I'll be interested to see how torque is modelled in planes like the camel with regards to control inputs.
The theoretical speeds for the fastest and tightest turns for these aircraft fall BELOW the stall speeds. Therefore, the maximum turn rate and tightest turn is calculated at the stall speed in a turn.
This simply cannot be correct.
That was my reaction. Still can't wrap my head around what that means. I'd love to see some other data/sources.Regards,Wab