The use of the finite element calculations to assess the impact of prolonged use on strength reliability of the turbine disk aviation engine

dc.contributor.author	Velikanova N.
dc.contributor.author	Velikanov P.
dc.contributor.author	Kiselev A.
dc.contributor.author	S Salih S.
dc.date.accessioned	2020-01-15T21:49:01Z
dc.date.available	2020-01-15T21:49:01Z
dc.date.issued	2019
dc.identifier.issn	1742-6588
dc.identifier.uri	https://dspace.kpfu.ru/xmlui/handle/net/156174
dc.description.abstract	© Published under licence by IOP Publishing Ltd. Based on the results of the calculation of the turbine disk by the finite element method and on the results of experimental tests of the disk samples from the heat-resistant deformable alloy under pulsing isothermal loading cycle, the effect of long-term operational life on the characteristics of the strength reliability of the disk is evaluated.
dc.relation.ispartofseries	Journal of Physics: Conference Series
dc.title	The use of the finite element calculations to assess the impact of prolonged use on strength reliability of the turbine disk aviation engine
dc.type	Conference Paper
dc.relation.ispartofseries-issue	4
dc.relation.ispartofseries-volume	1158
dc.collection	Публикации сотрудников КФУ
dc.source.id	SCOPUS17426588-2019-1158-4-SID85063808819

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Публикации сотрудников КФУ Scopus [24551]
Коллекция содержит публикации сотрудников Казанского федерального (до 2010 года Казанского государственного) университета, проиндексированные в БД Scopus, начиная с 1970г.