The main prob i see in here is the limited stick force.
in a plane without power boosted ailerons (P38L/FW190D13) the stick force is the most limiting factor to roll rate.
the diagramm tells us that at 50lbs the planes have the shown rollrates, but what happens at 60lbs, 70lbs and so on, and how far is this force increasing in relation to possible roll rate at that specific force.
i.e. u have two planes that must use 30 lbs stick force to roll 50 degree sec at a given speed, but plane #1 will roll at 120 degree/sec at 60lbs plane #2 will only manage 90 degree/sec at 60 lbs (due to airflown, areodynamics and other factors applied to the aileron), this might go on like this. here a short table of this example
force/rollrate#1/rollrate#2
30/50/50
40/65/60
45/80/69
50/95/78
55/108/85
60/120/90
65/130/93
70/138/95
if u take this table and imagine the influence it has on a fight between both planes (all other factors the same-but roll rates remain in the same ratio over the whole speed range)
#1 will always have an advantage due to easy handling
u can also go through it even more
consider #1 has reached max aileron deflection at 70 lbs so planes max roll rate will stay at 138 degree/sec
#2 has not reached max deflection at 70lbs. and would if u increase force to a bone breaking 200 lbs be capable of also 138 degree/sec but what pilot would ever be able to do so
Now to have max possible roll rates, it would be could to have a table that shows stick force needed to deflect ailerons full at any given speed and also roll rate at that speed
in a 2nd table u than would have to find out what the AH-alter-ego-pilot would be capable of and find the roll rates related to that force, it would even be possible that in some planes the stick force for full deflection is below the max possible AH-pilot stick force which means the plane would be really easy to handle
[ 07-28-2001: Message edited by: Naudet ]
[ 07-28-2001: Message edited by: Naudet ]