Study of surface roughness effect on a bluff body — The formation of asymmetric separation bubbles

Registro completo de metadados
MetadadosDescriçãoIdioma
Autor(es): dc.contributorUniversidade Estadual Paulista (Unesp)-
Autor(es): dc.contributorFederal University of Itajubá (UNIFEI)-
Autor(es): dc.contributorUniversidade do Estado do Rio de Janeiro (UERJ)-
Autor(es): dc.creatorBimbato, Alex Mendonça [UNESP]-
Autor(es): dc.creatorAlcântara Pereira, Luiz Antonio-
Autor(es): dc.creatorHirata, Miguel Hiroo-
Data de aceite: dc.date.accessioned2022-02-22T00:45:20Z-
Data de disponibilização: dc.date.available2022-02-22T00:45:20Z-
Data de envio: dc.date.issued2021-06-25-
Data de envio: dc.date.issued2021-06-25-
Data de envio: dc.date.issued2020-10-31-
Fonte completa do material: dc.identifierhttp://dx.doi.org/10.3390/en13226094-
Fonte completa do material: dc.identifierhttp://hdl.handle.net/11449/205793-
Fonte: dc.identifier.urihttp://educapes.capes.gov.br/handle/11449/205793-
Descrição: dc.descriptionTurbulent flows around bluff bodies are present in a large number of aeronautical, civil, mechanical, naval and oceanic engineering problems and still need comprehension. This paper provides a detailed investigation of turbulent boundary layer flows past a bluff body. The flows are disturbed by superficial roughness effect, one of the most influencing parameters present in engineering applications. A roughness model, recently developed by the authors, is here employed in order to capture the main features of these complex flows. Starting from subcritical Reynolds number simulations (Re = 1.0 × 105), typical phenomena found on critical and supercritical flow regimes are successfully captured, like non-zero lift force and its direction change, drag crisis followed by a gradual increase on this force, and separation and stagnation points displacement. The main contribution of this paper is to present a wide discussion related with the temporal history of aerodynamic loads of a single rough circular cylinder capturing the occurrence of asymmetric separation bubbles generation. The formation of asymmetric separation bubbles is an intrinsic phenomenon of the physical problem, which is successfully reported by our work. Unfortunately, there is a lack of numerical results available in the literature discussing the problem, which has also motivated the present paper. Previous study of our research group has only discussed the drag crisis, without to investigate its gradual increase and the change on lift force direction. Our results again confirm that the Lagrangian vortex method in association with Large-Eddy Simulation (LES) theory enables the development of two-dimensional roughness models.-
Descrição: dc.descriptionFundação de Amparo à Pesquisa do Estado de Minas Gerais (FAPEMIG)-
Descrição: dc.descriptionSchool of Engineering São Paulo State University (UNESP)-
Descrição: dc.descriptionMechanical Engineering Institute Federal University of Itajubá (UNIFEI)-
Descrição: dc.descriptionFaculty of Technology State University of Rio de Janeiro (FAT-UERJ)-
Descrição: dc.descriptionSchool of Engineering São Paulo State University (UNESP)-
Descrição: dc.descriptionFAPEMIG: APQ-02175-14-
Idioma: dc.languageen-
Relação: dc.relationEnergies-
???dc.source???: dc.sourceScopus-
Palavras-chave: dc.subjectBluff body aerodynamics-
Palavras-chave: dc.subjectBoundary layer separation-
Palavras-chave: dc.subjectLagrangian vortex method-
Palavras-chave: dc.subjectRoughness model-
Palavras-chave: dc.subjectVortex shedding-
Título: dc.titleStudy of surface roughness effect on a bluff body — The formation of asymmetric separation bubbles-
Tipo de arquivo: dc.typelivro digital-
Aparece nas coleções:Repositório Institucional - Unesp

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