Показать сокращенную информацию
dc.contributor.author | Elizarov A. | |
dc.contributor.author | Fokin D. | |
dc.date.accessioned | 2018-09-17T21:53:52Z | |
dc.date.available | 2018-09-17T21:53:52Z | |
dc.date.issued | 1999 | |
dc.identifier.issn | 0044-2267 | |
dc.identifier.uri | https://dspace.kpfu.ru/xmlui/handle/net/135574 | |
dc.description.abstract | In the present work the method of the inverse boundary-value problems is used to obtain upper estimates for two main integral airfoil characteristics: lift coefficient Cl and the aerodynamic ratio K in a certain class of airfoils flown by an incompressible flow of viscous fluid at a fixed angle of attack at high Reynolds number (106-107) with the presence of a thin non-separating turbulent boundary layer. | |
dc.relation.ispartofseries | ZAMM Zeitschrift fur Angewandte Mathematik und Mechanik | |
dc.title | Upper estimates of airfoil aerodynamic characteristics for a viscous incompressible flow | |
dc.type | Article | |
dc.relation.ispartofseries-issue | 11 | |
dc.relation.ispartofseries-volume | 79 | |
dc.collection | Публикации сотрудников КФУ | |
dc.relation.startpage | 757 | |
dc.source.id | SCOPUS00442267-1999-79-11-SID33645962351 |