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#421
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Show me any report of any 262 pilots who would go into a turning dogfight against a Mustang, Spit, La 7, whatever take your pick. The theoretical world is one thing, hard combat another. Look at it another way, Why did the Mig 17 do so well against the F4, F105 and so on. Find any US pilot who would go into a turning combat in any of the above against an old slow Mig 17. |
#422
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I love the way Kurfurst seems to think the 262 would even be in with a shot at a turning fight, at those speeds it's going to fly circles so big it's circumnavigating the globe
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#423
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It's not about turning fights, it's about the ability of a plane to sustain a turn at a given speed. That's what the chart shows. It's something else what you make of it - both here at the forum discussing it, and in the air piloting these planes.
Like with that Gripen, most accidents happen due to pilot error, not erroneous design calculations. It's rather an argument against the reliability of pilot accounts, than an argument against reliability of maths and physics - so I'm not quite sure why you posted the video. |
#424
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Of particular interest, translated from the paper. Condition of the airframe : The surface was painted after the serial production standard. The engine cowling was still rough, exhaust manifolds (DB-type, made at BFW) were lacking top cover. 2 Cowl- and wing-MGs were installed. Antenna wire. Undercarriage retracted, tailwheel out. For air intake, see the reports drawings. Radiator cooler flaps were 1/4 open. Coolant temperature observed as constant 90 degrees Celsius. Oil cooler flaps were closed. Oil temperature observed as 62/82 degrees Celsius.' Speed was measured on the four-way flight track in Haunstetten. Altiude trials were performed near Augsburg airfield. Measured speed for 0 m was 493 kph at 1,33ata. The engine was measured on test bench, and was found to develop 45 PS less than the guaranteed nominal output at 1,35 ata, so the flight results were corrected (see Blatt 5 for calculations) to the nominal engine ratings and German Standard day : 498 km/h at 0 m (CINA) at 1.35ata.. Quote:
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Il-2Bugtracker: Feature #200: Missing 100 octane subtypes of Bf 109E and Bf 110C http://www.il2bugtracker.com/issues/200 Il-2Bugtracker: Bug #415: Spitfire Mk I, Ia, and Mk II: Stability and Control http://www.il2bugtracker.com/issues/415 Kurfürst - Your resource site on Bf 109 performance! http://kurfurst.org ![]() |
#425
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By the time it was allowed to be a fighter those pilots had little intention of being fighters what with the sheer number of escorts to deal with. No, get fast and whip through the formations with those mighty cannon.
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#426
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Regarding level speed performance of the 109, a question raised by I think MiG-3U puzzled me, maybe you have a good explanation, I'm at a loss for now: How come the 109E is faster than the 109F at less power, if you accept the 498 km/h for the 109E at 990ish hp from the V15 test and the 495 km/h for the 109F at 1065ish hp from the 109F Kennblatt?
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#427
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Oh, have I misunderstood something? I just figured since the thread went OT within 7 pages or so and it turned into an argument about which aircraft had the turning advantage it 'was' about turning fights, if I'm not mistaken that is exactly what triggered the whole change of topic was a turning circle diagram and the usual suspects denying that the Spit would win in a turning fight.
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#428
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#429
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#430
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Doesn't the V in a designation mean a prototype/test a/c?
Bf 109 V15a |
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