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dc.contributor.authorСабирзянов, А.Н.
dc.contributor.authorКириллова, А.Н.
dc.date2016
dc.date.accessioned2025-08-22T12:21:32Z-
dc.date.available2025-08-22T12:21:32Z-
dc.date.issued2016
dc.identifier.identifierDspace\SGAU\20161103\59529
dc.identifier.citationМатериалы докладов междунар. науч.-техн. конф. 22-24 июня 2016 г. Ч. 2, с. 39-40
dc.identifier.isbn978-5-7883-1084-8
dc.identifier.urihttp://repo.ssau.ru/jspui/handle/123456789/14577-
dc.descriptionУДК 621.45.02+536.8+519.6
dc.description.abstractMultiparameter research of dependence of aircraft engine nozzle discharge coefficient on its geometrical parameters has been conducted using advanced CFD methods. Characteristic influence of a contour of supersonic section of the nozzle and its cylindrical section of the throat on nozzle discharge coefficient has been shown.
dc.languagerus
dc.publisherСамарский университет
dc.titleЧисленное моделирование влияния геометрических параметров сопла на коэффициент расхода ДЛА
dc.title.alternativeThe numerical simulation of the influence of nozzle's geometrical parameters on aircraft engines' discharge coefficient
dc.typeArticle
local.identifier.oldurihttp://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Chislennoe-modelirovanie-vliyaniya-geometricheskih-parametrov-sopla-na-koefficient-rashoda-DLA-59529
local.identifier.oldurihttp://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Chislennoe-modelirovanie-vliyaniya-geometricheskih-parametrov-sopla-na-koefficient-rashoda-DLA-59529
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