Fluid Dynamics of Thrust Vectorable Submerged Nozzle
A numerical simulation of the gas-dynamic processes in the thrust vectorable nozzle of the solid rocket motor is considered. Construction of a geometric model and a generation of computational mesh, and reconstruction of model and mesh at each time step are discussed. Calculations of the flowfield o...
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| Автори: | , , |
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| Формат: | Artigo |
| Мова: | Inglês |
| Опубліковано: |
MDPI AG
2021-08-01
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| Серія: | Fluids |
| Предмети: | |
| Онлайн доступ: | https://www.mdpi.com/2311-5521/6/8/278 |
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