Method of gas flows calculation in solid propellant rocket engines taking into account the combustion of solid fuel charge
The paper presents a method for calculating the local and integral characteristics of the flow in the axisymmetric gas-dynamic paths of solid propellant rocket motors, taking into account the combustion of a charge of solid fuel. The numerical method of calculation is based on the use of the Godunov...
| Published in: | IOP Conference Series: Materials Science and Engineering Vol. 597. P. 012077 (1-6) |
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| Other Authors: | , , , , , , |
| Format: | Article |
| Language: | English |
| Subjects: | |
| Online Access: | http://vital.lib.tsu.ru/vital/access/manager/Repository/vtls:000673871 Перейти в каталог НБ ТГУ |