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    Effect of Wrought Product Thickness and Stress Ratio on Fatigue Crack Growth Behavior of a Quaternary Aluminium-Lithium Alloy

    Source: Journal of Engineering Materials and Technology:;1999:;volume( 121 ):;issue: 003::page 393
    Author:
    Vikas Kumar Saxena
    ,
    V. M. Radhakrishnan
    DOI: 10.1115/1.2812392
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Effect of thickness on fatigue crack growth (FCG) behavior has been investigated at varying stress ratio in a quaternary Al-Li alloy. The thickness has been observed to influence FCG behavior in two opposite ways, depending on stress ratio. The crack closure concept has been invoked to rationalize the observed behavior. The roughness-induced crack closure is the main governing mechanism in the alloy under investigation. Factors such as fracture surface asperity size and severity of plane strain condition have been argued to affect the extent of crack closure, and consequently, fatigue crack growth behavior.
    keyword(s): Aluminum , Alloys , Stress , Fatigue cracks , Lithium , Thickness , Mechanisms , Plane strain , Fracture (Process) AND Surface roughness ,
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      Effect of Wrought Product Thickness and Stress Ratio on Fatigue Crack Growth Behavior of a Quaternary Aluminium-Lithium Alloy

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/122236
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    contributor authorVikas Kumar Saxena
    contributor authorV. M. Radhakrishnan
    date accessioned2017-05-08T23:59:47Z
    date available2017-05-08T23:59:47Z
    date copyrightJuly, 1999
    date issued1999
    identifier issn0094-4289
    identifier otherJEMTA8-26999#393_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/122236
    description abstractEffect of thickness on fatigue crack growth (FCG) behavior has been investigated at varying stress ratio in a quaternary Al-Li alloy. The thickness has been observed to influence FCG behavior in two opposite ways, depending on stress ratio. The crack closure concept has been invoked to rationalize the observed behavior. The roughness-induced crack closure is the main governing mechanism in the alloy under investigation. Factors such as fracture surface asperity size and severity of plane strain condition have been argued to affect the extent of crack closure, and consequently, fatigue crack growth behavior.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleEffect of Wrought Product Thickness and Stress Ratio on Fatigue Crack Growth Behavior of a Quaternary Aluminium-Lithium Alloy
    typeJournal Paper
    journal volume121
    journal issue3
    journal titleJournal of Engineering Materials and Technology
    identifier doi10.1115/1.2812392
    journal fristpage393
    journal lastpage398
    identifier eissn1528-8889
    keywordsAluminum
    keywordsAlloys
    keywordsStress
    keywordsFatigue cracks
    keywordsLithium
    keywordsThickness
    keywordsMechanisms
    keywordsPlane strain
    keywordsFracture (Process) AND Surface roughness
    treeJournal of Engineering Materials and Technology:;1999:;volume( 121 ):;issue: 003
    contenttypeFulltext
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