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Open access Sep 2026

Comparative aerodynamic performance assessment of NACA 2412 and NACA 0012 aerofoils with winglet integration: a computational study using MATLAB-CATIA-CFD framework

Winglets are aerodynamic devices that reduce induced drag by mitigating wingtip vortices, thereby improving aircraft fuel efficiency and overall performance. This study presents a comparative computational investigation of the aerodynamic performance of wings with NACA 2412 (cambered) and NACA 0012 (symmetric) airfoils...

Irfan Nazir Wani, Manoj Kumar, P. Shukla · 0 citations

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