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AERODYNAMIC PERFORMANCE ANALYSIS OF CO-FLOW JET AIRFOIL

<p>The work in this paper aims to increase the maximum lift coefficient of the airfoil by implementing the co-flow jet concept on NACA 0018 airfoil and also to investigate the performance of co-flow jet (CFJ) airfoil. To conduct numerical solution, RANS equations have been solved for 2D incompressib...

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Auteurs principaux: C M Vigneswaran, Vishnu Kumar G C
Format: Artigo
Langue:Inglês
Publié: Embry-Riddle Aeronautical University 2021-01-01
Collection:International Journal of Aviation, Aeronautics, and Aerospace
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Accès en ligne:https://commons.erau.edu/ijaaa/vol8/iss1/10
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