Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/32283
Full metadata record
DC FieldValueLanguage
dc.contributor.authorKaruskevich, M.V.-
dc.date.accessioned2017-12-26T12:45:12Z-
dc.date.available2017-12-26T12:45:12Z-
dc.date.issued2014-
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/32283-
dc.descriptionВісник НАУ, 2012, №1uk_UA
dc.description.abstractThe investigations of the new fatigue sensor that was carried out at the wide range of cyclic loads conditions show the ability of the indicator application in Structural Health Monitoring systems of planes, bridges, vessels, and other structures. Accumulated fatigue damage may by estimated by the intensity of deformation relief, i.e. by its extrusion/intrusion and persistent slip bands structures on the indicator surface.uk_UA
dc.language.isoenuk_UA
dc.publisherНіціональний авіаційний університетuk_UA
dc.subjectalclad aluminum alloysuk_UA
dc.subjectdeformation reliefuk_UA
dc.subjectfatigueuk_UA
dc.subjectfatigue indicatoruk_UA
dc.titleFatigue life prediction by the structurally sensitive damage indicatoruk_UA
dc.typeArticleuk_UA
dc.subject.udc620.179.1-
dc.specialityReliability and durabilityuk_UA
Appears in Collections:Статті в наукових виданнях кафедри конструкції літальних апаратів

Files in This Item:
File Description SizeFormat 
Sensor.pdfСтаття3.73 MBAdobe PDFView/Open


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