Browsing by Subject "Vortex dominated flowfield"
Now showing items 1-1 of 1
-
(2012-11-27)The leading edge flow structure of the NACA 0012 airfoil is experimentally investigated under dynamic stall conditions (M = 0.1; α = 16.7◦, 22.4◦; Rec = 1× 10^6) using planar particle image velocimetry. The airfoil was ...