Stability of a cylindrical shell under axial compression

dc.contributor.author	Bakhtieva L.
dc.contributor.author	Tazyukov F.
dc.date.accessioned	2018-09-18T20:18:08Z
dc.date.available	2018-09-18T20:18:08Z
dc.date.issued	2015
dc.identifier.issn	1068-7998
dc.identifier.uri	https://dspace.kpfu.ru/xmlui/handle/net/138485
dc.description.abstract	© 2015, Allerton Press, Inc. A new approach to solving the task of stability for a circular cylindrical shell under axial compression is presented, taking into account the dynamic buckling. The modification of the algorithm for solving the known problem by the Ritz method is also proposed that allows investigating the effect of geometrical factors on the buckling load.
dc.relation.ispartofseries	Russian Aeronautics
dc.subject	buckling load
dc.subject	deflection
dc.subject	shell
dc.subject	stability
dc.title	Stability of a cylindrical shell under axial compression
dc.type	Article
dc.relation.ispartofseries-issue	1
dc.relation.ispartofseries-volume	58
dc.collection	Публикации сотрудников КФУ
dc.relation.startpage	106
dc.source.id	SCOPUS10687998-2015-58-1-SID84935036018

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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.