Computational Fluid Dynamic Analysis of a Supersonic Turbine

Autores
Bacchi, Federico; Scarabino, Ana Elena
Año de publicación
2015
Idioma
inglés
Tipo de recurso
documento de conferencia
Estado
versión publicada
Descripción
The purpose of this work is to study numerically the flow in a supersonic axial flow impulse turbine. Computations were made with Ansys 15 CFD package, with a 3-dimensional model of one stator-rotor stage. The software implements a “mixing plane model” at the interface between the stator domain, which is stationary, and the rotor domain, which is rotating at a prescribed angular velocity, allowing computing each region separately. The flow information between these domains will be coupled at the mixing plane interface.
Grupo Fluidodinámica Computacional
Materia
Ingeniería Aeronáutica
supersonic flow
impulse turbine
turbomachines
Nivel de accesibilidad
acceso abierto
Condiciones de uso
http://creativecommons.org/licenses/by-nc-sa/4.0/
Repositorio
SEDICI (UNLP)
Institución
Universidad Nacional de La Plata
OAI Identificador
oai:sedici.unlp.edu.ar:10915/123978

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spelling Computational Fluid Dynamic Analysis of a Supersonic TurbineBacchi, FedericoScarabino, Ana ElenaIngeniería Aeronáuticasupersonic flowimpulse turbineturbomachinesThe purpose of this work is to study numerically the flow in a supersonic axial flow impulse turbine. Computations were made with Ansys 15 CFD package, with a 3-dimensional model of one stator-rotor stage. The software implements a “mixing plane model” at the interface between the stator domain, which is stationary, and the rotor domain, which is rotating at a prescribed angular velocity, allowing computing each region separately. The flow information between these domains will be coupled at the mixing plane interface.Grupo Fluidodinámica Computacional2015info:eu-repo/semantics/conferenceObjectinfo:eu-repo/semantics/publishedVersionResumenhttp://purl.org/coar/resource_type/c_5794info:ar-repo/semantics/documentoDeConferenciaapplication/pdfhttp://sedici.unlp.edu.ar/handle/10915/123978enginfo:eu-repo/semantics/altIdentifier/url/http://congress.cimne.com/PANACM2015/admin/files/fileabstract/a634.pdfinfo:eu-repo/semantics/openAccesshttp://creativecommons.org/licenses/by-nc-sa/4.0/Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International (CC BY-NC-SA 4.0)reponame:SEDICI (UNLP)instname:Universidad Nacional de La Platainstacron:UNLP2025-10-15T11:21:32Zoai:sedici.unlp.edu.ar:10915/123978Institucionalhttp://sedici.unlp.edu.ar/Universidad públicaNo correspondehttp://sedici.unlp.edu.ar/oai/snrdalira@sedici.unlp.edu.arArgentinaNo correspondeNo correspondeNo correspondeopendoar:13292025-10-15 11:21:33.181SEDICI (UNLP) - Universidad Nacional de La Platafalse
dc.title.none.fl_str_mv Computational Fluid Dynamic Analysis of a Supersonic Turbine
title Computational Fluid Dynamic Analysis of a Supersonic Turbine
spellingShingle Computational Fluid Dynamic Analysis of a Supersonic Turbine
Bacchi, Federico
Ingeniería Aeronáutica
supersonic flow
impulse turbine
turbomachines
title_short Computational Fluid Dynamic Analysis of a Supersonic Turbine
title_full Computational Fluid Dynamic Analysis of a Supersonic Turbine
title_fullStr Computational Fluid Dynamic Analysis of a Supersonic Turbine
title_full_unstemmed Computational Fluid Dynamic Analysis of a Supersonic Turbine
title_sort Computational Fluid Dynamic Analysis of a Supersonic Turbine
dc.creator.none.fl_str_mv Bacchi, Federico
Scarabino, Ana Elena
author Bacchi, Federico
author_facet Bacchi, Federico
Scarabino, Ana Elena
author_role author
author2 Scarabino, Ana Elena
author2_role author
dc.subject.none.fl_str_mv Ingeniería Aeronáutica
supersonic flow
impulse turbine
turbomachines
topic Ingeniería Aeronáutica
supersonic flow
impulse turbine
turbomachines
dc.description.none.fl_txt_mv The purpose of this work is to study numerically the flow in a supersonic axial flow impulse turbine. Computations were made with Ansys 15 CFD package, with a 3-dimensional model of one stator-rotor stage. The software implements a “mixing plane model” at the interface between the stator domain, which is stationary, and the rotor domain, which is rotating at a prescribed angular velocity, allowing computing each region separately. The flow information between these domains will be coupled at the mixing plane interface.
Grupo Fluidodinámica Computacional
description The purpose of this work is to study numerically the flow in a supersonic axial flow impulse turbine. Computations were made with Ansys 15 CFD package, with a 3-dimensional model of one stator-rotor stage. The software implements a “mixing plane model” at the interface between the stator domain, which is stationary, and the rotor domain, which is rotating at a prescribed angular velocity, allowing computing each region separately. The flow information between these domains will be coupled at the mixing plane interface.
publishDate 2015
dc.date.none.fl_str_mv 2015
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info:eu-repo/semantics/publishedVersion
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http://purl.org/coar/resource_type/c_5794
info:ar-repo/semantics/documentoDeConferencia
format conferenceObject
status_str publishedVersion
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dc.language.none.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv info:eu-repo/semantics/altIdentifier/url/http://congress.cimne.com/PANACM2015/admin/files/fileabstract/a634.pdf
dc.rights.none.fl_str_mv info:eu-repo/semantics/openAccess
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Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International (CC BY-NC-SA 4.0)
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rights_invalid_str_mv http://creativecommons.org/licenses/by-nc-sa/4.0/
Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International (CC BY-NC-SA 4.0)
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repository.name.fl_str_mv SEDICI (UNLP) - Universidad Nacional de La Plata
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