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    Some Recent Advances in Engineering Fracture Modeling for Turbomachinery

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 002::page 21005
    Author:
    Craig McClung, R.
    ,
    Lee, Yi-Der
    ,
    Sobotka, James C.
    ,
    Moody, Jonathan P.
    ,
    Bhamidipati, Vikram
    ,
    Enright, Michael P.
    ,
    Benjamin Guseman, D.
    ,
    Thomas, Colin B.
    DOI: 10.1115/1.4040901
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Recent advances in practical engineering methods for fracture analysis of turbomachinery components are described. A comprehensive set of weight function (WF) stress intensity factor (SIF) solutions for elliptical and straight cracks under univariant and bivariant stress gradients has been developed and verified. Specialized SIF solutions have been derived for curved through cracks, cracks at chamfered and angled corners, and cracks under displacement control. Automated fracture models are available to construct fatigue crack growth (FCG) life contours and critical initial crack size (CICS) contours for all nodal locations in two-dimensional or three-dimensional (2D or 3D) finite element (FE) models.
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      Some Recent Advances in Engineering Fracture Modeling for Turbomachinery

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    https://yetl.yabesh.ir/yetl1/handle/yetl/4255553
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    contributor authorCraig McClung, R.
    contributor authorLee, Yi-Der
    contributor authorSobotka, James C.
    contributor authorMoody, Jonathan P.
    contributor authorBhamidipati, Vikram
    contributor authorEnright, Michael P.
    contributor authorBenjamin Guseman, D.
    contributor authorThomas, Colin B.
    date accessioned2019-03-17T09:34:19Z
    date available2019-03-17T09:34:19Z
    date copyright9/19/2018 12:00:00 AM
    date issued2019
    identifier issn0742-4795
    identifier othergtp_141_02_021005.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4255553
    description abstractRecent advances in practical engineering methods for fracture analysis of turbomachinery components are described. A comprehensive set of weight function (WF) stress intensity factor (SIF) solutions for elliptical and straight cracks under univariant and bivariant stress gradients has been developed and verified. Specialized SIF solutions have been derived for curved through cracks, cracks at chamfered and angled corners, and cracks under displacement control. Automated fracture models are available to construct fatigue crack growth (FCG) life contours and critical initial crack size (CICS) contours for all nodal locations in two-dimensional or three-dimensional (2D or 3D) finite element (FE) models.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleSome Recent Advances in Engineering Fracture Modeling for Turbomachinery
    typeJournal Paper
    journal volume141
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.4040901
    journal fristpage21005
    journal lastpage021005-9
    treeJournal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 002
    contenttypeFulltext
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