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    Temperature and Load Ratio Effects on Crack-Growth Behavior of Austenitic Superalloys

    Source: Journal of Engineering Materials and Technology:;2010:;volume( 132 ):;issue: 001::page 11001
    Author:
    Ajit K. Roy
    ,
    Joydeep Pal
    ,
    Muhammad H. Hasan
    DOI: 10.1115/1.3184027
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The role of temperature and load ratio (R) on the crack propagation rate (da/dN) of Alloys 276 and 617 under cyclic loading was investigated. The results indicate that the rate of cracking was gradually enhanced with increasing temperature when the R value was kept constant. However, the temperature effect was more pronounced at 100–150°C. Both alloys exhibited maximum da/dN values at a load range of 4.5 kN that corresponds to an R value of 0.1. The number of cycles to failure for Alloy 276 was relatively higher compared with that of Alloy 617, indicating its slower crack-growth rate. Fractographic evaluation of the broken specimen surface revealed combined fatigue and ductile failures.
    keyword(s): Temperature , Alloys , Stress , Fracture (Materials) , Superalloys , Crack propagation AND Testing ,
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      Temperature and Load Ratio Effects on Crack-Growth Behavior of Austenitic Superalloys

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/143364
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    contributor authorAjit K. Roy
    contributor authorJoydeep Pal
    contributor authorMuhammad H. Hasan
    date accessioned2017-05-09T00:37:59Z
    date available2017-05-09T00:37:59Z
    date copyrightJanuary, 2010
    date issued2010
    identifier issn0094-4289
    identifier otherJEMTA8-27124#011001_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/143364
    description abstractThe role of temperature and load ratio (R) on the crack propagation rate (da/dN) of Alloys 276 and 617 under cyclic loading was investigated. The results indicate that the rate of cracking was gradually enhanced with increasing temperature when the R value was kept constant. However, the temperature effect was more pronounced at 100–150°C. Both alloys exhibited maximum da/dN values at a load range of 4.5 kN that corresponds to an R value of 0.1. The number of cycles to failure for Alloy 276 was relatively higher compared with that of Alloy 617, indicating its slower crack-growth rate. Fractographic evaluation of the broken specimen surface revealed combined fatigue and ductile failures.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleTemperature and Load Ratio Effects on Crack-Growth Behavior of Austenitic Superalloys
    typeJournal Paper
    journal volume132
    journal issue1
    journal titleJournal of Engineering Materials and Technology
    identifier doi10.1115/1.3184027
    journal fristpage11001
    identifier eissn1528-8889
    keywordsTemperature
    keywordsAlloys
    keywordsStress
    keywordsFracture (Materials)
    keywordsSuperalloys
    keywordsCrack propagation AND Testing
    treeJournal of Engineering Materials and Technology:;2010:;volume( 132 ):;issue: 001
    contenttypeFulltext
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