Monitoring of the fatigue of D16АТ alloy according to the characteristics of deformation surface pattern

dc.contributor.authorIgnatovich, S.R.
dc.contributor.authorYutskevich, S.S.
dc.date.accessioned2017-10-14T13:22:20Z
dc.date.available2017-10-14T13:22:20Z
dc.date.issued2012
dc.descriptionMaterials Science, Vol. 47, No. 5uk_UA
dc.description.abstractIt is shown that the deformation pattern is formed under cyclic loads and develops on the surface of the cladding layer of a structural aluminum alloy. The quantitative parameters of the deformation pattern, namely, the saturation, roughness, and plastic strains on the surface, serve as indicators of damage to the material. The experimental dependences of the analyzed parameters on the operating time (number of loading cycles) can be used for the creation of new methods aimed at the prediction of the limit state of structural elements of the aircraft structures.uk_UA
dc.identifier.issn1068-820X
dc.identifier.issn1573-885X
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/30711
dc.language.isoenuk_UA
dc.publisherSpringer Science+Business Media, Inc.uk_UA
dc.subjectdeformation patternuk_UA
dc.subjectinterference profilometryuk_UA
dc.subjectfatigueuk_UA
dc.subjectparameters of the deformation patternuk_UA
dc.titleMonitoring of the fatigue of D16АТ alloy according to the characteristics of deformation surface patternuk_UA
dc.typeArticleuk_UA

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