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 |
|