A novel strategy for comprehensive optimization of structural and operational parameters in a supersonic separator using computational fluid dynamics modeling

Abstract In this study, the effects of several structural and operational parameters affecting the separation efficiency of supersonic separators were investigated by numerical methods. Different turbulence models were used and their accuracies were evaluated. Based on the error analysis, the V2-f t...

Descripción completa

Guardado en:
Detalles Bibliográficos
Autores principales: Sina Nabati Shoghl, Abbas Naderifar, Fatola Farhadi, Gholamreza Pazuki
Formato: article
Lenguaje:EN
Publicado: Nature Portfolio 2021
Materias:
R
Q
Acceso en línea:https://doaj.org/article/c653c07b966a4fadab4ac5f56c96054a
Etiquetas: Agregar Etiqueta
Sin Etiquetas, Sea el primero en etiquetar este registro!
id oai:doaj.org-article:c653c07b966a4fadab4ac5f56c96054a
record_format dspace
spelling oai:doaj.org-article:c653c07b966a4fadab4ac5f56c96054a2021-11-14T12:19:13ZA novel strategy for comprehensive optimization of structural and operational parameters in a supersonic separator using computational fluid dynamics modeling10.1038/s41598-021-01303-52045-2322https://doaj.org/article/c653c07b966a4fadab4ac5f56c96054a2021-11-01T00:00:00Zhttps://doi.org/10.1038/s41598-021-01303-5https://doaj.org/toc/2045-2322Abstract In this study, the effects of several structural and operational parameters affecting the separation efficiency of supersonic separators were investigated by numerical methods. Different turbulence models were used and their accuracies were evaluated. Based on the error analysis, the V2-f turbulence model was more accurate for describing the high swirling turbulent flow than other investigated turbulence models. Therefore, the V2-f turbulence model and particle tracing model were selected to optimize the structure of the convergence part, the diffuser, the drainage port, and the swirler. The cooling performance of three line-type in the convergent section were calculated. The simulation results demonstrated that the convergent section designed by the Witoszynski curve had higher cooling depth compared to the Bi-cubic and Quintic curves. Furthermore, the expansion angle of 2° resulted in the highest stability of fluid flow and therefore was selected in the design of the diffuser. The effect of incorporating the swirler and its structure on the separation performance of supersonic separator was also studied. Three different swirler types, including axial, wall-mounted, and helical, were investigated. It was observed that installing the swirler significantly improved the separation efficiency of the supersonic separator. In addition, the simulation results demonstrated that the separation efficiency was higher for the axial swirler compared to the wall-mounted and helical swirlers. Therefore, for the improved nozzle, the swirling flow was generated by the axial swirler. The optimized axial swirler was constructed from 12 arced vanes each of which had a swirl angle of 40°. For the optimized structure, the effects of operating parameters such as inlet temperature, pressure recovery ratio, density, and droplet size was also investigated. It was concluded that increasing the droplet size and density significantly improved the separation efficiency of the supersonic separator. For hydrocarbon droplets, the separation efficiency improved from 4.6 to 76.7% upon increasing the droplet size from 0.1 to 2 µm.Sina Nabati ShoghlAbbas NaderifarFatola FarhadiGholamreza PazukiNature PortfolioarticleMedicineRScienceQENScientific Reports, Vol 11, Iss 1, Pp 1-25 (2021)
institution DOAJ
collection DOAJ
language EN
topic Medicine
R
Science
Q
spellingShingle Medicine
R
Science
Q
Sina Nabati Shoghl
Abbas Naderifar
Fatola Farhadi
Gholamreza Pazuki
A novel strategy for comprehensive optimization of structural and operational parameters in a supersonic separator using computational fluid dynamics modeling
description Abstract In this study, the effects of several structural and operational parameters affecting the separation efficiency of supersonic separators were investigated by numerical methods. Different turbulence models were used and their accuracies were evaluated. Based on the error analysis, the V2-f turbulence model was more accurate for describing the high swirling turbulent flow than other investigated turbulence models. Therefore, the V2-f turbulence model and particle tracing model were selected to optimize the structure of the convergence part, the diffuser, the drainage port, and the swirler. The cooling performance of three line-type in the convergent section were calculated. The simulation results demonstrated that the convergent section designed by the Witoszynski curve had higher cooling depth compared to the Bi-cubic and Quintic curves. Furthermore, the expansion angle of 2° resulted in the highest stability of fluid flow and therefore was selected in the design of the diffuser. The effect of incorporating the swirler and its structure on the separation performance of supersonic separator was also studied. Three different swirler types, including axial, wall-mounted, and helical, were investigated. It was observed that installing the swirler significantly improved the separation efficiency of the supersonic separator. In addition, the simulation results demonstrated that the separation efficiency was higher for the axial swirler compared to the wall-mounted and helical swirlers. Therefore, for the improved nozzle, the swirling flow was generated by the axial swirler. The optimized axial swirler was constructed from 12 arced vanes each of which had a swirl angle of 40°. For the optimized structure, the effects of operating parameters such as inlet temperature, pressure recovery ratio, density, and droplet size was also investigated. It was concluded that increasing the droplet size and density significantly improved the separation efficiency of the supersonic separator. For hydrocarbon droplets, the separation efficiency improved from 4.6 to 76.7% upon increasing the droplet size from 0.1 to 2 µm.
format article
author Sina Nabati Shoghl
Abbas Naderifar
Fatola Farhadi
Gholamreza Pazuki
author_facet Sina Nabati Shoghl
Abbas Naderifar
Fatola Farhadi
Gholamreza Pazuki
author_sort Sina Nabati Shoghl
title A novel strategy for comprehensive optimization of structural and operational parameters in a supersonic separator using computational fluid dynamics modeling
title_short A novel strategy for comprehensive optimization of structural and operational parameters in a supersonic separator using computational fluid dynamics modeling
title_full A novel strategy for comprehensive optimization of structural and operational parameters in a supersonic separator using computational fluid dynamics modeling
title_fullStr A novel strategy for comprehensive optimization of structural and operational parameters in a supersonic separator using computational fluid dynamics modeling
title_full_unstemmed A novel strategy for comprehensive optimization of structural and operational parameters in a supersonic separator using computational fluid dynamics modeling
title_sort novel strategy for comprehensive optimization of structural and operational parameters in a supersonic separator using computational fluid dynamics modeling
publisher Nature Portfolio
publishDate 2021
url https://doaj.org/article/c653c07b966a4fadab4ac5f56c96054a
work_keys_str_mv AT sinanabatishoghl anovelstrategyforcomprehensiveoptimizationofstructuralandoperationalparametersinasupersonicseparatorusingcomputationalfluiddynamicsmodeling
AT abbasnaderifar anovelstrategyforcomprehensiveoptimizationofstructuralandoperationalparametersinasupersonicseparatorusingcomputationalfluiddynamicsmodeling
AT fatolafarhadi anovelstrategyforcomprehensiveoptimizationofstructuralandoperationalparametersinasupersonicseparatorusingcomputationalfluiddynamicsmodeling
AT gholamrezapazuki anovelstrategyforcomprehensiveoptimizationofstructuralandoperationalparametersinasupersonicseparatorusingcomputationalfluiddynamicsmodeling
AT sinanabatishoghl novelstrategyforcomprehensiveoptimizationofstructuralandoperationalparametersinasupersonicseparatorusingcomputationalfluiddynamicsmodeling
AT abbasnaderifar novelstrategyforcomprehensiveoptimizationofstructuralandoperationalparametersinasupersonicseparatorusingcomputationalfluiddynamicsmodeling
AT fatolafarhadi novelstrategyforcomprehensiveoptimizationofstructuralandoperationalparametersinasupersonicseparatorusingcomputationalfluiddynamicsmodeling
AT gholamrezapazuki novelstrategyforcomprehensiveoptimizationofstructuralandoperationalparametersinasupersonicseparatorusingcomputationalfluiddynamicsmodeling
_version_ 1718429314015297536