Design of airfoils providing the absence of separation in a compressible flow in a specified range of angles of attack

dc.contributor.author	Dunaeva O.
dc.contributor.author	Il'inskii N.
dc.date.accessioned	2018-09-18T20:04:32Z
dc.date.available	2018-09-18T20:04:32Z
dc.date.issued	2008
dc.identifier.issn	0021-8944
dc.identifier.uri	https://dspace.kpfu.ru/xmlui/handle/net/136258
dc.description.abstract	A problem of modification of the classical airfoils that ensure the absence of separation in a subsonic ideal-gas flow in a specified range of angles of attack is solved by a numerical-analytical method based on the quasi-solution of inverse boundary-value problems of aerohydrodynamics and Kármán-Jiang formulas. Loitsyanskii's criterion of the non-separated flow is used to determine the boundary-layer separation point. © MAIK/Nauka 2008.
dc.relation.ispartofseries	Journal of Applied Mechanics and Technical Physics
dc.subject	Allowance for compressibility
dc.subject	Inverse boundary-layer problem of aerohydrodynamics
dc.subject	Method of quasi-solutions
dc.subject	Non-separated flow
dc.title	Design of airfoils providing the absence of separation in a compressible flow in a specified range of angles of attack
dc.type	Article
dc.relation.ispartofseries-issue	6
dc.relation.ispartofseries-volume	49
dc.collection	Публикации сотрудников КФУ
dc.relation.startpage	971
dc.source.id	SCOPUS00218944-2008-49-6-SID56749165149

Файлы в этом документе

Размер: 44.02Kb

Формат: PDF

Публикации сотрудников КФУ Scopus [24551]
Коллекция содержит публикации сотрудников Казанского федерального (до 2010 года Казанского государственного) университета, проиндексированные в БД Scopus, начиная с 1970г.