Evolution of the deformation relief on the surface of a clad aluminum alloy at random cyclic loads

dc.contributor.authorIgnatovich, S.R.
dc.contributor.authorKaruskevich, M.V.
dc.contributor.authorYutskevych, S.S.
dc.date.accessioned2017-12-17T14:42:28Z
dc.date.available2017-12-17T14:42:28Z
dc.date.issued2017
dc.descriptionInternational Journal of Fatigueuk_UA
dc.description.abstractThe deformation relief was revealed to be formed and evolved on the surface of a cladding layer of a D16AT aluminum alloy under random cyclic loading. The surface saturation, roughness, and microplastic deformation are found to be quantitative estimates of the deformation relief and damage levels. Experimental deformation relief characteristics-load cycle number relations are similar and can be employed for predicting the fatigue crack initiation in aircraft structure elements.uk_UA
dc.identifier.issn0142-1123
dc.identifier.urihttp://er.nau.edu.ua/handle/NAU/31967
dc.language.isoenuk_UA
dc.publisherIPC Science and Technology Pressuk_UA
dc.specialityReliability and Durabilityuk_UA
dc.titleEvolution of the deformation relief on the surface of a clad aluminum alloy at random cyclic loadsuk_UA
dc.typeArticleuk_UA

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