Показать сокращенную информацию
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 |