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    Identification and Validation of a Low Cycle Fatigue Damage Model for Al 7075 T6 Alloy

    Source: Journal of Engineering Materials and Technology:;2015:;volume( 137 ):;issue: 001::page 11004
    Author:
    Masih, Saeed
    ,
    Mashayekhi, Mohammad
    ,
    Torabian, Noushin
    DOI: 10.1115/1.4028840
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In 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.
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      Identification and Validation of a Low Cycle Fatigue Damage Model for Al 7075 T6 Alloy

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    https://yetl.yabesh.ir/yetl1/handle/yetl/158121
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    • Journal of Engineering Materials and Technology

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    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
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