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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Format: | Article |
Language: | English |
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MDPI AG
2021-08-01
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Series: | Fluids |
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Online Access: | https://www.mdpi.com/2311-5521/6/8/278 |
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author | Sergey Denisikhin Vladislav Emelyanov Konstantin Volkov |
author_facet | Sergey Denisikhin Vladislav Emelyanov Konstantin Volkov |
author_sort | Sergey Denisikhin |
collection | DOAJ |
description | 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 of combustion products in the pre-nozzle chamber and nozzle block are carried out for various angles of nozzle rotation. The distributions of the gas dynamic quantities in the pre-nozzle volume corresponding to the outflow of the combustion products from the cylindrical channel and star-shaped channel are compared, as well as the solutions of the problem obtained with quasi-stationary and unsteady formulations. The effects of the channel shape on the distribution of flow quantities and formation of a vortical flow structure in the nozzle block are discussed. |
first_indexed | 2024-03-10T08:49:24Z |
format | Article |
id | doaj.art-14ee3c3bf7bf4fc5adadba2465b2c363 |
institution | Directory Open Access Journal |
issn | 2311-5521 |
language | English |
last_indexed | 2024-03-10T08:49:24Z |
publishDate | 2021-08-01 |
publisher | MDPI AG |
record_format | Article |
series | Fluids |
spelling | doaj.art-14ee3c3bf7bf4fc5adadba2465b2c3632023-11-22T07:36:52ZengMDPI AGFluids2311-55212021-08-016827810.3390/fluids6080278Fluid Dynamics of Thrust Vectorable Submerged NozzleSergey Denisikhin0Vladislav Emelyanov1Konstantin Volkov2Faculty of Aerospace Engineering, Baltic State Technical University, 190005 St. Petersburg, RussiaFaculty of Aerospace Engineering, Baltic State Technical University, 190005 St. Petersburg, RussiaInstitute of Hydrodynamics and Control Processes, St. Petersburg State Marine Technical University, 190121 St. Petersburg, RussiaA 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 of combustion products in the pre-nozzle chamber and nozzle block are carried out for various angles of nozzle rotation. The distributions of the gas dynamic quantities in the pre-nozzle volume corresponding to the outflow of the combustion products from the cylindrical channel and star-shaped channel are compared, as well as the solutions of the problem obtained with quasi-stationary and unsteady formulations. The effects of the channel shape on the distribution of flow quantities and formation of a vortical flow structure in the nozzle block are discussed.https://www.mdpi.com/2311-5521/6/8/278solid rocket motorthrustvectorable nozzlesubmerged nozzlenumerical simulationvortical structure |
spellingShingle | Sergey Denisikhin Vladislav Emelyanov Konstantin Volkov Fluid Dynamics of Thrust Vectorable Submerged Nozzle Fluids solid rocket motor thrust vectorable nozzle submerged nozzle numerical simulation vortical structure |
title | Fluid Dynamics of Thrust Vectorable Submerged Nozzle |
title_full | Fluid Dynamics of Thrust Vectorable Submerged Nozzle |
title_fullStr | Fluid Dynamics of Thrust Vectorable Submerged Nozzle |
title_full_unstemmed | Fluid Dynamics of Thrust Vectorable Submerged Nozzle |
title_short | Fluid Dynamics of Thrust Vectorable Submerged Nozzle |
title_sort | fluid dynamics of thrust vectorable submerged nozzle |
topic | solid rocket motor thrust vectorable nozzle submerged nozzle numerical simulation vortical structure |
url | https://www.mdpi.com/2311-5521/6/8/278 |
work_keys_str_mv | AT sergeydenisikhin fluiddynamicsofthrustvectorablesubmergednozzle AT vladislavemelyanov fluiddynamicsofthrustvectorablesubmergednozzle AT konstantinvolkov fluiddynamicsofthrustvectorablesubmergednozzle |