A mathematical model of metallized solid propellant combustion under the changing pressure
This paper presents the mathematical model describing a non-stationary combustion of metallized solid propellant. The model takes into account the heat transfer, the oxidizer decomposition and gasification of the solid propellant, two-phase, dual-velocity, two-temperature reactant flow over the prop...
| Опубликовано в: : | MATEC Web of conferences Vol. 115. P. 03001 (1-5) |
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| Главный автор: | |
| Формат: | Статья в журнале |
| Язык: | English |
| Предметы: | |
| Online-ссылка: | http://vital.lib.tsu.ru/vital/access/manager/Repository/vtls:000618230 Перейти в каталог НБ ТГУ |