dc.contributor.author |
Kayumov R. |
|
dc.contributor.author |
Zakirov I. |
|
dc.contributor.author |
Alekseev K. |
|
dc.contributor.author |
Zinnurov R. |
|
dc.date.accessioned |
2018-09-18T20:17:59Z |
|
dc.date.available |
2018-09-18T20:17:59Z |
|
dc.date.issued |
2007 |
|
dc.identifier.issn |
1068-7998 |
|
dc.identifier.uri |
https://dspace.kpfu.ru/xmlui/handle/net/138456 |
|
dc.description.abstract |
In this paper, the problem on creation of a mathematical model describing the behavior of a sandwich panel with chevron-type cores is considered. The model is meant for calculating the ultimate shearing compressive loads and its parameters are determined by the identification methods on the basis of experimental data. © Allerton Press, Inc. 2007. |
|
dc.relation.ispartofseries |
Russian Aeronautics |
|
dc.title |
Determination of load-carrying capacity in panels with chevron-type cores |
|
dc.type |
Article |
|
dc.relation.ispartofseries-issue |
4 |
|
dc.relation.ispartofseries-volume |
50 |
|
dc.collection |
Публикации сотрудников КФУ |
|
dc.relation.startpage |
357 |
|
dc.source.id |
SCOPUS10687998-2007-50-4-SID42449129245 |
|