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dc.creatorPutić, Slaviša
dc.creatorUskoković, Petar
dc.creatorAleksić, Radoslav
dc.date.accessioned2021-03-10T10:04:48Z
dc.date.available2021-03-10T10:04:48Z
dc.date.issued2003
dc.identifier.issn0039-2316
dc.identifier.urihttp://TechnoRep.tmf.bg.ac.rs/handle/123456789/499
dc.description.abstractA study of high frequency fatigue in carbon-fiber reinforced composites has been undertaken. A comparison has been made between the fatigue behavior of crossply (0 / 90) and angleply (± 45) carbon/epoxy unnotched and notched laminates. Additionally, a micromechanical analysis of fracture surfaces performed by scanning electron microscopy was carried out to evaluate the micromechanisms that occurred during fatigue. Experimental observations indicate that fatigue damage consists of a combination of matrix cracks, longitudinal splitting, fiber fracture, delamination. In order to minimize the effects of residual strain due to temperature rise, a method is proposed for determining real fatigue strength at the level of variable load not lower than the fatigue limit, at which residual strains are minimal.en
dc.rightsrestrictedAccess
dc.sourceStrength of Materials
dc.subjectcomposite laminatesen
dc.subjectcrack growthen
dc.subjectfatigueen
dc.subjectS - N curveen
dc.titleAnalysis of fatigue and crack growth in carbon-fiber epoxy matrix composite laminatesen
dc.typearticle
dc.rights.licenseARR
dc.citation.epage507
dc.citation.issue5
dc.citation.other35(5): 500-507
dc.citation.spage500
dc.citation.volume35
dc.identifier.doi10.1023/B:STOM.0000004538.77270.1e
dc.identifier.pmid
dc.identifier.scopus2-s2.0-77953857237
dc.type.versionpublishedVersion


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Приказ основних података о документу