Numerical Study on the Effect of an Off-Surface Micro-Rod Vortex Generator Placed Upstream NACA0012 Aerofoil

In this paper, 3D numerical simulations have been carried out to enhance the understanding of a flow over a passive control device composed of micro cylinder with, d/c = 1.34% placed in the vicinity of NACA0012 aerofoil wing, by means of γ–Reθt transition sensitive turbulence model meant to predict...

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Autores principales: Larabi Abderrahim, Pereira Michael, Ravelet Florent, Azzam Tarik, Oualli Hamid, Menfoukh Laiche, Bakir Farid
Formato: article
Lenguaje:EN
FR
Publicado: EDP Sciences 2021
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Acceso en línea:https://doaj.org/article/edaf51e8ac174a0ca6f9e3e4c85fa136
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