Now showing items 1-2 of 2

    • Suryakumar, Vishvas Samuel (2016-12-12)
      Recent experiments have suggested a strong correlation between local flow features on the airfoil surface such as the leading edge stagnation point (LESP), transition or the flow separation point with global integrated ...
    • Pruski, Brandon (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 ...