Numerical study of gas mixture separation in curved nozzles
- Autores
- Guozden, Tomas Manuel; Clausse, Alejandro
- Año de publicación
- 2016
- Idioma
- inglés
- Tipo de recurso
- artículo
- Estado
- versión publicada
- Descripción
- Species separation can be produced by imposing a pressure gradient in gaseous mixtures, which induces different molecular velocities depending on the molar weight. Pressure gradients can be achieved by centrifugal forces brought about by the passage of the gas through a curved nozzle at supersonic velocity. The efficiency of this process depends on the geometry of the nozzle as well as the flow operating conditions. The numerical solver Fluent was used in order to produce a model of the aerodynamics and the oxygen diffusion of a steady-state flow of air in a curved nozzle. The development of the pressure and O2 concentration profiles along the nozzle were analyzed for different pressure boundary conditions at the inlet and the exit, testing several nozzle sizes. Optimum values of the cut and the inlet pressure were found which maximize the separation efficiency. The effect of the exit pressure was associated with the axial pressure distribution along the inner wall of the nozzle. The results were compared with measurements showing good agreement.
Fil: Guozden, Tomas Manuel. Comisión Nacional de Energía Atómica. Gerencia del Área de Energía Nuclear. Instituto Balseiro; Argentina. Consejo Nacional de Investigaciones Científicas y Técnicas; Argentina
Fil: Clausse, Alejandro. Comisión Nacional de Energía Atómica; Argentina. Universidad Nacional del Centro de la Provincia de Buenos Aires; Argentina. Consejo Nacional de Investigaciones Científicas y Técnicas; Argentina - Materia
-
Curved Nozzle
Separative Capacity
Species Separation
Supersonic Flow - Nivel de accesibilidad
- acceso abierto
- Condiciones de uso
- https://creativecommons.org/licenses/by-nc-nd/2.5/ar/
- Repositorio
.jpg)
- Institución
- Consejo Nacional de Investigaciones Científicas y Técnicas
- OAI Identificador
- oai:ri.conicet.gov.ar:11336/58704
Ver los metadatos del registro completo
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Numerical study of gas mixture separation in curved nozzlesGuozden, Tomas ManuelClausse, AlejandroCurved NozzleSeparative CapacitySpecies SeparationSupersonic Flowhttps://purl.org/becyt/ford/2.3https://purl.org/becyt/ford/2Species separation can be produced by imposing a pressure gradient in gaseous mixtures, which induces different molecular velocities depending on the molar weight. Pressure gradients can be achieved by centrifugal forces brought about by the passage of the gas through a curved nozzle at supersonic velocity. The efficiency of this process depends on the geometry of the nozzle as well as the flow operating conditions. The numerical solver Fluent was used in order to produce a model of the aerodynamics and the oxygen diffusion of a steady-state flow of air in a curved nozzle. The development of the pressure and O2 concentration profiles along the nozzle were analyzed for different pressure boundary conditions at the inlet and the exit, testing several nozzle sizes. Optimum values of the cut and the inlet pressure were found which maximize the separation efficiency. The effect of the exit pressure was associated with the axial pressure distribution along the inner wall of the nozzle. The results were compared with measurements showing good agreement.Fil: Guozden, Tomas Manuel. Comisión Nacional de Energía Atómica. Gerencia del Área de Energía Nuclear. Instituto Balseiro; Argentina. Consejo Nacional de Investigaciones Científicas y Técnicas; ArgentinaFil: Clausse, Alejandro. Comisión Nacional de Energía Atómica; Argentina. Universidad Nacional del Centro de la Provincia de Buenos Aires; Argentina. Consejo Nacional de Investigaciones Científicas y Técnicas; ArgentinaPergamon-Elsevier Science Ltd2016-07info:eu-repo/semantics/articleinfo:eu-repo/semantics/publishedVersionhttp://purl.org/coar/resource_type/c_6501info:ar-repo/semantics/articuloapplication/pdfapplication/pdfhttp://hdl.handle.net/11336/58704Guozden, Tomas Manuel; Clausse, Alejandro; Numerical study of gas mixture separation in curved nozzles; Pergamon-Elsevier Science Ltd; International Journal Of Heat And Mass Transfer; 98; 7-2016; 176-1820017-9310CONICET DigitalCONICETenginfo:eu-repo/semantics/altIdentifier/doi/10.1016/j.ijheatmasstransfer.2016.03.015info:eu-repo/semantics/altIdentifier/url/https://www.sciencedirect.com/science/article/pii/S0017931015313004info:eu-repo/semantics/openAccesshttps://creativecommons.org/licenses/by-nc-nd/2.5/ar/reponame:CONICET Digital (CONICET)instname:Consejo Nacional de Investigaciones Científicas y Técnicas2025-11-05T10:50:44Zoai:ri.conicet.gov.ar:11336/58704instacron:CONICETInstitucionalhttp://ri.conicet.gov.ar/Organismo científico-tecnológicoNo correspondehttp://ri.conicet.gov.ar/oai/requestdasensio@conicet.gov.ar; lcarlino@conicet.gov.arArgentinaNo correspondeNo correspondeNo correspondeopendoar:34982025-11-05 10:50:45.184CONICET Digital (CONICET) - Consejo Nacional de Investigaciones Científicas y Técnicasfalse |
| dc.title.none.fl_str_mv |
Numerical study of gas mixture separation in curved nozzles |
| title |
Numerical study of gas mixture separation in curved nozzles |
| spellingShingle |
Numerical study of gas mixture separation in curved nozzles Guozden, Tomas Manuel Curved Nozzle Separative Capacity Species Separation Supersonic Flow |
| title_short |
Numerical study of gas mixture separation in curved nozzles |
| title_full |
Numerical study of gas mixture separation in curved nozzles |
| title_fullStr |
Numerical study of gas mixture separation in curved nozzles |
| title_full_unstemmed |
Numerical study of gas mixture separation in curved nozzles |
| title_sort |
Numerical study of gas mixture separation in curved nozzles |
| dc.creator.none.fl_str_mv |
Guozden, Tomas Manuel Clausse, Alejandro |
| author |
Guozden, Tomas Manuel |
| author_facet |
Guozden, Tomas Manuel Clausse, Alejandro |
| author_role |
author |
| author2 |
Clausse, Alejandro |
| author2_role |
author |
| dc.subject.none.fl_str_mv |
Curved Nozzle Separative Capacity Species Separation Supersonic Flow |
| topic |
Curved Nozzle Separative Capacity Species Separation Supersonic Flow |
| purl_subject.fl_str_mv |
https://purl.org/becyt/ford/2.3 https://purl.org/becyt/ford/2 |
| dc.description.none.fl_txt_mv |
Species separation can be produced by imposing a pressure gradient in gaseous mixtures, which induces different molecular velocities depending on the molar weight. Pressure gradients can be achieved by centrifugal forces brought about by the passage of the gas through a curved nozzle at supersonic velocity. The efficiency of this process depends on the geometry of the nozzle as well as the flow operating conditions. The numerical solver Fluent was used in order to produce a model of the aerodynamics and the oxygen diffusion of a steady-state flow of air in a curved nozzle. The development of the pressure and O2 concentration profiles along the nozzle were analyzed for different pressure boundary conditions at the inlet and the exit, testing several nozzle sizes. Optimum values of the cut and the inlet pressure were found which maximize the separation efficiency. The effect of the exit pressure was associated with the axial pressure distribution along the inner wall of the nozzle. The results were compared with measurements showing good agreement. Fil: Guozden, Tomas Manuel. Comisión Nacional de Energía Atómica. Gerencia del Área de Energía Nuclear. Instituto Balseiro; Argentina. Consejo Nacional de Investigaciones Científicas y Técnicas; Argentina Fil: Clausse, Alejandro. Comisión Nacional de Energía Atómica; Argentina. Universidad Nacional del Centro de la Provincia de Buenos Aires; Argentina. Consejo Nacional de Investigaciones Científicas y Técnicas; Argentina |
| description |
Species separation can be produced by imposing a pressure gradient in gaseous mixtures, which induces different molecular velocities depending on the molar weight. Pressure gradients can be achieved by centrifugal forces brought about by the passage of the gas through a curved nozzle at supersonic velocity. The efficiency of this process depends on the geometry of the nozzle as well as the flow operating conditions. The numerical solver Fluent was used in order to produce a model of the aerodynamics and the oxygen diffusion of a steady-state flow of air in a curved nozzle. The development of the pressure and O2 concentration profiles along the nozzle were analyzed for different pressure boundary conditions at the inlet and the exit, testing several nozzle sizes. Optimum values of the cut and the inlet pressure were found which maximize the separation efficiency. The effect of the exit pressure was associated with the axial pressure distribution along the inner wall of the nozzle. The results were compared with measurements showing good agreement. |
| publishDate |
2016 |
| dc.date.none.fl_str_mv |
2016-07 |
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info:eu-repo/semantics/article info:eu-repo/semantics/publishedVersion http://purl.org/coar/resource_type/c_6501 info:ar-repo/semantics/articulo |
| format |
article |
| status_str |
publishedVersion |
| dc.identifier.none.fl_str_mv |
http://hdl.handle.net/11336/58704 Guozden, Tomas Manuel; Clausse, Alejandro; Numerical study of gas mixture separation in curved nozzles; Pergamon-Elsevier Science Ltd; International Journal Of Heat And Mass Transfer; 98; 7-2016; 176-182 0017-9310 CONICET Digital CONICET |
| url |
http://hdl.handle.net/11336/58704 |
| identifier_str_mv |
Guozden, Tomas Manuel; Clausse, Alejandro; Numerical study of gas mixture separation in curved nozzles; Pergamon-Elsevier Science Ltd; International Journal Of Heat And Mass Transfer; 98; 7-2016; 176-182 0017-9310 CONICET Digital CONICET |
| dc.language.none.fl_str_mv |
eng |
| language |
eng |
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info:eu-repo/semantics/altIdentifier/doi/10.1016/j.ijheatmasstransfer.2016.03.015 info:eu-repo/semantics/altIdentifier/url/https://www.sciencedirect.com/science/article/pii/S0017931015313004 |
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info:eu-repo/semantics/openAccess https://creativecommons.org/licenses/by-nc-nd/2.5/ar/ |
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openAccess |
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Pergamon-Elsevier Science Ltd |
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Pergamon-Elsevier Science Ltd |
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dasensio@conicet.gov.ar; lcarlino@conicet.gov.ar |
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