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dc.contributor.author | Bakhtieva L. | |
dc.contributor.author | Tazyukov F. | |
dc.date.accessioned | 2018-09-18T20:34:43Z | |
dc.date.available | 2018-09-18T20:34:43Z | |
dc.date.issued | 2014 | |
dc.identifier.issn | 1995-0802 | |
dc.identifier.uri | https://dspace.kpfu.ru/xmlui/handle/net/141331 | |
dc.description.abstract | © 2014, Pleiades Publishing, Ltd. The stability problem for a thin shell under an axial impulsive load is considered. A new approach to building a mathematical model is presented, which is based on the Ostrogradskii-Hamilton principle of stationary action. It is shown that the problem reduces to a system of nonlinear differential equations that can be solved numerically and by using an approximate calculation algorithm developed by the authors. A formula determining the dependence between the load intensity and the initial conditions of the problem is derived. In the above setting, the stability problem for a circular cylindrical shell is solved. To determine the critical value of the load impulse, the Lyapunov theory of dynamic stability is used. | |
dc.relation.ispartofseries | Lobachevskii Journal of Mathematics | |
dc.subject | impulse | |
dc.subject | shell | |
dc.subject | stability | |
dc.title | Solution of the stability problem for a thin shell under impulsive loading | |
dc.type | Article | |
dc.relation.ispartofseries-issue | 4 | |
dc.relation.ispartofseries-volume | 35 | |
dc.collection | Публикации сотрудников КФУ | |
dc.relation.startpage | 384 | |
dc.source.id | SCOPUS19950802-2014-35-4-SID84915778947 |