Plunging Airfoil Load Characteristics Equipped with Gurney Flap

M. Mani

Volume 10, Issue 2 , September 2013, , Pages 25-36

Abstract
  Numerous experiments have been conducted on plunging Eppler 361 airfoil in a subsonic wind tunnel. The experimental tests involved measuring the surface pressure distribution over the airfoil at Re=1.5×105. The airfoil was equipped with Gurney flap(heights of 2.6, 3.3 and 5% chord) and plunged at 6cm ...  Read More