Compression, as ive understood,is modeled. Compression means, that you reach speed, where your aeliron movements doesent have any effect to the plane roll/whatever. If you reach 100% deflection when you compress, it has no affect to your plane or only very slight. In AH you can reach it easily in p38, but jug breaks up before that speed.
Also pilot strenght is modeled in il-2, but its not that restricted as 50lbs max, someone stated that its 40-50kg in il-2; makes big difference in performance of higher speeds like over 300mph. 50kg is no big deal atleast with 2 hands and pull/push. Sideways are different.
There was no aerodyamic restriction of 109-g2 rolling almost as fast as some 190 models, atleast this has been stated by Oleg and i have no doubt about hes professionalism in aerodynamics. Only difference can be seen in NACA charts, theyre accurate, but only to 50lbs stick forces. The quoted books have very different statemens, but i believe the stories are not made up. The pilot just maybe were fatigued, newbie or had bad petrolium. AH is not based on book statements, but on test charts, same goes on il-2.
(250kmh/156mph)
(650kmh/406mph)
(notice the speed and aeliron deflection)
"I've made some (very simple) rollrate-tests, and according to these tests, the ME109 takes approx. 2,5 seconds for a360°-roll @250km/h and 5 seconds @650KM/h (same altitude, both throttle @0%, left roll)
So, I see a decrease in rollrate with speed."
[ 09-01-2001: Message edited by: Tuomio ]