- #1
aeHiFlyer210
- 4
- 0
First post here on pf!
I wanted to ask if it's feasible to determine velocities at the top / bottom surface of an airfoil due to the vortex sheet placed on the camber line (due to thin airfoil theory).
I'm attempting to do this because the big picture is to determine the Cp distribution on the top and bottom surface of the airfoil.
Thanks!
I wanted to ask if it's feasible to determine velocities at the top / bottom surface of an airfoil due to the vortex sheet placed on the camber line (due to thin airfoil theory).
I'm attempting to do this because the big picture is to determine the Cp distribution on the top and bottom surface of the airfoil.
Thanks!