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    Accelerated Aging of the Thermal Expansion of Unidirectional Graphite/Epoxy Composites by Thermal Fatigue

    Source: Journal of Engineering Materials and Technology:;1989:;volume( 111 ):;issue: 004::page 331
    Author:
    W. L. Morris
    ,
    M. R. James
    ,
    R. V. Inman
    DOI: 10.1115/1.3226475
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The longitudinal coefficient of thermal expansion (α1 ) of unidirectional T300/934 and AS/3501-5A graphite/epoxy (Gr/Ep) composite changes within a thousand thermal cycles at ranges greater than 210°C. A phenomenological model is developed to extrapolate α1 to a smaller thermal range (< 100°C) and longer duration (2×105 cycles) typical of service in low earth orbit. Factors affecting fiber/matrix interface cracking are considered, and the utility of calculating α1 from an “effective” fiber volume fraction, which excludes from the volume fiber segments disbonded from the matrix, is demonstrated. This analysis is used to estimate the effect of fiber volume on α1 of T300/934 Gr/Ep during thermal fatigue.
    keyword(s): Thermal expansion , Fatigue , Composite materials , Epoxy adhesives , Graphite , Fibers , Cycles AND Fracture (Process) ,
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      Accelerated Aging of the Thermal Expansion of Unidirectional Graphite/Epoxy Composites by Thermal Fatigue

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/105452
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    • Journal of Engineering Materials and Technology

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    contributor authorW. L. Morris
    contributor authorM. R. James
    contributor authorR. V. Inman
    date accessioned2017-05-08T23:30:06Z
    date available2017-05-08T23:30:06Z
    date copyrightOctober, 1989
    date issued1989
    identifier issn0094-4289
    identifier otherJEMTA8-26931#331_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/105452
    description abstractThe longitudinal coefficient of thermal expansion (α1 ) of unidirectional T300/934 and AS/3501-5A graphite/epoxy (Gr/Ep) composite changes within a thousand thermal cycles at ranges greater than 210°C. A phenomenological model is developed to extrapolate α1 to a smaller thermal range (< 100°C) and longer duration (2×105 cycles) typical of service in low earth orbit. Factors affecting fiber/matrix interface cracking are considered, and the utility of calculating α1 from an “effective” fiber volume fraction, which excludes from the volume fiber segments disbonded from the matrix, is demonstrated. This analysis is used to estimate the effect of fiber volume on α1 of T300/934 Gr/Ep during thermal fatigue.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleAccelerated Aging of the Thermal Expansion of Unidirectional Graphite/Epoxy Composites by Thermal Fatigue
    typeJournal Paper
    journal volume111
    journal issue4
    journal titleJournal of Engineering Materials and Technology
    identifier doi10.1115/1.3226475
    journal fristpage331
    journal lastpage337
    identifier eissn1528-8889
    keywordsThermal expansion
    keywordsFatigue
    keywordsComposite materials
    keywordsEpoxy adhesives
    keywordsGraphite
    keywordsFibers
    keywordsCycles AND Fracture (Process)
    treeJournal of Engineering Materials and Technology:;1989:;volume( 111 ):;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
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