Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/31969
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dc.contributor.authorPetrasek, M.-
dc.contributor.authorIgnatovich, S. R.-
dc.contributor.authorKaruskevich, M. V.-
dc.contributor.authorMaslak, T. P.-
dc.date.accessioned2017-12-17T17:42:18Z-
dc.date.available2017-12-17T17:42:18Z-
dc.date.issued2013-12-
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/31969-
dc.descriptionAdvances in Military Technology, Vol. 8, No. 2, December 2013uk_UA
dc.description.abstractThe possibility of fatigue damage analysis by the extrusion/intrusion structures on the surface of aluminium alloy is shown. Quantitative characteristics of the extrusion/intrusion structures and the methods for their monitoring are substantiated. Two approaches for fatigue analysis are presented: a) direct inspection of the aircraft components, b) application of fatigue sensors.uk_UA
dc.language.isoenuk_UA
dc.publisherUniversity of Defenceuk_UA
dc.subjectaircraftuk_UA
dc.subjectfatigueuk_UA
dc.subjectalclad alloyuk_UA
dc.subjectdeformation reliefuk_UA
dc.subjectfatigue sensoruk_UA
dc.subjectstructural health monitoringuk_UA
dc.titleSurface of metal as an indicator of fatigue damageuk_UA
dc.typeArticleuk_UA
dc.specialityReliability and durabilityuk_UA
Appears in Collections:Статті в наукових виданнях кафедри конструкції літальних апаратів

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