Sep 19, 2018 #1 Zipper730 Chief Master Sergeant 4,430 1,023 Nov 9, 2015 I'm curious about the P-51's wings: With the thickest part so far aft was the C/L at 40% or so, or still at 20-30%?
I'm curious about the P-51's wings: With the thickest part so far aft was the C/L at 40% or so, or still at 20-30%?
Jun 8, 2019 #2 W wells Airman 98 70 Mar 9, 2008 Ontario, Canada It's more dependent upon the mean line, not the thickness distribution. The component of lift due to angle of attack acts at 25%, so it will move forward as the angle of attack increases.
It's more dependent upon the mean line, not the thickness distribution. The component of lift due to angle of attack acts at 25%, so it will move forward as the angle of attack increases.