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#1
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http://kurfurst.org/Engine/DB60x/DB6...sheets_A0.html I always thought Aa was basically slightly modified (re-designed head, reinforced valves allowing higher MFP, different supercharger gear ratio (I am not sure about exact details here) leading to slightly lower FTH traded for more power below FTH. Quote:
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I also only seen it here and I remember the power of DB 601A-1 was set at 1020PS. I'll try to find that data, I have no idea how to extract anything from the game.
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Bobika. |
#2
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To the trimm topic. I know, it's G, but the trimm mechanics is the same:
(For those who doubt that the trim could be used at any time... ![]() "Sarantola recalled that the MT was a very stable plane, but not the most maneuverable. The stick forces were quite large and elevator trim was used quite frequently while maneuvering. MT was easy to fly and overall a safe plane. Flying and landing was easy." - Olli Sarantola, Finnish fighter pilot. Source: Blitz '01 - Meeting With The Veterans by Finnish Virtual Pilots Association. Even more interesting is the fact that they tried different positions of the trimming. With the wrong trimset - the one for cruising at high altitude it was not possible to pull out of the dive just by using the stick. They needed to use the trimwheel to recover the plane from the dive. This happened in such violent manner that the testpilot had to push the stick foreward to be not blacked out... If the trim was set to +1.15° it was possible to recover without using the trimwheel - both flightpaths, with and without the trimwheel, are very similar. So even with the concrete stick the limitating factor seems to be the pilot. Also interesting in the dive the canopy iced, also the mechanism of the trim, so it was not possible to set it smooth, but in \"jumps\", but it was still adjustable... - Source: Hochgeschwindigkeitsversusche mit Me 109, Messerschmitt AG, Augsburg. Clarification of the escape dive: "It didn't stay (vertical) otherwise, it had to be kept with the stabilizer. I trimmed it so the plane was certainly nose down. Once I felt it didn't burn anymore and there was no black smoke in the mirror, then I began to straighten it up, and it wouldn't obey. The stick was so stiff it was useless. So a nudge at a time, (then straightening off with trims). Then the wings came alive with the flutter effect, I was afraid it's coming apart and shut the throttle. Only then I began to level out. To a thousand meters. It was a long time - and the hard pull blacked me out." - Edvald Estama, Finnish fighter pilot. Source: Recollections by Eino and Edvald Estama by Finnish Virtual Pilots Association.
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#4
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![]() Is not working as it should? This means that I lost the thread somewhere ![]() There is ticket on the bugtracker about this issue?
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#5
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You've done a few 109 issues Tom, is this one for you perhaps?? I also think that there needs to be some research into the Spitfire and Hurricane trims too, although perhaps nobody has complained really because they are already better turners so it isn't needed (exception of when the trim is used as per the original point of the thread) |
#6
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The stability is one of the reasons for the higher control forces. The high elevator control forces is a function of the "stick force per G" of the control design. It is way beyond the scope of a gaming forum to adequately explain stability and control. I will try and explain it so you get the basic idea. There is a point in the aircraft's balance that is called the neutral point. If our center of gravity was placed at this point, the aircraft would have no tendency to return to last condition of trim. It would be neutral and continue in whatever direction we told it too. It would also require no force at all to move the stick, only the resistance from the hinge moments. Do you know the law of levers; it is the basis for all Stability and control? It says that at the fulcrum, two moments or torque force of the levers will be equal. Our basic formula for determing the torque force: Moment = Arm x weight Weight is the weight of the object or amount of force we place on the arm. Arm is the distance from the Neutral Point in the case of stability. Moment is the torque force required to move about the nuetral point. The distance between our center of gravity and our neutral point determines the stability of the aircraft. The longer our arm or farther away we are from the neutral point, the more torque force we generate to return to last trimmed condition of flight. WTE_Galloway was correct in his explaination. Understand? Neutral stability, for the most part, is not good in an aircraft. Neutrally stable aircraft are "twitchy" and difficult to precisely control. Stable aircraft are easier to precisely manuver but come at the cost of higher input forces. The only axis Neutral stability is considered acceptable is lateral. Wings inhernetly have a considerable amount of roll stability. Unstable is even worse and does require modern fly by wire controls to safely fly the aircraft. Most WWII fighters were just barely stable. Now is above corner speed, you want a high stick force per G gradiant. It keeps the pilot safe by ensuring he does not destroy the airframe. Last edited by Crumpp; 04-20-2012 at 12:15 AM. |
#7
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I am not saying the Bf-109 does not require trim input. There is a very tenious connection. It is entirely possible to have an unstable aircraft that trims very positively just as it is possible to have a stable aircraft that cannot be trimmed. Last edited by Crumpp; 04-20-2012 at 12:15 AM. |
#8
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![]() ![]() ![]() I can not help with RAF types, I have only pilot's manual (no technical info, only aircraft handling and performance)
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![]() ![]() i7 7700K 4.8GHz, 32GB Ram 3GHz, MSI GTX 1070 8GB, 27' 1920x1080, W10/64, TrackIR 4Pro, G940 Cliffs of Dover Bugtracker site: share and vote issues here Last edited by VO101_Tom; 04-20-2012 at 02:33 AM. |
#9
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I had asked if 109 drivers were using trim to gain more lead and if so was this accurate to RL. From reading the thread I think there are 2 potential issues: 1. That presently the 109 does not require trim to be pulled out of a high speed dive. In RL trim would have to be set prior to the dive in order to pull out. 2. The trim wheel in game moves too quickly compared to how a RL pilot could make adjustments (there are answers and videos in the thread). Some O/L pilots are using this to gain lead quickly, which is unrealistic. I suggested that a 109 expert validate the information gathered in order to make the 109 more accurate via the bugtracker. I do not know if the same problem occurs in RAF fighters however I suspect this would not be required given that they already have the turn advantage. Does that make sense? ~S~ |
#10
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I have very little data of the technical 601Aa, apart from that it seems that it was originally meant as an export version (small a = auslandisch or foreign, ie. export), but about 1/3 of all 601s were of the Aa version (info via butch2k). All E-7s (save the ones with 601N) and all /B versions had the Aa. The rest were probably mixed. As for output, all I can say it had improved output and higher manifold pressures. As for the improved supercharger, I can attach to technical sheet (showing the increased FTH of the new supercharger, or neue Lader) and power curves for the new supercharger DB 601A-1. I believe the A-0 was an early pre-production model only. Quote:
I believe the conversion between continental PS and imperial BHP is 0,986 PS = 1 HP. It makes very little difference, especially in practice considering the tolerance for production engines. One 109 report I have for example shows the engine was down about 50 HP compared to nominal.. 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 ![]() |
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