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Stability of a cylindrical shell under axial compression

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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.

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