Yes, where or how do you get this data?
Well Ded, it's a lot of work. Both Mosq and I have spent dozens of hours each test flying the P-39s. We have our own flight test cards, not unlike those used by real-world test pilots. Virtually every aspect of the flight envelope is explored and quantified.
For example, speed testing is done at increments of 5,000 feet, beginning at sea level (50ft). When I find myself close to the best altitude, I then test in 1,000 foot increments. I've actually broken it down to 100 foot increments on occasion. In the case of the P-39Q, it can reach 383 mph at 12,000 feet, with 383 mph at 13,000 feet and 381 mph at 14k. The P-39Q is a bit faster than the P-38J from 8k thru 13k and about 15 mph faster than the 190A5 at 12k... It's not a rocket, but it is competitive with most fighters between 8K and 14K.
Sea level speed is 329 mph, which is 30 mph faster than the P-40E. Comparing the La-7 to the 109G-14 produces the same speed ratio. Thus, it is quite significant. Moreover, the P-39Q is 10 mph faster at sea level using MIL power than the P-40E is using WEP. Again, this is substantial and an important fact.
Testing shows that the P-39Q accelerates faster and climbs faster than the P-51B or any of the -1 type Corsairs. Clean, it out turns them quite easily. The F4Us are better with flaps, but first they have to survive long enough to slow down and get them out.
So, why does the P-39Q out-perform the P-40E by such a margin? It's really rather easy to understand when you realize that the P-39 is much lighter, has more horsepower and similar wing area. It also has a much lower drag coefficient, which translates into speed.
My regards,
Widewing