Algorithm of calculating the light airplane flight performance and rational design airscrew parameters at the preliminary design stage

dc.contributor.author	Gainutdinova T.
dc.contributor.author	Gainutdinova A.
dc.date.accessioned	2018-09-19T20:59:28Z
dc.date.available	2018-09-19T20:59:28Z
dc.date.issued	2016
dc.identifier.issn	1068-7998
dc.identifier.uri	https://dspace.kpfu.ru/xmlui/handle/net/143488
dc.description.abstract	© 2016, Allerton Press, Inc.A technique is proposed of calculating the characteristic flight velocities for an airplane with taking into account the nominal performance of a piston engine. We consider an algorithm of design calculation for the airscrew blade geometry (twist angle, chord and optimal angle of attack along blade). Feasible rational versions of design parameters are discussed.
dc.relation.ispartofseries	Russian Aeronautics
dc.subject	airscrew
dc.subject	algorithms
dc.subject	flight performance
dc.title	Algorithm of calculating the light airplane flight performance and rational design airscrew parameters at the preliminary design stage
dc.type	Article
dc.relation.ispartofseries-issue	3
dc.relation.ispartofseries-volume	59
dc.collection	Публикации сотрудников КФУ
dc.relation.startpage	364
dc.source.id	SCOPUS10687998-2016-59-3-SID85007346538

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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.