The word 'circles' is plural, so I assume they meant under more than one condition, but you're right, that's not very scientific.
Yes, the report mentions that there were tests at different altitudes, but we have no idea what test was carried out or under what conditions so there simply isn't enough information to interpret the statements correctly.
Also, the roll rates being very much the same, seems to indicate there were no material differences that were worth noting.
That's not surprising... same wings, same wing span, same controls, very little difference in the moment of inertia in the roll axis, you wouldn't expect much difference in roll.
But the most important part to me was them saying it maneuvers as well as the IX and outperforms at all heights, and is easy to fly.
The catch is that in this report when they refer to maneuvering, they are also talking about how well the aircraft responds to control commands in terms of pitch rates and roll acceleration and how the aircraft responded to the controls, not only how well it turned, and there is nothing to quantity it. Also when they refer to performance, they typically mean linear speed or acceleration, not how well it turned, and again, not quantified.
So, I'm guessing Bruv is right in that the torque is overdone.
I would guess otherwise, because the torque can be easily calculated, it is high school physics and depends on the engine and prop configuration. Also the engine and prop data is far easier to find than flight test data so I think it is very unlikely that HTC would get that wrong.
Also the roll rates are probably too slow and it gets too unstable at slow speed turns.
Again, that report doesn't provide enough information to quantify either the roll rates or low speed stability.
Is the Spitfire Mk XIV correct? As I said before, I haven't done enough work on the Mk XIV to be sure. But one thing I am sure of, is that the report linked to above will be of very limited help.
Regards
Badboy