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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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