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    Life Prediction for Complex Structures

    Source: Journal of Engineering for Gas Turbines and Power:;2005:;volume( 127 ):;issue: 004::page 814
    Author:
    S. C. Forth
    ,
    B. S. Annigeri
    ,
    W. D. Keat
    DOI: 10.1115/1.1448330
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The surface integral method, an indirect boundary element method that represents a crack as a distribution of force dipoles, has been developed to model three-dimensional nonplanar crack growth in complex structures. The finite body was effectively modeled by superposition of stress influence functions for a half-space. As a result of this strategy, only the fracture has to be discretized. Crack propagation was modeled using the maximum circumferential stress theory to predict crack direction and the Forman fatigue equation, modified with an equivalent stress intensity solution for mixed-mode, to predict extension. Comparisons with benchmark solutions and field data verified the computational methodology and defined the limits of its applicability.
    keyword(s): Stress , Fracture (Materials) , Fracture (Process) , Equations , Spectra (Spectroscopy) , Fatigue , Elastic half space , Functions AND Force ,
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      Life Prediction for Complex Structures

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/131738
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorS. C. Forth
    contributor authorB. S. Annigeri
    contributor authorW. D. Keat
    date accessioned2017-05-09T00:16:02Z
    date available2017-05-09T00:16:02Z
    date copyrightOctober, 2005
    date issued2005
    identifier issn1528-8919
    identifier otherJETPEZ-26882#814_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/131738
    description abstractThe surface integral method, an indirect boundary element method that represents a crack as a distribution of force dipoles, has been developed to model three-dimensional nonplanar crack growth in complex structures. The finite body was effectively modeled by superposition of stress influence functions for a half-space. As a result of this strategy, only the fracture has to be discretized. Crack propagation was modeled using the maximum circumferential stress theory to predict crack direction and the Forman fatigue equation, modified with an equivalent stress intensity solution for mixed-mode, to predict extension. Comparisons with benchmark solutions and field data verified the computational methodology and defined the limits of its applicability.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLife Prediction for Complex Structures
    typeJournal Paper
    journal volume127
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.1448330
    journal fristpage814
    journal lastpage819
    identifier eissn0742-4795
    keywordsStress
    keywordsFracture (Materials)
    keywordsFracture (Process)
    keywordsEquations
    keywordsSpectra (Spectroscopy)
    keywordsFatigue
    keywordsElastic half space
    keywordsFunctions AND Force
    treeJournal of Engineering for Gas Turbines and Power:;2005:;volume( 127 ):;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
    yabeshDSpacePersian