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dc.contributor.authorЗаваркин, В.Н.
dc.contributor.authorКарпов, Ф.В.
dc.contributor.authorЛаршин, Д.И.
dc.contributor.authorНемтырева, И.А.
dc.date2016
dc.date.accessioned2025-08-22T12:22:09Z-
dc.date.available2025-08-22T12:22:09Z-
dc.date.issued2016
dc.identifier.identifierDspace\SGAU\20161117\59861
dc.identifier.citationМатериалы докладов междунар. науч.-техн. конф. 22-24 июня 2016 г. Ч. 1, с. 25-27
dc.identifier.isbn978-5-7883-1084-8
dc.identifier.urihttp://repo.ssau.ru/jspui/handle/123456789/14510-
dc.descriptionУДК 621.438
dc.description.abstractCurrently NPO Saturn is facing a problem of the GTD-110 stage 1 blade failure in the root area, which supposedly has been caused by excitations in the harmonics multiple of the number of nozzle vanes. A series of actions has been developed to solve this problem. One of them is change a number the nozzle vane second stage.
dc.languagerus
dc.publisherСамарский университет
dc.titleНестационарный газодинамический расчёт второй ступени турбины ГТД-110М с неравномерной расстановкой лопаток в сопловом аппарате
dc.title.alternativeTransient fluid dynamic analysis of flowing in second stage of turbine GTD-110M with irregular spacing of vanes in nozzle
dc.typeArticle
local.identifier.oldurihttp://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Nestacionarnyi-gazodinamicheskii-raschet-vtoroi-stupeni-turbiny-GTD110M-s-neravnomernoi-rasstanovkoi-lopatok-v-soplovom-apparate-59861
local.identifier.oldurihttp://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Nestacionarnyi-gazodinamicheskii-raschet-vtoroi-stupeni-turbiny-GTD110M-s-neravnomernoi-rasstanovkoi-lopatok-v-soplovom-apparate-59861
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