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    Effect of KIII on Fatigue Crack Growth Behavior

    Source: Journal of Engineering Materials and Technology:;2012:;volume( 134 ):;issue: 004::page 41009
    Author:
    Masanori Kikuchi
    ,
    Yoshitaka Wada
    ,
    Chikako Ohdama
    DOI: 10.1115/1.4006978
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this study, mixed-mode fatigue tests are conducted using surface-cracked specimens. Slant surface-cracked specimens are prepared with crack angles of 15 deg, 30 deg, 45 deg, and 60 deg. It is shown that a “factory roof” fracture is formed at the deepest point of the surface crack due to ΔKIII and causes the crack growth rate to decrease. Additionally, fatigue crack growth is simulated using the superposition finite element method (FEM) with crack growth criteria. It is shown that conventional crack growth criteria are not applicable to factory roof fractures. Finally, a modified criterion for the prediction of crack growth rate is proposed, fatigue crack growth simulation is conducted using this criterion, and the results are compared with experimental results.
    keyword(s): Fracture (Materials) , Fatigue cracks , Finite element model , Roofs , Surface cracks , Stress , Fatigue testing , Shapes , Finite element methods AND Fracture (Process) ,
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      Effect of KIII on Fatigue Crack Growth Behavior

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/148961
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    contributor authorMasanori Kikuchi
    contributor authorYoshitaka Wada
    contributor authorChikako Ohdama
    date accessioned2017-05-09T00:50:44Z
    date available2017-05-09T00:50:44Z
    date copyrightOctober, 2012
    date issued2012
    identifier issn0094-4289
    identifier otherJEMTA8-926030#041009_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/148961
    description abstractIn this study, mixed-mode fatigue tests are conducted using surface-cracked specimens. Slant surface-cracked specimens are prepared with crack angles of 15 deg, 30 deg, 45 deg, and 60 deg. It is shown that a “factory roof” fracture is formed at the deepest point of the surface crack due to ΔKIII and causes the crack growth rate to decrease. Additionally, fatigue crack growth is simulated using the superposition finite element method (FEM) with crack growth criteria. It is shown that conventional crack growth criteria are not applicable to factory roof fractures. Finally, a modified criterion for the prediction of crack growth rate is proposed, fatigue crack growth simulation is conducted using this criterion, and the results are compared with experimental results.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffect of KIII on Fatigue Crack Growth Behavior
    typeJournal Paper
    journal volume134
    journal issue4
    journal titleJournal of Engineering Materials and Technology
    identifier doi10.1115/1.4006978
    journal fristpage41009
    identifier eissn1528-8889
    keywordsFracture (Materials)
    keywordsFatigue cracks
    keywordsFinite element model
    keywordsRoofs
    keywordsSurface cracks
    keywordsStress
    keywordsFatigue testing
    keywordsShapes
    keywordsFinite element methods AND Fracture (Process)
    treeJournal of Engineering Materials and Technology:;2012:;volume( 134 ):;issue: 004
    contenttypeFulltext
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