ORIGINAL: britbrat
Well if you don't like that one, here is another much simpler explanation for lack of left roll until stall -- the (normally) proverse rudder-roll couple is offsetting the torque reaction, thus preventing, or reducing the left roll. In aircraft that exhibit adverse rudder-roll, they will indeed roll left prior to stall.
I have more.
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Lost me on that one. 'splain the pro-verse adverse rudder roll concept
thanks