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

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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.

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