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    Interlaminar Crack Growth Resistances of Various Ceramic Matrix Composites in Mode I and Mode II Loading

    Source: Journal of Engineering for Gas Turbines and Power:;2008:;volume( 130 ):;issue: 003::page 31301
    Author:
    Sung R. Choi
    ,
    Robert W. Kowalik
    DOI: 10.1115/1.2800349
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Interlaminar crack growth resistances were evaluated for five different SiC fiber-reinforced ceramic matrix composites (CMCs) including three gas-turbine grade melt-infiltrated SiC∕SiC composites. Modes I and II crack growth resistances, GI and GII, were determined at ambient temperature using double cantilever beam and end notched flexure methods, respectively. The CMCs exhibited GI=200–500J∕m2 and GII=200–900J∕m2. All the composites (except for one SiC/CAS composite) showed a rising R-curve behavior either in mode I or in mode II, presumably attributed to fiber bridging (in modes I and II) and frictional constraint (mode II) in the wake region of a propagating crack. A glass fiber-reinforced epoxy polymer matrix composite showed typically two to three times greater GI and eight times greater GII, compared to the CMCs. An experimental error analysis regarding the effect of the off-the-center of a crack plane on GI and GII was also made.
    keyword(s): Composite materials , Fibers , Ceramic matrix composites , Fracture (Materials) , Glass , Epoxy adhesives , Bending (Stress) , Cantilever beams AND Temperature ,
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      Interlaminar Crack Growth Resistances of Various Ceramic Matrix Composites in Mode I and Mode II Loading

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/137919
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorSung R. Choi
    contributor authorRobert W. Kowalik
    date accessioned2017-05-09T00:27:53Z
    date available2017-05-09T00:27:53Z
    date copyrightMay, 2008
    date issued2008
    identifier issn1528-8919
    identifier otherJETPEZ-27012#031301_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/137919
    description abstractInterlaminar crack growth resistances were evaluated for five different SiC fiber-reinforced ceramic matrix composites (CMCs) including three gas-turbine grade melt-infiltrated SiC∕SiC composites. Modes I and II crack growth resistances, GI and GII, were determined at ambient temperature using double cantilever beam and end notched flexure methods, respectively. The CMCs exhibited GI=200–500J∕m2 and GII=200–900J∕m2. All the composites (except for one SiC/CAS composite) showed a rising R-curve behavior either in mode I or in mode II, presumably attributed to fiber bridging (in modes I and II) and frictional constraint (mode II) in the wake region of a propagating crack. A glass fiber-reinforced epoxy polymer matrix composite showed typically two to three times greater GI and eight times greater GII, compared to the CMCs. An experimental error analysis regarding the effect of the off-the-center of a crack plane on GI and GII was also made.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInterlaminar Crack Growth Resistances of Various Ceramic Matrix Composites in Mode I and Mode II Loading
    typeJournal Paper
    journal volume130
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.2800349
    journal fristpage31301
    identifier eissn0742-4795
    keywordsComposite materials
    keywordsFibers
    keywordsCeramic matrix composites
    keywordsFracture (Materials)
    keywordsGlass
    keywordsEpoxy adhesives
    keywordsBending (Stress)
    keywordsCantilever beams AND Temperature
    treeJournal of Engineering for Gas Turbines and Power:;2008:;volume( 130 ):;issue: 003
    contenttypeFulltext
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