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    Tensile Behavior of Glass/Ceramic Composite Materials at Elevated Temperatures

    Source: Journal of Engineering for Gas Turbines and Power:;1987:;volume( 109 ):;issue: 003::page 267
    Author:
    J. F. Mandell
    ,
    D. H. Grande
    ,
    J. Jacobs
    DOI: 10.1115/1.3240035
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the tensile behavior of high-temperature composite materials containing continuous Nicalon ceramic fiber reinforcement and glass and glass/ceramic matrices. The longitudinal properties of these materials can approach theoretical expectations for brittle matrix composites, failing at a strength and ultimate strain level consistent with those of the fibers. The brittle, high-modulus matrices result in a nonlinear stress-strain curve due to the onset of stable matrix cracking at 10 to 30 percent of the fiber strain to failure, and at strains below this range in off-axis plies. Current fibers and matrices can provide attractive properties well above 1000°C, but composites experience embrittlement in oxidizing atmospheres at 800 to 1000°C due to oxidation of a carbon interface reaction layer. The oxidation effect greatly increases the interface bond strength, causing composite embrittlement.
    keyword(s): Temperature , Glass , Ceramic composites , Composite materials , Fibers , Brittleness , Embrittlement , oxidation , High temperature , Failure , Ceramic fibers , Stress-strain curves , Bond strength , Carbon , Fracture (Process) AND Ceramics ,
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      Tensile Behavior of Glass/Ceramic Composite Materials at Elevated Temperatures

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/102430
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorJ. F. Mandell
    contributor authorD. H. Grande
    contributor authorJ. Jacobs
    date accessioned2017-05-08T23:24:44Z
    date available2017-05-08T23:24:44Z
    date copyrightJuly, 1987
    date issued1987
    identifier issn1528-8919
    identifier otherJETPEZ-26647#267_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/102430
    description abstractThis paper describes the tensile behavior of high-temperature composite materials containing continuous Nicalon ceramic fiber reinforcement and glass and glass/ceramic matrices. The longitudinal properties of these materials can approach theoretical expectations for brittle matrix composites, failing at a strength and ultimate strain level consistent with those of the fibers. The brittle, high-modulus matrices result in a nonlinear stress-strain curve due to the onset of stable matrix cracking at 10 to 30 percent of the fiber strain to failure, and at strains below this range in off-axis plies. Current fibers and matrices can provide attractive properties well above 1000°C, but composites experience embrittlement in oxidizing atmospheres at 800 to 1000°C due to oxidation of a carbon interface reaction layer. The oxidation effect greatly increases the interface bond strength, causing composite embrittlement.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleTensile Behavior of Glass/Ceramic Composite Materials at Elevated Temperatures
    typeJournal Paper
    journal volume109
    journal issue3
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3240035
    journal fristpage267
    journal lastpage273
    identifier eissn0742-4795
    keywordsTemperature
    keywordsGlass
    keywordsCeramic composites
    keywordsComposite materials
    keywordsFibers
    keywordsBrittleness
    keywordsEmbrittlement
    keywordsoxidation
    keywordsHigh temperature
    keywordsFailure
    keywordsCeramic fibers
    keywordsStress-strain curves
    keywordsBond strength
    keywordsCarbon
    keywordsFracture (Process) AND Ceramics
    treeJournal of Engineering for Gas Turbines and Power:;1987:;volume( 109 ):;issue: 003
    contenttypeFulltext
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