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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 |