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    Thermomechanical Fatigue Crack Growth Modeling in a Ni Based Superalloy Subjected to Sustained Load

    Source: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 001::page 12503
    Author:
    Storgأ¤rds, Erik
    ,
    Simonsson, Kjell
    ,
    Sjأ¶strأ¶m, Sأ¶ren
    ,
    Moverare, Johan
    DOI: 10.1115/1.4031158
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Thermomechanical fatigue (TMF) crack growth modeling has been conducted on Inconel 718 with dwell time at maximum load. A history dependent damage model taking dwell damage into account, developed under isothermal conditions, has been extended for TMF conditions. Parameter determination for the model is carried out on isothermal load controlled tests at 550–650 آ°C for surface cracks, which later have been used to extrapolate parameters used for TMF crack growth. Further, validation of the developed model is conducted on a notched specimen subjected to strain control at 50–550 آ°C. Satisfying results are gained within reasonable scatter level compared for test and simulated number of cycles to failure.
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      Thermomechanical Fatigue Crack Growth Modeling in a Ni Based Superalloy Subjected to Sustained Load

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/160966
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorStorgأ¤rds, Erik
    contributor authorSimonsson, Kjell
    contributor authorSjأ¶strأ¶m, Sأ¶ren
    contributor authorMoverare, Johan
    date accessioned2017-05-09T01:27:58Z
    date available2017-05-09T01:27:58Z
    date issued2016
    identifier issn1528-8919
    identifier othergtp_138_01_012503.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/160966
    description abstractThermomechanical fatigue (TMF) crack growth modeling has been conducted on Inconel 718 with dwell time at maximum load. A history dependent damage model taking dwell damage into account, developed under isothermal conditions, has been extended for TMF conditions. Parameter determination for the model is carried out on isothermal load controlled tests at 550–650 آ°C for surface cracks, which later have been used to extrapolate parameters used for TMF crack growth. Further, validation of the developed model is conducted on a notched specimen subjected to strain control at 50–550 آ°C. Satisfying results are gained within reasonable scatter level compared for test and simulated number of cycles to failure.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleThermomechanical Fatigue Crack Growth Modeling in a Ni Based Superalloy Subjected to Sustained Load
    typeJournal Paper
    journal volume138
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4031158
    journal fristpage12503
    journal lastpage12503
    identifier eissn0742-4795
    treeJournal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 001
    contenttypeFulltext
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