dc.contributor.author |
Gainutdinova T. |
|
dc.contributor.author |
Mirkhazov R. |
|
dc.date.accessioned |
2018-09-18T20:18:05Z |
|
dc.date.available |
2018-09-18T20:18:05Z |
|
dc.date.issued |
2011 |
|
dc.identifier.issn |
1068-7998 |
|
dc.identifier.uri |
https://dspace.kpfu.ru/xmlui/handle/net/138476 |
|
dc.description.abstract |
An algorithm of analyzing the design parameters for a thin-walled wing from composite material based on the efficient distribution of structural material between load-carrying elements is described. We consider the problems of convergence acceleration for the iteration design analysis. Also presented are the examples of determining the design parameters for a superlight aircraft wing and the rational parameters of the filler in the form of a three-dimensional rod structure. © 2011 Allerton Press, Inc. |
|
dc.relation.ispartofseries |
Russian Aeronautics |
|
dc.subject |
Composite material |
|
dc.subject |
Design analysis automation |
|
dc.subject |
Software package |
|
dc.subject |
Thin-walled structure |
|
dc.title |
A software package for computer-aided design analysis of thin-walled structures from composite materials |
|
dc.type |
Article |
|
dc.relation.ispartofseries-issue |
4 |
|
dc.relation.ispartofseries-volume |
54 |
|
dc.collection |
Публикации сотрудников КФУ |
|
dc.relation.startpage |
334 |
|
dc.source.id |
SCOPUS10687998-2011-54-4-SID84860858540 |
|