WF2,
GP can be a factor depending on the yaw rate and angle of bank. With rotaries, it can almost be guaranteed to be a factor. Consider the effect it has on the ease of turning right vs. left. I never explicitly mentioned torque so I'm not sure why you reply to me saying it won't be a factor?
And torque won't (usually) be a (significant) factor
only if we limit the discussion to
engine torque, as generating/countering torque is really the main reason for having ailerons, elevators and rudder in the first place...

(Anyone else competing for the Messerschmidt (a k a besserwisser) award?)
Differential ailerons are not the end-all, be all to induced yaw. In fact, there still induced yaw even with differential ailerons. It's just reduced. Hop in a Twin Astir (
with differential ailerons) and you'll see. Frise ailerons do get closer if done right, or so I'm told (no personal experience).
Not that it matters in most (powered) aircraft except for in the slow-speed regime.
RocketDog,
you are correct in that the CoG position matters squat diddley for the yaw input required in a coordinated turn. The CoG only matters if there's acceleration in the plane concerned, and in a steady coordinated turn there's no acceleration in the aircraft yaw (xy) plane.