A method for constructing an airfoil using a specified chord velocity diagram

dc.contributor.author	Salimov R.
dc.contributor.author	Labutkin A.
dc.date.accessioned	2018-09-18T20:18:03Z
dc.date.available	2018-09-18T20:18:03Z
dc.date.issued	2009
dc.identifier.issn	1068-7998
dc.identifier.uri	https://dspace.kpfu.ru/xmlui/handle/net/138468
dc.description.abstract	A problem of determining a shape of the airfoil being streamlined by a potential incompressible inviscid flow is solved by the successive approximation method using a specified chord velocity diagram. It is shown that a closed airfoil that possesses a specified chord velocity diagram can be constructed with a sufficient accuracy; if the chord diagram is unsuccessfully specified, the closed airfoil may prove to be not univalent, that is, physically unrealizable. © 2009 Allerton Press, Inc.
dc.relation.ispartofseries	Russian Aeronautics
dc.subject	Airfoil
dc.subject	Chord diagram
dc.subject	Flow velocity
dc.title	A method for constructing an airfoil using a specified chord velocity diagram
dc.type	Article
dc.relation.ispartofseries-issue	4
dc.relation.ispartofseries-volume	52
dc.collection	Публикации сотрудников КФУ
dc.relation.startpage	408
dc.source.id	SCOPUS10687998-2009-52-4-SID76449087323

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