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    Fatigue Behavior of a 22Cr-20Ni-18Co-Fe Alloy at Elevated Temperatures

    Source: Journal of Engineering Materials and Technology:;1994:;volume( 116 ):;issue: 001::page 54
    Author:
    T. H. Krukemyer
    ,
    R. W. Swindeman
    ,
    A. Fatemi
    DOI: 10.1115/1.2904255
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental investigation was conducted on Haynes Alloy 556 to study the fatigue behavior of the material at elevated temperatures. Fatigue tests were run at constant temperatures ranging from room temperature to 871°C with strain ranges from 0.265 to 1.5 percent resulting in lives between 102 and 106 cycles. Cyclic deformation properties were evaluated based on the fatigue data. Three fatigue life models were evaluated for their ability to predict the isothermal fatigue lives of the material. These included the Ostergren, Frequency Separation and Stress-Strain-Time models. Strengths and weaknesses of each model are discussed based on the experimental results.
    keyword(s): Alloys , Fatigue , Temperature , Separation (Technology) , Deformation , Stress , Cycles , Fatigue life AND Fatigue testing ,
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      Fatigue Behavior of a 22Cr-20Ni-18Co-Fe Alloy at Elevated Temperatures

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/113725
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    • Journal of Engineering Materials and Technology

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    contributor authorT. H. Krukemyer
    contributor authorR. W. Swindeman
    contributor authorA. Fatemi
    date accessioned2017-05-08T23:44:28Z
    date available2017-05-08T23:44:28Z
    date copyrightJanuary, 1994
    date issued1994
    identifier issn0094-4289
    identifier otherJEMTA8-26961#54_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/113725
    description abstractAn experimental investigation was conducted on Haynes Alloy 556 to study the fatigue behavior of the material at elevated temperatures. Fatigue tests were run at constant temperatures ranging from room temperature to 871°C with strain ranges from 0.265 to 1.5 percent resulting in lives between 102 and 106 cycles. Cyclic deformation properties were evaluated based on the fatigue data. Three fatigue life models were evaluated for their ability to predict the isothermal fatigue lives of the material. These included the Ostergren, Frequency Separation and Stress-Strain-Time models. Strengths and weaknesses of each model are discussed based on the experimental results.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFatigue Behavior of a 22Cr-20Ni-18Co-Fe Alloy at Elevated Temperatures
    typeJournal Paper
    journal volume116
    journal issue1
    journal titleJournal of Engineering Materials and Technology
    identifier doi10.1115/1.2904255
    journal fristpage54
    journal lastpage61
    identifier eissn1528-8889
    keywordsAlloys
    keywordsFatigue
    keywordsTemperature
    keywordsSeparation (Technology)
    keywordsDeformation
    keywordsStress
    keywordsCycles
    keywordsFatigue life AND Fatigue testing
    treeJournal of Engineering Materials and Technology:;1994:;volume( 116 ):;issue: 001
    contenttypeFulltext
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