|
Paul:
I'm trying to visualize your control surface
shaping suggestions.
Are you saying that if the trailing edge of the
wing ahead of the aileron or elevator were 10 centimeters thick, the
leading edge of the aileron or elevater should be 11.5 centimeters thick
(rounded, of course) on each side for a total thickness of 13 centimeters?
And that the control surface thickness would swell aft of that to
maintain a convex shape? Or did you mean to say "concave", which would
reduce the thickness aft of the leading edge?
JHK
Struggling to learn
|