Velocity measurements were taken using a single hot wire probe driven by a constant temperature anemometer. Velocity profile data were taken at an angle of attack of 4Ad and Re- c=235, 000 at chord positions ranging from x/c=0.15 to x/c= 0.99 . ... The first vortex generators to be applied to the airfoil were the Wheeler wishbone type with a maximum apex height of 1.27mm, corresponding to approximatelyanbsp;...
|Title||:||AIAA 28th Aerospace Sciences Meeting|