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    On the Changing Order of Singularity at a Crack Tip

    Source: Journal of Applied Mechanics:;1977:;volume( 044 ):;issue: 004::page 625
    Author:
    R. J. Nuismer
    ,
    G. P. Sendeckyj
    DOI: 10.1115/1.3424147
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The nature of the transition in the crack tip stress singularity from an inverse square root to an inverse fractional power as a crack tip reaches a phase boundary or a geometrical discontinuity for interface cracks is examined. This is done by analyzing the simple closed-form solution to the problem of a rigid line inclusion with one side partially debonded for the case of antiplane deformation. For this example, the crack tip stress singularity changes from an inverse square root to an inverse three-quarters power as the crack tips approach the inclusion tips (i.e., when one face of the rigid line inclusion is completely debonded). A detailed analysis, based on series expansions of the closed-form solution, is used to show how the singularity transition occurs. Moreover, the expansions indicate difficulties that may be encountered when solving such problems by approximate methods.
    keyword(s): Fracture (Materials) , Stress singularity AND Deformation ,
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      On the Changing Order of Singularity at a Crack Tip

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    https://yetl.yabesh.ir/yetl1/handle/yetl/89428
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    contributor authorR. J. Nuismer
    contributor authorG. P. Sendeckyj
    date accessioned2017-05-08T23:02:06Z
    date available2017-05-08T23:02:06Z
    date copyrightDecember, 1977
    date issued1977
    identifier issn0021-8936
    identifier otherJAMCAV-26081#625_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/89428
    description abstractThe nature of the transition in the crack tip stress singularity from an inverse square root to an inverse fractional power as a crack tip reaches a phase boundary or a geometrical discontinuity for interface cracks is examined. This is done by analyzing the simple closed-form solution to the problem of a rigid line inclusion with one side partially debonded for the case of antiplane deformation. For this example, the crack tip stress singularity changes from an inverse square root to an inverse three-quarters power as the crack tips approach the inclusion tips (i.e., when one face of the rigid line inclusion is completely debonded). A detailed analysis, based on series expansions of the closed-form solution, is used to show how the singularity transition occurs. Moreover, the expansions indicate difficulties that may be encountered when solving such problems by approximate methods.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOn the Changing Order of Singularity at a Crack Tip
    typeJournal Paper
    journal volume44
    journal issue4
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3424147
    journal fristpage625
    journal lastpage630
    identifier eissn1528-9036
    keywordsFracture (Materials)
    keywordsStress singularity AND Deformation
    treeJournal of Applied Mechanics:;1977:;volume( 044 ):;issue: 004
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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