Разработка программного комплекса для расчета течений продуктов сгорания в проточном тракте РДТТ с учетом изменения геометрии наполнителя
In the present study calculations algorithm of gas flow in solid-fuel rocket engine are shown. The algorithm is based on the solution of two-dimensional gas dynamics equations. Calculations are done for solidfuel rocket engine model which consists of combustion chamber and nozzle. The results in ag...
| Published in: | Перспективы развития фундаментальных наук. Т. 3 : сборник научных трудов XVI Международной конференции студентов, аспирантов и молодых ученых, 23-26 апреля 2019 г. Т. 3 : Математика. С. 71-73 |
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| Main Author: | |
| Other Authors: | , |
| Format: | Book Chapter |
| Language: | Russian |
| Subjects: | |
| Online Access: | http://vital.lib.tsu.ru/vital/access/manager/Repository/vtls:000787459 Перейти в каталог НБ ТГУ |
| Summary: | In the present study calculations algorithm of gas flow in solid-fuel rocket engine are shown. The algorithm is based on the solution of two-dimensional gas dynamics equations. Calculations are done for solidfuel rocket engine model which consists of combustion chamber and nozzle. The results in agreement with known solutions. |
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| Bibliography: | Библиогр.: 6 назв. |
| ISBN: | 9785438708858 9785438708827 |