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dc.contributor.authorСемкин, Е.В.
dc.date2016
dc.date.accessioned2025-08-22T12:21:34Z-
dc.date.available2025-08-22T12:21:34Z-
dc.date.issued2016
dc.identifier.identifierDspace\SGAU\20161107\59571
dc.identifier.citationМатериалы докладов междунар. науч.-техн. конф. 22-24 июня 2016 г. Ч. 2, с. 59
dc.identifier.isbn978-5-7883-1084-8
dc.identifier.urihttp://repo.ssau.ru/jspui/handle/123456789/14606-
dc.descriptionУДК 621.454.2-181.4:621.43.038.8
dc.description.abstractThis paper describes simulation results of working liquid (water) flow from centrifugal nozzle in the hydraulic duct of 13,34 N liquid propellant thruster into air at atmospheric pressure. Has been presented results of flow simulation for single oxidizer nozzle and single fuel nozzle and mixing elements of coaxial centrifugal nozzles. Has been used double-speed and one-speed models of two-phase liquid flow. Menter models (SST, BSL) and Wilcox model (k-w) are used as turbulence models. The calculation results has been compared with hydraulic test results.
dc.languagerus
dc.publisherСамарский университет
dc.titleИсследование процессов истечения жидкости из малорасходных центробежных форсунок ЖРДМТ тягой 13,34 Н
dc.title.alternativeScientific research of liquid flow process from low consumption centrifugal nozzles of 13,34 N liquid propellant thruster
dc.typeArticle
local.identifier.oldurihttp://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Issledovanie-processov-istecheniya-zhidkosti-iz-malorashodnyh-centrobezhnyh-forsunok-ZhRDMT-tyagoi-1334-N-59571
local.identifier.oldurihttp://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Issledovanie-processov-istecheniya-zhidkosti-iz-malorashodnyh-centrobezhnyh-forsunok-ZhRDMT-tyagoi-1334-N-59571
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