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| IL-2 Sturmovik: Cliffs of Dover Latest instalment in the acclaimed IL-2 Sturmovik series from award-winning developer Maddox Games. |
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#1
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The problem may be this: if we assume that the gauge reading of +6 1/4lbs is a true value, i.e. it truly represents the maximum manifold pressure, then there is something wrong in the conversion of the boost value to thrust and speed. I don't know how this is coded in CoD but its probably somewhere in the chain of formulas and values that convert throttle position to manifold pressure, manifold pressure to engine power output, rpm setting, propeller/thrust modelling, drag factors, atmospheric pressure, and probably other factors, to arrive at speed. I assume several of these are the same for both Spitfire and Hurricane (same engine, same propeller) so it could be a common factor (engine modelling) and/or different aerodynamics for the two aircraft (they are both undermodelled at low altitude).
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klem 56 Squadron RAF "Firebirds" http://firebirds.2ndtaf.org.uk/ ASUS Sabertooth X58 /i7 950 @ 4GHz / 6Gb DDR3 1600 CAS8 / EVGA GTX570 GPU 1.28Gb superclocked / Crucial 128Gb SSD SATA III 6Gb/s, 355Mb-215Mb Read-Write / 850W PSU Windows 7 64 bit Home Premium / Samsung 22" 226BW @ 1680 x 1050 / TrackIR4 with TrackIR5 software / Saitek X52 Pro & Rudders Last edited by klem; 04-26-2012 at 08:37 AM. |
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#2
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Is there a graph for the spit IIa (real life, before and after patch lines)?
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#3
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klem 56 Squadron RAF "Firebirds" http://firebirds.2ndtaf.org.uk/ ASUS Sabertooth X58 /i7 950 @ 4GHz / 6Gb DDR3 1600 CAS8 / EVGA GTX570 GPU 1.28Gb superclocked / Crucial 128Gb SSD SATA III 6Gb/s, 355Mb-215Mb Read-Write / 850W PSU Windows 7 64 bit Home Premium / Samsung 22" 226BW @ 1680 x 1050 / TrackIR4 with TrackIR5 software / Saitek X52 Pro & Rudders |
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#4
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#5
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I don't have any other graphs or information now.
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klem 56 Squadron RAF "Firebirds" http://firebirds.2ndtaf.org.uk/ ASUS Sabertooth X58 /i7 950 @ 4GHz / 6Gb DDR3 1600 CAS8 / EVGA GTX570 GPU 1.28Gb superclocked / Crucial 128Gb SSD SATA III 6Gb/s, 355Mb-215Mb Read-Write / 850W PSU Windows 7 64 bit Home Premium / Samsung 22" 226BW @ 1680 x 1050 / TrackIR4 with TrackIR5 software / Saitek X52 Pro & Rudders |
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#6
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But we can compare along the chain where there is historical data, and currently boost is kind of right but the final speeds are wrong. There are some problems with boost though, last night looking at the offline with cockpit off (apologies, I'm sure similar data has cropped up in many other threads): Spits and Hurris have a boost controller (red cutout "off") that gives +5 1/4 to +5 1/2 psi minus boost cutout at 3000rpm full throttle. Boost drops as soon as the throttle is retarded, so CoD model is closest to the "variable datum" type of boost controller for all RAF aircraft. This should be +6 1/4 psi though. Oddly, CoD boost increases to about right (+6.2 psi) when rpm is decreased to the 2600-2800 rpm range. From my reading this is incorrect, the boost controller should not be rpm dependant. The Spit II with boost cutout activated (sea level; full throttle) achieves +9psi at 2600 rpm, +8psi at 3000 rpm (again the rpm-boost quirk). So the CoD Spit II acts most like a 100 octane conversion where the cutout was modified for +9 instead of +12 psi. At 3000rpm, the engine makes some distressed noises/ vibration but does not fail. Dropping rpm to 2600 rpm and/or putting mixture to weak smooths the engine. At sea level, boost cutout on, rad half open, weak mixture, 2600 rpm and +9 psi boost I could maintain 320 mph (IAS and TAS) for a full sortie. That is some serious speed (512 kmh) The CoD Spit Ia/Hurri act (in boost characteristics) like 100 octane conversions where someone drilled the wrong size holes in error and gave tiny increments in boost. You can see the boost cutout effect in Hurri at 2600 rpm if you turn it off and on and watch the boost gauge(+6.2 to +6.4 psi), alhough I could not detect a speed difference. So you can't tell if the virtual tanks have 87 or 100 octane in them, it doesn't matter because the boost never gets high enough. But getting the boost behaviour exactly right doesn't help much if the model does not pass the next check..that the boost combined with other inputs ends up producing overall performance in line with historical norms...which is more of a problem. I didn't realise the Spit II could sit on 320 mph. Had an online sortie on ATAG, I just zigzagged up and down the channel on the wavetops at 320 mph, and started bouncing people from below. Fun, but not very historical I guess camber |
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#7
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Well ... all the problems that they have adapting the performance curve to RL comes from the inefficiency of the formulae to bring the fast boost of the pressure changes (+6 psi at full throttle).
A base curve and then add pressure changes to the FM, as I said, is a effective method to fix this, but is only my opinion. Whatever is the solution I hope that they are on it. Last edited by Buchon; 04-27-2012 at 07:56 AM. |
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#8
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Cheers! |
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#9
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This is another problem with the engine model - switching to auto weak mixture at high boost settings should have quite the opposite affect, causing severe detonation and rapid engine damage. The manual states a maximum boost of 3 3/4 lb when using a weak mixture. These are 100 octane settings and you can halve them if using 87 octane. |
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#10
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I agree Sutts, that mixture feature of the CloD Spit II does not make sense. I can live with it but I would rather it not be there.
I also am concerned about the fact that top speed in the Hurri and Spits is achieved at lower rpm than maximum (2600-2800 vs 3000). I have not seen any historical reference that to get top level speed, you should retard rpm. On the contrary, maximum speed data is given for 3000rpm. I suspect it is a consequence of the rpm-boost quirk of the CloD engine model. Lowering rpm from 3000 to 2600 in CloD adds some boost (although in reality the boost controller should be keeping boost constant regardless of rpm). More boost = more power = more thrust in the flight model (presumably), so the non-historical boost increase at lowered rpm gives a corresponding non-historical speed increase at lowered rpm. |
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