Show simple item record

contributor authorMasih, Saeed
contributor authorMashayekhi, Mohammad
contributor authorTorabian, Noushin
date accessioned2017-05-09T01:18:30Z
date available2017-05-09T01:18:30Z
date issued2015
identifier issn0094-4289
identifier othermats_137_01_011004.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/158121
description abstractIn this paper, the behavior of 7075T6 aluminum alloy under low cycle fatigue (LCF) loading is experimentally and numerically investigated using continuum damage mechanics (CDM). An experimental procedure is established to identify the damage parameters for Al 7075T6. A damagecoupled explicit finite element code is developed using the experimentally extracted damage parameters to study the material behavior under LCF loading. Moreover, fractographic examinations are conducted to identify the fatigue crack initiation locations and propagation mechanisms. The model is employed for lifetime assessment of stringerskin connection of a fuselage and the results are compared with the data available in the literature.
publisherThe American Society of Mechanical Engineers (ASME)
titleIdentification and Validation of a Low Cycle Fatigue Damage Model for Al 7075 T6 Alloy
typeJournal Paper
journal volume137
journal issue1
journal titleJournal of Engineering Materials and Technology
identifier doi10.1115/1.4028840
journal fristpage11004
journal lastpage11004
identifier eissn1528-8889
treeJournal of Engineering Materials and Technology:;2015:;volume( 137 ):;issue: 001
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record