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dc.contributor.authorУрлапкин, А.В.
dc.contributor.authorЕрмаков, А.И.
dc.date2016
dc.date.accessioned2025-08-22T12:22:05Z-
dc.date.available2025-08-22T12:22:05Z-
dc.date.issued2016
dc.identifier.identifierDspace\SGAU\20161109\59684
dc.identifier.citationМатериалы докладов междунар. науч.-техн. конф. 22-24 июня 2016 г. Ч. 2, с. 89-90
dc.identifier.isbn978-5-7883-1084-8
dc.identifier.urihttp://repo.ssau.ru/jspui/handle/123456789/14780-
dc.descriptionУДК 621.45.026.8; 533.662.3
dc.description.abstractThe shows the development of a calculation model to account the aerodynamic damping and connectedness of blade forced vibrations. Has been solved the problem of aeroelasticity in the case of plane blades vibrations. Has been proposed a method for replacing the aeroelastic problem by the gas-dynamic calculation of an equivalent mechanical system. Main laws of aeroelastic vibrations are identified.
dc.languagerus
dc.publisherСамарский университет
dc.titleРазработка модели учёта аэродинамической связанности и демпфирования при колебаниях лопаток
dc.title.alternativeDevelopment of aerodynamic connectedness and damping accounting model for blade vibrations
dc.typeArticle
local.identifier.oldurihttp://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Razrabotka-modeli-ucheta-aerodinamicheskoi-svyazannosti-i-dempfirovaniya-pri-kolebaniyah-lopatok-59684
local.identifier.oldurihttp://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Razrabotka-modeli-ucheta-aerodinamicheskoi-svyazannosti-i-dempfirovaniya-pri-kolebaniyah-lopatok-59684
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