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From SL to 5000 ft, the difference in F4U-4s WEP vs. MIL power was 15% increase. Since the F8F was a mech supercharged engine, perhaps the analogy would be better with that R-2800? A 15 % increase makes 2590 HP from 2250.
Here is the URL of WWIIaircraft performance.org: FW 190 D-9 Flight Trials
... and the site you posted is on the other side of the spectrum. I have far too few original documents myself to make a thorough assessment, but when I see readily available test reports "left out" and quotes taken out of context or selected very one-sidedly (others simply ignored), I know what to take with a grain of salt.
You can easily find the P-51B test on the same site. It shows:
Test of a P-541B with V-1650-7 engine @ 8500 pounds:
392 mph @ sea level, 428 mph @ 9800 feet, falling to 420 mph @ 17400 feet, increasing to 454 mph @ 25600 feet, falling to 441 mph @ 35000 feet.
Sure. http://www.wwiiaircraftperformance.org/mustang/p-51b-engdiv-na-flighttestdata.jpg
This graph shows the P-51B going a bit faster at 27,400 feet than I have ever seen anywhere else.
That's why I usually take all the numbers and average them for a first-order estimate.
I see reports on the Fw 190D's and Ta-152's that vary as much as 60 mph or more. What that tells me is there is a wide variety of test conditions, pilots, and test configurations. Might also be some bias there somewhere.
I get most of my estimates these days from the Planes of Fame library in Chino, and they have a LOT of volumes.
Max level speed is just what it says. The maximum speed the plane could achieve while flying straight and level at that altitude.
"Combat speed" is going to lower but there is no real way to measure "combat speed". Any deviation from straight and level flight is going to slow the plane down, even a bank of 5-10 degrees is going to try to cause a gentile turn, the combination of the loss of lift and the drag will slow the plane down. AND that is assuming the plane was at max speed to begin with. It also takes time to accelerate to max speed and just like a car, the last few mph take a disproportionate amount of time to get. A 450mph plane doing 300 mph will take more seconds to accelerate from 350mph to 400 mph than it did from 300mph to 350 mph and the last 50 mph, from 400 to 450 will take an even longer time period.
A 440mph plane will, on average, have a higher combat speed than a 400mph plane because at the lower speeds (320-360mph) the 440mph plane will have better acceleration coming out of a gentile maneuver or cruise setting.
Here is the URL of WWIIaircraft performance.org: FW 190 D-9 Flight Trials
According to test reports of an Fw 190D-9:
With special emergency power, MW50, 3250 RPM, gaps and engine sealed: Max speed was 412 mph @ 20,000 feet and performance fell off after that. Started out at about 378 mph @ sea level, went to 402 mph @ 6,000 feet, fell off to 392 mph @ 11,700 feet. QUOTE]
Actuyually the site you reference quotes a speed of 437mph as well.
Here is what is going on. Most of these tests are the engineers trying to gather data, they are not high speed runs, but there simply to gather aerodynamic coefficients. Many do not involved the use of WEP.
Most notworthy is that fact that these tests are carried out with early engines with slightly dodgy superchargers that cost around 100hp at most altitudes. Many are only carried out at 3000 rpm instead of 3250rpm.
A little history lesson is also worth reviewing. The Jumo 213A that powered the FW 190D-9 was a bomber engine of about 1770 metric hp that ran of B4 ie 87 octane fuel. It really didn't have an emergeny boost system. Had the Germans been serious about the FW 190D9 they would have powered it by the 2000hp Jumo 213C engine which ran of C3 fuel and produced that power level without MW50. It also had the mountings for a propeller and a motor canon. As it was they had a surplus of bomber engines to make use of.
The FW 190's Jumo 213 thus received a series of rapid modification which were added in the field to upgrade the Jumo 213A.
The first was a mixture injection system that transfered fuel from the multipoint injection system into the eye of the supercharger: this achieved 1900hp though a charge cooling effect.
The second was a basic water methanol injection system called the Oldenberg system that worked by using supercharger pressure to blow the MW-50 out of the tank into the engine. This system was fitted by Luftwaffe technicians.
The third was an high flow junkers MW-50 system, which was fitted by Junkers factory technicians because it needed control system modes, I expect it used used injection pumps with better vaporisation and flow rates.
Somewhere in there is an RPM increase from 3000 rpm to 3250 rpm and latter still use of C3 fuel.
Most FW 190's would have been fitted with one of the MW-50s by the end of 1944 and certainly by January 1945.
AFAIKT the speed of a FW m190D-9 in actual combat trim was around 430-432 at 1.8 ata . This is very respectable at the medium to lower altitudes in question.
The FW 190D-9 with the Jumo 213C engine was never produced, however a few with the Jumo 213F engine installed in the FW 190D-13 (with at two stage supercharger) did see service.
This aircraft had hydraulically boosted ailerons. (Discovered when Yellow 12 was mated with its orginal wings)