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    Optimal Cool Down in Nonlinear Thermoviscoelasticity With Application to Graphite/Peek (APC-2) Laminates

    Source: Journal of Applied Mechanics:;1994:;volume( 061 ):;issue: 002::page 367
    Author:
    K. Lee
    ,
    Y. Weitsman
    DOI: 10.1115/1.2901453
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Many thermoplastic resin composite laminates, such as those made of APC-2, undergo a substantial temperature drop during their post-manufacturing cool down. This thermal excursion induces significant residual thermal stresses into the laminate due to the mutual geometric constraints among the multidirectional plies. In view of the considerable time-dependent relaxation which occurs during the cooling process, the residual thermal stresses exhibit strong dependence on the temperature history. However, in view of the high magnitudes of those stresses, the relaxation behavior is viscoelastically nonlinear. This paper demonstrates that it is possible to obtain an optimal cool-down path which minimizes the residual thermal stresses in APC-2 composites upon the termination of the cooling process.
    keyword(s): Laminates , Graphite , Thermal stresses , Relaxation (Physics) , Temperature , Cooling , Composite materials , Manufacturing , Stress , Drops AND Resins ,
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      Optimal Cool Down in Nonlinear Thermoviscoelasticity With Application to Graphite/Peek (APC-2) Laminates

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/113124
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    • Journal of Applied Mechanics

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    contributor authorK. Lee
    contributor authorY. Weitsman
    date accessioned2017-05-08T23:43:23Z
    date available2017-05-08T23:43:23Z
    date copyrightJune, 1994
    date issued1994
    identifier issn0021-8936
    identifier otherJAMCAV-26356#367_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/113124
    description abstractMany thermoplastic resin composite laminates, such as those made of APC-2, undergo a substantial temperature drop during their post-manufacturing cool down. This thermal excursion induces significant residual thermal stresses into the laminate due to the mutual geometric constraints among the multidirectional plies. In view of the considerable time-dependent relaxation which occurs during the cooling process, the residual thermal stresses exhibit strong dependence on the temperature history. However, in view of the high magnitudes of those stresses, the relaxation behavior is viscoelastically nonlinear. This paper demonstrates that it is possible to obtain an optimal cool-down path which minimizes the residual thermal stresses in APC-2 composites upon the termination of the cooling process.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOptimal Cool Down in Nonlinear Thermoviscoelasticity With Application to Graphite/Peek (APC-2) Laminates
    typeJournal Paper
    journal volume61
    journal issue2
    journal titleJournal of Applied Mechanics
    identifier doi10.1115/1.2901453
    journal fristpage367
    journal lastpage374
    identifier eissn1528-9036
    keywordsLaminates
    keywordsGraphite
    keywordsThermal stresses
    keywordsRelaxation (Physics)
    keywordsTemperature
    keywordsCooling
    keywordsComposite materials
    keywordsManufacturing
    keywordsStress
    keywordsDrops AND Resins
    treeJournal of Applied Mechanics:;1994:;volume( 061 ):;issue: 002
    contenttypeFulltext
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