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dc.contributor.authorДиденко, А.А.
dc.contributor.authorАбрашкин, В.Ю.
dc.contributor.authorСоколов, А.Б.
dc.contributor.authorЧечет, И.В.
dc.contributor.authorМишенков, С.Ю.
dc.contributor.authorАхтеряков, А.В.
dc.date2016
dc.date.accessioned2025-08-22T12:22:02Z-
dc.date.available2025-08-22T12:22:02Z-
dc.date.issued2016
dc.identifier.identifierDspace\SGAU\20161114\59775
dc.identifier.citationМатериалы докладов междунар. науч.-техн. конф. 22-24 июня 2016 г. Ч. 2, с. 192-193
dc.identifier.isbn978-5-7883-1084-8
dc.identifier.urihttp://repo.ssau.ru/jspui/handle/123456789/14536-
dc.descriptionУДК 621.45.022:535.3
dc.description.abstractHas been achieved a detailed study of fields in the gas flow rate using a three-component laser dopler anemometer 3D-LDA LAD-056S and the characteristics of the composition and temperature of the gas at the outlet of the GTE tubular combustion chamber. Fields of gas temperature are measured by point thermocouple. Sampling to determine the chemical composition has been carried out by a single point and integrated sampler. The measurements have been carried out in the SSAU scientific and educational center of the gas dynamic research.
dc.languagerus
dc.publisherСамарский университет
dc.titleИсследование неравномерности потока газа на выходе из камеры сгорания газотурбинного двигателя по измерениям температуры, химического состава и лазерным измерениям скорости
dc.title.alternativeAnalysis of unsteady flow in the GTE combustion chamber outlet by measuring temperature, chemical composition and laser speed measurement
dc.typeArticle
local.identifier.oldurihttp://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Issledovanie-neravnomernosti-potoka-gaza-na-vyhode-iz-kamery-sgoraniya-gazoturbinnogo-dvigatelya-59775
local.identifier.oldurihttp://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Issledovanie-neravnomernosti-potoka-gaza-na-vyhode-iz-kamery-sgoraniya-gazoturbinnogo-dvigatelya-59775
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