum 6061T6 from the average strain energy density and the average plastic strain range. By this framework, the applied stress range is related to the fatigue life by a power law whose parameters are functions of the fatigue toughness and the cyclic parameters. The predicted fatigue lives are found to be in a good agreement with the experimental data.
dc.publisherThe American Society of Mechanical Engineers (ASME)
dc.titleA Modified Closed Form Energy Based Framework for Fatigue Life Assessment for Aluminum 6061 T6—Damaging Energy Approach
dc.typeJournal Paper
dc.journal.volume137
dc.journal.issue2
dc.journal.titleJournal of Engineering Materials and Technology
dc.identifier.doi10.1115/1.4029532
dc.journal.fristpage21008
dc.journal.lastpage21008
dc.identifier.eissn1528-8889
dc.treeJournal of Engineering Materials and Technology:;2015:;volume( 137 ):;issue: 002
dc.contenttypeFulltext


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