jBAY Modeling of Vane-Type Vortex Generators and Study on Airfoil Aerodynamic Performance
dc.contributor.author | Chillón, Sergio | |
dc.contributor.author | Uriarte Uriarte, Antxon | |
dc.contributor.author | Aramendia Iradi, Iñigo | |
dc.contributor.author | Martínez Filgueira, Pablo | |
dc.contributor.author | Fernández Gámiz, Unai | |
dc.contributor.author | Ibarra Udaeta, Iosu | |
dc.date.accessioned | 2020-06-01T10:41:47Z | |
dc.date.available | 2020-06-01T10:41:47Z | |
dc.date.issued | 2020-05-12 | |
dc.identifier.citation | Energies 13(10) : (2020) // Article ID 2423 | es_ES |
dc.identifier.issn | 1996-1073 | |
dc.identifier.uri | http://hdl.handle.net/10810/43660 | |
dc.description.abstract | The increased demand for wind power is related to changes in the sizes of wind turbines and the development of flow control devices, such as vortex generators (VGs). In the present study, an analysis of the vortices generated by a vane-type VG is performed. To that end, the aerodynamic performance of a DU97W300 airfoil with and without VG is evaluated. The jBAY source term model was implemented for simulation of a triangular-shaped VG and the resolution of the fully meshed computational fluid dynamics (CFD) model. Reynolds-averaged Navier–Stokes (RANS) based simulations were used to calculate the effect of VGs in steady state, and the detached eddy simulation (DES) method was used for angles of attack (AoAs) around the stall situation. All jBAY based numerical simulations were carried out with a Reynolds number of Re = 2 × 106 to analyze the influence of VGs with AoAs between 0 and 20° and were validated versus experimental wind tunnel results. The results show that setting up a VG device on an airfoil benefits its aerodynamic performance and that the use of the jBAY model for simulation is accurate and efficient. | es_ES |
dc.description.sponsorship | The authors are grateful to the government of the Basque Country and the University of the Basque Country UPV/EHU through the SAIOTEK (S-PE11UN112) and EHU12/26 research programs, respectively. | es_ES |
dc.language.iso | eng | es_ES |
dc.publisher | MDPI | es_ES |
dc.rights | info:eu-repo/semantics/openAccess | es_ES |
dc.rights.uri | http://creativecommons.org/licenses/by/3.0/es/ | |
dc.subject | flow control | es_ES |
dc.subject | vortex generator | es_ES |
dc.subject | jBAY model | es_ES |
dc.subject | computational fluid dynamics (CFD) | es_ES |
dc.subject | source-term model | es_ES |
dc.subject | boundary layer | es_ES |
dc.title | jBAY Modeling of Vane-Type Vortex Generators and Study on Airfoil Aerodynamic Performance | es_ES |
dc.type | info:eu-repo/semantics/article | es_ES |
dc.date.updated | 2020-05-28T14:09:49Z | |
dc.rights.holder | 2020 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/). | es_ES |
dc.relation.publisherversion | https://www.mdpi.com/1996-1073/13/10/2423/htm | es_ES |
dc.identifier.doi | 10.3390/en13102423 | |
dc.departamentoes | Ingeniería nuclear y mecánica de fluidos | |
dc.departamentoeu | Ingeniaritza nuklearra eta jariakinen mekanika |
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Except where otherwise noted, this item's license is described as 2020 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/).