STUDY OF MESH REFINEMENT ON THE AERODYNAMIC COEFFICIENTS FOR NACA2412 PROFILE WITH DIFFERENT ANGLE OF ATTACK AND k - w TURBULENCE MODEL

Nícolas Lima Oliveira, Eric Vargas Loureiro, Patrícia Habib Hallak

Resumo


This work presents the studies  obtained using OpenFOAM OpenSource Computational Fluid Dynamics (CFD) Software. Experiments were performed to predict lift coefficient and drag coefficient curves for the NACA2412 profile. Subsequently, the results obtained were compared with the results of the bibliography and discussed.

Palavras-chave


CFD; OpenFOAM; airfoil

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DOI: http://dx.doi.org/10.21575/25254782rmetg2020vol5n21141

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Direitos autorais 2020 Nícolas Lima Oliveira, Patrícia Habib Hallak, Eric Vargas Loureiro

Revista Mundi Engenharia, Tecnologia e Gestão ISSN 2525-4782

Qualis: B4 - Interdisciplinar, B5 - Geografia, B5 - Administração Pública e de Empresas, Ciências Contábeis e Turismo, B5 - Comunicação e Informação, B5 - Engenharias III