Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/32282
Full metadata record
DC FieldValueLanguage
dc.contributor.authorKaruskevich, M.V.-
dc.contributor.authorKaruskevich, O.-
dc.contributor.authorMaslak, T.P.-
dc.contributor.authorSchepak, S.V.-
dc.date.accessioned2017-12-26T12:38:04Z-
dc.date.available2017-12-26T12:38:04Z-
dc.date.issued2011-02-22-
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/32282-
dc.descriptionInternational Journal of Fatigue 39 (2012)uk_UA
dc.description.abstractTwo approaches to aircraft fatigue monitoring by the computer-aided analysis of surface structures are described: (a) application of fatigue indicators attached to the aircraft unit; (b) the direct observation of the alclad aluminium alloys surface. The evolution of aluminium surface state has been monitored at various fatigue loading regimes. Some parameters have been used for the quantitative analysis of surface structures: (a) density of slip lines for single-crystals; (b) intensity and fractal dimensions of the deformation relief for polycrystalline aluminium. The possibility of a fatigue process prediction both at crack initiation stage and fatigue crack propagation stage is shown.uk_UA
dc.language.isoenuk_UA
dc.publisherIPC Science and Technology Pressuk_UA
dc.subjectFull scale fatigue testinguk_UA
dc.subjectLife predictionuk_UA
dc.subjectAluminium alloysuk_UA
dc.subjectDamage accumulationuk_UA
dc.subjectFatigue initiationuk_UA
dc.titleExtrusion/intrusion structures as quantitative indicators of accumulated fatigue damageuk_UA
dc.typeArticleuk_UA
dc.specialityReliability and Durabilityuk_UA
Appears in Collections:Статті в наукових виданнях кафедри конструкції літальних апаратів

Files in This Item:
File Description SizeFormat 
IJF.pdfСтаття1.08 MBAdobe PDFView/Open


Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.