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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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