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

Please use this identifier to cite or link to this item: https://er.nau.edu.ua/handle/NAU/31967

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DC Field	Value	Language
dc.contributor.author	Ignatovich, S.R.	-
dc.contributor.author	Karuskevich, M.V.	-
dc.contributor.author	Yutskevych, S.S.	-
dc.date.accessioned	2017-12-17T14:42:28Z	-
dc.date.available	2017-12-17T14:42:28Z	-
dc.date.issued	2017	-
dc.identifier.issn	0142-1123	-
dc.identifier.uri	http://er.nau.edu.ua/handle/NAU/31967	-
dc.description	International Journal of Fatigue	uk_UA
dc.description.abstract	The 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.language.iso	en	uk_UA
dc.publisher	IPC Science and Technology Press	uk_UA
dc.title	Evolution of the deformation relief on the surface of a clad aluminum alloy at random cyclic loads	uk_UA
dc.type	Article	uk_UA
dc.speciality	Reliability and Durability	uk_UA
Appears in Collections:	Статті в наукових виданнях кафедри конструкції літальних апаратів

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