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    Interlaminar Fracture Toughness of a Graphite/Epoxy Multidirectional Composite1

    Source: Journal of Engineering Materials and Technology:;2000:;volume( 122 ):;issue: 004::page 428
    Author:
    Z. Yang
    ,
    C. T. Sun
    DOI: 10.1115/1.1289027
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, an experimental investigation on interlaminar fracture behavior and fracture toughness of a graphite/epoxy multidirectional composite laminate is presented using end-notched flexure specimens. The 0/θ interfaces are considered. The interlaminar fracture toughness is obtained and compared using three data reduction methods, i.e., the area method, classical laminated plate theory, and finite element analysis. Results show that the toughness value depends on the data reduction method used. Two different crack-length-to-span ratios are chosen to study how the stable or unstable crack extension influences the toughness measurement. It is observed that the toughness obtained from the tests of stable crack extension is appreciably higher than that from the tests of unstable crack extension. It is also seen that friction resulting from contact of crack surfaces greatly affects the measured toughness in the case of stable crack extension. In addition, effects of the specimen geometry and fiber orientation on the interlaminar fracture toughness are also evaluated. [S0094-4289(00)02804-8]
    keyword(s): Laminates , Fracture (Materials) , Fracture toughness , Toughness , Composite materials , Graphite , Epoxy adhesives , Finite element analysis , Fracture (Process) , Fibers AND Stress ,
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      Interlaminar Fracture Toughness of a Graphite/Epoxy Multidirectional Composite1

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    http://yetl.yabesh.ir/yetl1/handle/yetl/123742
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    contributor authorZ. Yang
    contributor authorC. T. Sun
    date accessioned2017-05-09T00:02:31Z
    date available2017-05-09T00:02:31Z
    date copyrightOctober, 2000
    date issued2000
    identifier issn0094-4289
    identifier otherJEMTA8-27013#428_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/123742
    description abstractIn this paper, an experimental investigation on interlaminar fracture behavior and fracture toughness of a graphite/epoxy multidirectional composite laminate is presented using end-notched flexure specimens. The 0/θ interfaces are considered. The interlaminar fracture toughness is obtained and compared using three data reduction methods, i.e., the area method, classical laminated plate theory, and finite element analysis. Results show that the toughness value depends on the data reduction method used. Two different crack-length-to-span ratios are chosen to study how the stable or unstable crack extension influences the toughness measurement. It is observed that the toughness obtained from the tests of stable crack extension is appreciably higher than that from the tests of unstable crack extension. It is also seen that friction resulting from contact of crack surfaces greatly affects the measured toughness in the case of stable crack extension. In addition, effects of the specimen geometry and fiber orientation on the interlaminar fracture toughness are also evaluated. [S0094-4289(00)02804-8]
    publisherThe American Society of Mechanical Engineers (ASME)
    titleInterlaminar Fracture Toughness of a Graphite/Epoxy Multidirectional Composite1
    typeJournal Paper
    journal volume122
    journal issue4
    journal titleJournal of Engineering Materials and Technology
    identifier doi10.1115/1.1289027
    journal fristpage428
    journal lastpage433
    identifier eissn1528-8889
    keywordsLaminates
    keywordsFracture (Materials)
    keywordsFracture toughness
    keywordsToughness
    keywordsComposite materials
    keywordsGraphite
    keywordsEpoxy adhesives
    keywordsFinite element analysis
    keywordsFracture (Process)
    keywordsFibers AND Stress
    treeJournal of Engineering Materials and Technology:;2000:;volume( 122 ):;issue: 004
    contenttypeFulltext
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