Aerodynamic study of a drag reduction system and its actuation system for a formula student competition car

Detalhes bibliográficos
Autor(a) principal: Loução, Ricardo
Data de Publicação: 2022
Outros Autores: Duarte, Gonçalo O., J. G. C. Mendes, M.
Tipo de documento: Artigo
Idioma: eng
Título da fonte: Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos)
Texto Completo: http://hdl.handle.net/10400.21/15471
Resumo: This work presents a computational fluid dynamic (CFD) analysis of a drag reduction system (DRS) used in a Formula Student competition vehicle, focusing on the interaction between the triple wing elements, as well as on the electrical actuators used to provide movement to the upper two flaps. The S1123 wing profile was chosen, and a 2D analysis of the wing profile was made. The trailing edge was rounded off to conform to Formula Student competition safety rules, resulting in around a 4% decrease in the lift coefficient and around a 12% increase in the drag coefficient for an angle of attack of 12°, compared to the original wing profile. The multi-element profile characteristics are: wing main plate with 4°, first flap 28°, and second flap 60°. To evaluate the wing operation, end plates and electrical linear actuators were added, generating a maximum lift coefficient of 1.160 and drag coefficient of 0.397, which provides around a 10% reduction in lift and a 9% increase in drag compared to the absence of the linear actuators. When activating the DRS, the flap rotation generates about a 78% decrease in the aerodynamic drag coefficient and 53% in the lift coefficient for the minimum aerodynamic drag setting.
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spelling Aerodynamic study of a drag reduction system and its actuation system for a formula student competition carAerodynamic studyDrag reduction systemWings actuatorsFormula student competition carThis work presents a computational fluid dynamic (CFD) analysis of a drag reduction system (DRS) used in a Formula Student competition vehicle, focusing on the interaction between the triple wing elements, as well as on the electrical actuators used to provide movement to the upper two flaps. The S1123 wing profile was chosen, and a 2D analysis of the wing profile was made. The trailing edge was rounded off to conform to Formula Student competition safety rules, resulting in around a 4% decrease in the lift coefficient and around a 12% increase in the drag coefficient for an angle of attack of 12°, compared to the original wing profile. The multi-element profile characteristics are: wing main plate with 4°, first flap 28°, and second flap 60°. To evaluate the wing operation, end plates and electrical linear actuators were added, generating a maximum lift coefficient of 1.160 and drag coefficient of 0.397, which provides around a 10% reduction in lift and a 9% increase in drag compared to the absence of the linear actuators. When activating the DRS, the flap rotation generates about a 78% decrease in the aerodynamic drag coefficient and 53% in the lift coefficient for the minimum aerodynamic drag setting.MDPIRCIPLLoução, RicardoDuarte, Gonçalo O.J. G. C. Mendes, M.2023-02-02T16:47:01Z2022-09-162022-09-16T00:00:00Zinfo:eu-repo/semantics/publishedVersioninfo:eu-repo/semantics/articleapplication/pdfhttp://hdl.handle.net/10400.21/15471engLOUÇÃO, Ricardo; [et al] – Aerodynamic study of a drag reduction system and Its actuation system for a formula student competition car. Fluids. EISSN 2311-5521. Vol. 7, N.º 9 (2022) p. 1-12.10.3390/fluids70903092311-5521info:eu-repo/semantics/openAccessreponame:Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos)instname:Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informaçãoinstacron:RCAAP2023-08-03T10:13:02Zoai:repositorio.ipl.pt:10400.21/15471Portal AgregadorONGhttps://www.rcaap.pt/oai/openaireopendoar:71602024-03-19T20:23:08.155386Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos) - Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informaçãofalse
dc.title.none.fl_str_mv Aerodynamic study of a drag reduction system and its actuation system for a formula student competition car
title Aerodynamic study of a drag reduction system and its actuation system for a formula student competition car
spellingShingle Aerodynamic study of a drag reduction system and its actuation system for a formula student competition car
Loução, Ricardo
Aerodynamic study
Drag reduction system
Wings actuators
Formula student competition car
title_short Aerodynamic study of a drag reduction system and its actuation system for a formula student competition car
title_full Aerodynamic study of a drag reduction system and its actuation system for a formula student competition car
title_fullStr Aerodynamic study of a drag reduction system and its actuation system for a formula student competition car
title_full_unstemmed Aerodynamic study of a drag reduction system and its actuation system for a formula student competition car
title_sort Aerodynamic study of a drag reduction system and its actuation system for a formula student competition car
author Loução, Ricardo
author_facet Loução, Ricardo
Duarte, Gonçalo O.
J. G. C. Mendes, M.
author_role author
author2 Duarte, Gonçalo O.
J. G. C. Mendes, M.
author2_role author
author
dc.contributor.none.fl_str_mv RCIPL
dc.contributor.author.fl_str_mv Loução, Ricardo
Duarte, Gonçalo O.
J. G. C. Mendes, M.
dc.subject.por.fl_str_mv Aerodynamic study
Drag reduction system
Wings actuators
Formula student competition car
topic Aerodynamic study
Drag reduction system
Wings actuators
Formula student competition car
description This work presents a computational fluid dynamic (CFD) analysis of a drag reduction system (DRS) used in a Formula Student competition vehicle, focusing on the interaction between the triple wing elements, as well as on the electrical actuators used to provide movement to the upper two flaps. The S1123 wing profile was chosen, and a 2D analysis of the wing profile was made. The trailing edge was rounded off to conform to Formula Student competition safety rules, resulting in around a 4% decrease in the lift coefficient and around a 12% increase in the drag coefficient for an angle of attack of 12°, compared to the original wing profile. The multi-element profile characteristics are: wing main plate with 4°, first flap 28°, and second flap 60°. To evaluate the wing operation, end plates and electrical linear actuators were added, generating a maximum lift coefficient of 1.160 and drag coefficient of 0.397, which provides around a 10% reduction in lift and a 9% increase in drag compared to the absence of the linear actuators. When activating the DRS, the flap rotation generates about a 78% decrease in the aerodynamic drag coefficient and 53% in the lift coefficient for the minimum aerodynamic drag setting.
publishDate 2022
dc.date.none.fl_str_mv 2022-09-16
2022-09-16T00:00:00Z
2023-02-02T16:47:01Z
dc.type.status.fl_str_mv info:eu-repo/semantics/publishedVersion
dc.type.driver.fl_str_mv info:eu-repo/semantics/article
format article
status_str publishedVersion
dc.identifier.uri.fl_str_mv http://hdl.handle.net/10400.21/15471
url http://hdl.handle.net/10400.21/15471
dc.language.iso.fl_str_mv eng
language eng
dc.relation.none.fl_str_mv LOUÇÃO, Ricardo; [et al] – Aerodynamic study of a drag reduction system and Its actuation system for a formula student competition car. Fluids. EISSN 2311-5521. Vol. 7, N.º 9 (2022) p. 1-12.
10.3390/fluids7090309
2311-5521
dc.rights.driver.fl_str_mv info:eu-repo/semantics/openAccess
eu_rights_str_mv openAccess
dc.format.none.fl_str_mv application/pdf
dc.publisher.none.fl_str_mv MDPI
publisher.none.fl_str_mv MDPI
dc.source.none.fl_str_mv reponame:Repositório Científico de Acesso Aberto de Portugal (Repositórios Cientìficos)
instname:Agência para a Sociedade do Conhecimento (UMIC) - FCT - Sociedade da Informação
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