Hi!
There was a discussion about that NACA report in the rec.aviation.military
Should be easily found with the google. Here is couple parts:
data come from: Fw 190, Spitfires, Typhoon, Mustang: RAE TN No. Aero 1231
"It should be pointed out, however that where Frise ailerons are used, there is liable to be a variation in the feel of the aircraft. Our pilots, who have now flown three F.W.190s, have, infact noticed this variation; they report that the machine on which measurements were made had rather heavier ailerons than the other two."
A snip from the RAE TN No. Aero 1231:
"Synchronized, automatically recorded readings of aileron angle and angle of bank were taken at speeds between 200 m.p.h. A.S.I. and 400 m.p.h. A.S.I., using a "rat" to record angles, and a free gyro for measuring angle of bank, the instruments being synchronized by a common electrical timer. Measurements were made both to port and starboard using roughly quarter, half and three quarters full aileron movement, and in most cases the stick force to apply aileron was noted on a Henschel type stick force indicator. All the observations of the time to bank have been corrected to 10000 ft."
Hejdå
Gripen