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    Fatigue Cracking in Fiber-Reinforced Metal Matrix Composites Under Mechanical and Thermal Loads

    Source: Journal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 002::page 416
    Author:
    G. Bao
    ,
    R. M. McMeeking
    DOI: 10.1115/1.2816606
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This article reviews micromechanical models developed for fatigue cracking in fiber-reinforced metal matrix composites under mechanical and thermal loads. Emphasis is placed on the formulae and design charts that can quantify the fatigue crack growth and fiber fracture. The composite is taken to be linear elastic, with unidirectional aligned fibers. Interfacial debonding is assumed to occur readily, allowing fibers to slide relative to the matrix resisted by a uniform shear stress. The fibers therefore bridge any matrix crack that develops. The crack bridging traction law includes the effect of thermal expansion mismatch between the fiber and the matrix and a temperature dependence of the frictional shear stress. Predictions are made of the crack tip stress intensities, matrix fatigue crack growth, and maximum fiber stresses under mechanical or thermomechanical loads. For composites under thermomechanical load, both in-phase and out-of-phase fatigue are modeled. The implications for life prediction for fiber-reinforced metal matrix composites are discussed.
    keyword(s): Fibers , Metal matrix composites , Stress , Fatigue cracks , Shear (Mechanics) , Composite materials , Design , Fracture (Process) , Formulas , Traction , Thermal expansion , Fatigue AND Temperature ,
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      Fatigue Cracking in Fiber-Reinforced Metal Matrix Composites Under Mechanical and Thermal Loads

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/116955
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorG. Bao
    contributor authorR. M. McMeeking
    date accessioned2017-05-08T23:50:09Z
    date available2017-05-08T23:50:09Z
    date copyrightApril, 1996
    date issued1996
    identifier issn1528-8919
    identifier otherJETPEZ-26751#416_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/116955
    description abstractThis article reviews micromechanical models developed for fatigue cracking in fiber-reinforced metal matrix composites under mechanical and thermal loads. Emphasis is placed on the formulae and design charts that can quantify the fatigue crack growth and fiber fracture. The composite is taken to be linear elastic, with unidirectional aligned fibers. Interfacial debonding is assumed to occur readily, allowing fibers to slide relative to the matrix resisted by a uniform shear stress. The fibers therefore bridge any matrix crack that develops. The crack bridging traction law includes the effect of thermal expansion mismatch between the fiber and the matrix and a temperature dependence of the frictional shear stress. Predictions are made of the crack tip stress intensities, matrix fatigue crack growth, and maximum fiber stresses under mechanical or thermomechanical loads. For composites under thermomechanical load, both in-phase and out-of-phase fatigue are modeled. The implications for life prediction for fiber-reinforced metal matrix composites are discussed.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFatigue Cracking in Fiber-Reinforced Metal Matrix Composites Under Mechanical and Thermal Loads
    typeJournal Paper
    journal volume118
    journal issue2
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2816606
    journal fristpage416
    journal lastpage423
    identifier eissn0742-4795
    keywordsFibers
    keywordsMetal matrix composites
    keywordsStress
    keywordsFatigue cracks
    keywordsShear (Mechanics)
    keywordsComposite materials
    keywordsDesign
    keywordsFracture (Process)
    keywordsFormulas
    keywordsTraction
    keywordsThermal expansion
    keywordsFatigue AND Temperature
    treeJournal of Engineering for Gas Turbines and Power:;1996:;volume( 118 ):;issue: 002
    contenttypeFulltext
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