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wmaxt said:No, those stats say it could/should. We still need the actuall numbers produced in the manouvers in question ie how fast does it accelerate, roll, turn, enter an accelerated stall and retain energy. There is often a dissparity between theory and reality.
I've read pilot accounts on both sides that say their plane was better and at least for those pilots that was true or they would not have lived to say it. Or is it only because the Bf-109 is harder to fly at it's max and the average German pilot was to inexperianced to make full use of it?
Right now I see two aircraft that are very close, one has some stats that infer it could/should be better. We have nothing difinitive yet that can tell us it was better or by how much.
According to pilot accounts and aerodynamic data, this is by far the most likely theory. Although I would alter it to the "average German pilot in 44-45".
Soren said:Remember the 109K-4 would do 4,880ft/min and reach 20,000ft in 4.7min, and had a max speed of 452mph. This coupled with the much lower lift-loading and better wing-aspect ratio, power-loading, wing CL-max, max wing AoA, is more than enough if you ask me...
erich, whats up with all the 2's (twos) ???two cents on the topic.
I./JG 27 lost 42 K-4's during the war.
II./JG 27 lost 2 K-4's
IV./JG 27 lost 22 K-4's
1 outta 3.... Hmmmmmm....IV./JG 27 lost 25 K-4's in 1945 with 9 pilots KIA
Only problem with those number is that they are for 1.98 ata and required C3 fuel. Consider the low fuel stocks in Germany at the time and the 190 had to use C3 it is questionable, how many of the K-4s in the 4 Gruppen that were suppose to convert to 1.98 really did so. The 4 Gruppen (I. / JG 27, III. / JG 2, III. / JG 53, IV. / JG 53) had only 91 operational K-4s as of April 9 1945. Testing of 1.98 started in Dec 1944 but was questionably cleared in early/mid March 1945. There was also much reliabilty problems with the DB605 which also puts into question the use of 1.98.
1.80 ata gave the K-4 a speed of 444mph
wmaxt said:Soren,
The problem with those numbers is that except for the climb and top speed they are static design numbers. There have been hundreds of aircraft that never achieved the theoretical promise of the design and a few that have exceeded it. If the point made above about the fuel is valid then the actual Speed/Climb numbers were also unavailable and we are still looking for Performance figures to compare. Anything else is assumption.
wmaxt
DAVIDICUS said:Wmaxt said, "There have been hundreds of aircraft that never achieved the theoretical promise of the design and a few that have exceeded it."
I remember reading somewhere on this forum that the mechanics in the field had tweaked the R-2800 engines of some late war "D" model Thunderbolts. The engines were rated at 2,530hp at WEP but were developing about 2,700 horsepower as a result.
Soren said:DAVIDICUS said:Wmaxt said, "There have been hundreds of aircraft that never achieved the theoretical promise of the design and a few that have exceeded it."
I remember reading somewhere on this forum that the mechanics in the field had tweaked the R-2800 engines of some late war "D" model Thunderbolts. The engines were rated at 2,530hp at WEP but were developing about 2,700 horsepower as a result.
It certainly wasnt impossible to tweak them that much, but it would be very rare.