Effects of Leading Edge Protuberances on the Aerodynamic Performance of 2D Cambered Airfoil

The pressure and lift coefficients were measured for airfoils with leading edge protuberances in a subsonic wind tunnel and compared with the performance of a baseline NACA 4415 airfoil with a straight leading edge. These protuberances of 2D airfoil mimic the leading edge configuration of the flippe...

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Bibliographic Details
Main Authors: Abeer Mukhtar, Humera Golandaz, Young Hwan Kim
Format: Article
Language:English
Published: University of Žilina 2012-12-01
Series:Communications
Subjects:
Online Access:https://komunikacie.uniza.sk/artkey/csl-201211-0011_effects-of-leading-edge-protuberances-on-the-aerodynamic-performance-of-2d-cambered-airfoil.php