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    Use of Statical Indentation Laws in the Impact Analysis of Laminated Composite Plates

    Source: Journal of Applied Mechanics:;1985:;volume( 052 ):;issue: 001::page 6
    Author:
    T. M. Tan
    ,
    C. T. Sun
    DOI: 10.1115/1.3169029
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The low-velocity impact response of graphite/epoxy laminates was investigated theoretically and experimentally. A nine-node isoparametric plate finite element in conjunction with an empirical contact law was used for the theoretical investigation. Theoretical results are in good agreement with strain-gage experimental data. The results of the investigation indicate that the present theoretical procedure describes the impact response of laminate for low-impact velocities.
    keyword(s): Composite materials , Plates (structures) , Laminates , Epoxy adhesives , Finite element analysis , Graphite AND Strain gages ,
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      Use of Statical Indentation Laws in the Impact Analysis of Laminated Composite Plates

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    https://yetl.yabesh.ir/yetl1/handle/yetl/99442
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    contributor authorT. M. Tan
    contributor authorC. T. Sun
    date accessioned2017-05-08T23:19:31Z
    date available2017-05-08T23:19:31Z
    date copyrightMarch, 1985
    date issued1985
    identifier issn0021-8936
    identifier otherJAMCAV-26250#6_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/99442
    description abstractThe low-velocity impact response of graphite/epoxy laminates was investigated theoretically and experimentally. A nine-node isoparametric plate finite element in conjunction with an empirical contact law was used for the theoretical investigation. Theoretical results are in good agreement with strain-gage experimental data. The results of the investigation indicate that the present theoretical procedure describes the impact response of laminate for low-impact velocities.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleUse of Statical Indentation Laws in the Impact Analysis of Laminated Composite Plates
    typeJournal Paper
    journal volume52
    journal issue1
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.3169029
    journal fristpage6
    journal lastpage12
    identifier eissn1528-9036
    keywordsComposite materials
    keywordsPlates (structures)
    keywordsLaminates
    keywordsEpoxy adhesives
    keywordsFinite element analysis
    keywordsGraphite AND Strain gages
    treeJournal of Applied Mechanics:;1985:;volume( 052 ):;issue: 001
    contenttypeFulltext
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