Originally Posted by basic service
"An aircraft in a steady balanced level turn is developing the same amount of lift from both wings"
is not correct because it is the sum of the rolling moments around of the C of M that determines whether or not the aircraft is rolling, not the sum of the forces on each side.
And a moment is:
a) an instant in time.
b) a
force acting at a distance from some axis of rotation.
Answers on a postcard please....
Now you could perhaps make a case that there's an additional moment to offset the prop torque, unless it's a glider, in which case, the rolling moments come from?