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dc.contributor.authorЗубанов, Д.В.
dc.contributor.authorСтепанов, Д.В.
dc.contributor.authorШаблий, Л.С.
dc.date2016
dc.date.accessioned2025-08-22T12:22:10Z-
dc.date.available2025-08-22T12:22:10Z-
dc.date.issued2016
dc.identifier.identifierDspace\SGAU\20161114\59744
dc.identifier.citationМатериалы докладов междунар. науч.-техн. конф. 22-24 июня 2016 г. Ч. 2, с. 173-175
dc.identifier.isbn978-5-7883-1084-8
dc.identifier.urihttp://repo.ssau.ru/jspui/handle/123456789/14518-
dc.descriptionУДК 621.454.2
dc.description.abstractHas been described method to simulate the transient ignition processes in the rocket engine operating on gaseous hydrogen and oxygen. Have been considered features of the method and its relevance to tasks with transient ignition simulation. Has been given the description of used software tools. Has been described the chemical reaction system. Has been given the way of estimating the chemical reaction system from the physical process point of view.
dc.languagerus
dc.publisherСамарский университет
dc.titleМетодика моделирования нестационарных процессов зажигания ракетного двигателя на газообразном топливе кислород и водород
dc.title.alternativeTransient ignition processes simulation of the rocket engine operating on gaseous hydrogen and oxygen
dc.typeArticle
local.identifier.oldurihttp://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Metodika-modelirovaniya-nestacionarnyh-processov-zazhiganiya-raketnogo-dvigatelya-na-gazoobraznom-toplive-kislorod-i-vodorod-59744
local.identifier.oldurihttp://repo.ssau.ru/handle/Mezhdunarodnaya-nauchnotehnicheskaya-konferenciya-Problemy-i-perspektivy-razvitiya-dvigatelestroeniya/Metodika-modelirovaniya-nestacionarnyh-processov-zazhiganiya-raketnogo-dvigatelya-na-gazoobraznom-toplive-kislorod-i-vodorod-59744
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