Numerical simulation of the unsteady combustion of solid rocket propellants at a harmonic pressure change
This study focuses on a numerical investigation of the unsteady burning rate of solid propellants at a harmonic pressure change in the combustion chamber of a solid propellant rocket engine. The physico-mathematical model includes the equations of heat transfer and decomposition of the oxidizer in...
| Published in: | Journal of mechanical science and technology Vol. 34, № 1. P. 489-497 |
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| Main Author: | |
| Other Authors: | , |
| Format: | Article |
| Language: | English |
| Subjects: | |
| Online Access: | http://vital.lib.tsu.ru/vital/access/manager/Repository/vtls:000794758 Перейти в каталог НБ ТГУ |