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    Fabrication Stresses in Graphite-Resin Composites

    Source: Journal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 004::page 377
    Author:
    R. C. Novak
    ,
    M. A. DeCrescente
    DOI: 10.1115/1.3445367
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Residual thermal stresses are present in cross-plied graphite-epoxy composites due to the anisotropic thermal and mechanical properties of the individual layers. Experimental measurements and analytical calculations of the thermal stress induced in two different cross-plied composites during fabrication are presented and shown to be in good agreement. The occurrence of cracking in certain composites is explained in terms of the transverse tensile strength of the unidirectional composite layers and the stress developed during fabrication. Two approaches are presented to avoid cracking during fabrication.
    keyword(s): Composite materials , Manufacturing , Stress , Graphite , Resins , Thermal stresses , Fracture (Process) , Mechanical properties , Tensile strength , Epoxy adhesives AND Measurement ,
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      Fabrication Stresses in Graphite-Resin Composites

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/142067
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorR. C. Novak
    contributor authorM. A. DeCrescente
    date accessioned2017-05-09T00:35:36Z
    date available2017-05-09T00:35:36Z
    date copyrightOctober, 1970
    date issued1970
    identifier issn1528-8919
    identifier otherJETPEZ-26688#377_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/142067
    description abstractResidual thermal stresses are present in cross-plied graphite-epoxy composites due to the anisotropic thermal and mechanical properties of the individual layers. Experimental measurements and analytical calculations of the thermal stress induced in two different cross-plied composites during fabrication are presented and shown to be in good agreement. The occurrence of cracking in certain composites is explained in terms of the transverse tensile strength of the unidirectional composite layers and the stress developed during fabrication. Two approaches are presented to avoid cracking during fabrication.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleFabrication Stresses in Graphite-Resin Composites
    typeJournal Paper
    journal volume92
    journal issue4
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3445367
    journal fristpage377
    journal lastpage380
    identifier eissn0742-4795
    keywordsComposite materials
    keywordsManufacturing
    keywordsStress
    keywordsGraphite
    keywordsResins
    keywordsThermal stresses
    keywordsFracture (Process)
    keywordsMechanical properties
    keywordsTensile strength
    keywordsEpoxy adhesives AND Measurement
    treeJournal of Engineering for Gas Turbines and Power:;1970:;volume( 092 ):;issue: 004
    contenttypeFulltext
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