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...
Main Authors: | , , |
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Format: | Article |
Language: | English |
Published: |
University of Žilina
2012-12-01
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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 |