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dc.date.accessioned 2021-09-01T17:42:37Z
dc.date.available 2021-09-01T17:42:37Z
dc.date.issued 2015
dc.identifier.uri http://sedici.unlp.edu.ar/handle/10915/123978
dc.description.abstract 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. en
dc.language en es
dc.subject supersonic flow es
dc.subject impulse turbine es
dc.subject turbomachines es
dc.title Computational Fluid Dynamic Analysis of a Supersonic Turbine en
dc.type Objeto de conferencia es
sedici.identifier.uri http://congress.cimne.com/PANACM2015/admin/files/fileabstract/a634.pdf es
sedici.creator.person Bacchi, Federico es
sedici.creator.person Scarabino, Ana Elena es
sedici.subject.materias Ingeniería Aeronáutica es
sedici.description.fulltext true es
mods.originInfo.place Grupo Fluidodinámica Computacional es
sedici.subtype Resumen es
sedici.rights.license Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International (CC BY-NC-SA 4.0)
sedici.rights.uri http://creativecommons.org/licenses/by-nc-sa/4.0/
sedici.date.exposure 2015
sedici.relation.event First Pan American Congress on Computational Mechanics (PANACM 2015) (Buenos Aires, Argentina, April 27-29, 2015) es
sedici.description.peerReview peer-review es


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Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International (CC BY-NC-SA 4.0) Excepto donde se diga explícitamente, este item se publica bajo la siguiente licencia Creative Commons Attribution-NonCommercial-ShareAlike 4.0 International (CC BY-NC-SA 4.0)