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dc.contributor.authorШаблий, Л.С.
dc.contributor.authorЗубанов, В.М.
dc.contributor.authorСтепанов, Д.В.
dc.date2016
dc.date.accessioned2025-08-22T12:22:05Z-
dc.date.available2025-08-22T12:22:05Z-
dc.date.issued2016
dc.identifier.identifierDspace\SGAU\20161109\59687
dc.identifier.citationМатериалы докладов междунар. науч.-техн. конф. 22-24 июня 2016 г. Ч. 2, с. 95-96
dc.identifier.isbn978-5-7883-1084-8
dc.identifier.urihttp://repo.ssau.ru/jspui/handle/123456789/14824-
dc.descriptionУДК 621.454.2
dc.description.abstractA work presents methods for simulation of burning process in the rocket engine chamber. Has been mentioned four software tools for burning simulation. Here are considered widely used burning models. The detailed calculation of hydrogen-oxygen rocket engine chamber has been performed in ANSYS CFX with Eddy Dissipation model for two sets of chemistry: one global reaction and detailed chemical system with 8 components and 18 reactions. The comparison of results gives more smooth contours of parameters for set with detailed system against variant with one reaction.
dc.languagerus
dc.publisherСамарский университет
dc.titleМетодики моделирования процессов горения в камере ракетного двигателя
dc.title.alternativeSimulation methods of a burning process inside a rocket engine chamber
dc.typeArticle
local.identifier.oldurihttp://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Metodiki-modelirovaniya-processov-goreniya-v-kamere-raketnogo-dvigatelya-59687
local.identifier.oldurihttp://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Metodiki-modelirovaniya-processov-goreniya-v-kamere-raketnogo-dvigatelya-59687
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