Originally posted by ddekel
Bernard,
In a coordinated turn (with no sideslip)
what makes the plane stay in it's bank angle
is the deflection of the ailerons.
the inner wing has lower airfoil camber (lower CL) due to aileron up, and the outer wing has an increase in airfoil camber
due to aileron down (higher CL)
if you live the sticks while in a turn,
low c.g A/P will roll back while others like EXTRA 300 (middle c.g)
will stay in it's current bank angle.
please explain in a more scientific manner what is wrong
with my previous explanation.
Obviously, the deflection of the ailerons induce the bank (not the turn), but, as consequence, if you don't want the plane to sink, you have to apply elevator to counteract for loss of lift.
I don't care a bit about the scientific langage, as if you can't explain and understand in simple terms, it means you don't have a good grasp on the concepts. In French "Ce qui ce concoit bien s'enonce clairement".
You should re-read my previous message, and answer to it, this answer do not address the point.
Bernard