Ok, I'll admit to an obvious typo - now corrected.
I can't see much point in arguing torque vs gyroscopic precession unless you can explain how the torque changes as the result of a turn.
And please read what other people have written regarding turns:
Quote:
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And at a given pressure altitude, airspeed and angle of bank, in a coordinated turn (i.e. no sideslip), the radius/rate will for most practical purposes be the same for any aircraft. This is down to simple physics.
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Do you agree or disagree with this statement? And if you disagree, can you explain why?