View Single Post
Old Oct 09, 2012, 12:35 PM
DPATE is offline
Find More Posts by DPATE
Grad student in aeronautics
United States, GA, Atlanta
Joined Oct 2010
525 Posts
The reason there would be a vortex there is because of the sudden change in the lift distribution, which an aileron or flap in isolation would have as well. I'm sure reducing the sudden changes in the lift distribution using the "distance-proportional deflection rule" helps.
DPATE is offline Find More Posts by DPATE
Reply With Quote