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dc.contributor.authorАлексеев, Р.А.
dc.contributor.authorСидоров, А.С.
dc.date2016
dc.date.accessioned2025-08-22T12:21:33Z-
dc.date.available2025-08-22T12:21:33Z-
dc.date.issued2016
dc.identifier.identifierDspace\SGAU\20161118\59924
dc.identifier.citationМатериалы докладов междунар. науч.-техн. конф. 22-24 июня 2016 г. Ч. 1, с. 106-108
dc.identifier.isbn978-5-7883-1084-8
dc.identifier.urihttp://repo.ssau.ru/jspui/handle/123456789/14599-
dc.descriptionУДК 621.438-226.2.048
dc.description.abstractExhaust diffuser of medium gas turbine engine with a high swirling flow at the exit of the low pressure turbine (LPT) is investigated. Authors propose a design of LPT exhaust diffuser in which the swirling gas flow straightening and mixing with air from fan duct at the same time. Comparison between nozzles with original and new exhaust diffusers showed that thrust increased by 2.2% in second case.
dc.languagerus
dc.publisherСамарский университет
dc.titleПроектирование затурбинного устройства среднеразмерного двигателя
dc.title.alternativeDevelopment of exhaust diffuser for medium gas turbine engine
dc.typeArticle
local.identifier.oldurihttp://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Proektirovanie-zaturbinnogo-ustroistva-srednerazmernogo-dvigatelya-59924
local.identifier.oldurihttp://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Proektirovanie-zaturbinnogo-ustroistva-srednerazmernogo-dvigatelya-59924
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