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#1
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Winger |
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#2
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Wonder if there is a bug with the mixture...Its auto so we can't change it,but it sounds like the mix is too rich at altitude.
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#3
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Today I tried again with my friends in multiplayer (with the "mod" finally we can fly together, but the multiplay "seems" limited to 6 players, have you ever hosted for more humans?): flying in a inflight 109 (former AI) I reached the 5 km before any shake. Maybe I had the first shake after x seconds from the airplane selection (takeoff/2,5km = 2km/5km) I really don't know: anyway we tested some SpitIIa vs 109E4 and, I'm really sorry to say it, but the energy management seems to be AGAIN the one of IL2 version < 4.10. It was our first real test, so probably we are still noobs with the full EM: anyway the 109 seems to lose tons of energy in a candle. I'm still optimist (but please I can't wait AGAIN 10 years to have good FMs): for now the priorities are others I hope.
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![]() A whole generation of pilots learned to treasure the Spitfire for its delightful response to aerobatic manoeuvres and its handiness as a dogfighter. Iit is odd that they had continued to esteem these qualities over those of other fighters in spite of the fact that they were of only secondary importance tactically.Thus it is doubly ironic that the Spitfire’s reputation would habitually be established by reference to archaic, non-tactical criteria. |
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#4
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The Spitfire Mk IIa is modelled quite well for a +12 lbs boost version (even thought he boost shows as +8 lbs). Unfortunately the 109 is about 30-60 kph too slow at all altitudes.
That would explain why your 109 lost so much energy, it simply has too little power. Last edited by ICDP; 04-10-2011 at 06:56 PM. |
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#5
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#6
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I have rarely flown the 109 up to now but on some forums the rumor rans that the mixture ratio of the 109 is messed up and only has 0 or 100%. Could this be the reason why the performance is lacking? I could imagine that optimising the mixture also might be a factor for engine power ...
I am just guessing ... |
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#7
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Unfortunatly I don't have time to dig my teeth into this right now but here is the relevant ingame data.
Quick first impressions: 1. Cl max seems too low for both retracted and fully extended flaps. Should be 1.4 and 1.9 according to british testing, 1.3 and 1.62 ingame atm. 2. Turn time of 25 seconds corresponds with british testing but is significantly higher then the 18. something stated in the official Baubeschreibung. 3. 460 km/h on the deck corresponds with both german testing of Wrk.Nr. 1792 and swiss testing. The Baubeschreibung on the other hand gives 500 km/h. Any ideas where that difference might come from Kurfy? Anyway here are the cold hard facts: ; ; Messerschmitt Bf. 109 E-3 Flightmodel ; ; [Aircraft] ; Wingspan 9.867 m Length 8.738 m ; [Systems] ; Propulsion Engine Daimler-Benz DB601A Propellor VDM Generic Hydraulics Source Engine0 Pressure 100 bar Reservoir 8.5 pt Electrics Source Engine0 Voltage 25.1 V BatteryCapacity 54 Ah GeneratorOutput 650 sW at 2000 RPM LandingFlaps Mechanical Extends 25 sec Undercarriage Retractable Hydraulic Extends 5.0 sec Folds Outwards OperatesThrough 320 kmh EmergencySystem PneumaticDischarge SafetyLock Nil SpringsStiffness Main 0.6 Tail 0.6 MaxDragEquivalentS 0.7 m2 WheelBrakes Hydraulic Efficiency 1.5 Fenster Mechanical Opens 0.5 sec PitotHeater Electrical LeadingEdgeSlats Mechanical Automatic Move 0.1 sec ResponseRange 15.0 to 15.01 deg Hatch0 Mechanical Motion Type SwingingForward Time 2.0 sec Jettison Type Detachable Time 0.2 sec Hatch1 Mechanical Motion Type Nil Time 0.0 sec Jettison Type Detachable Time 0.2 sec ; [Controls] ; Aileron Slider Threshold 340 kmh Elevator Slider Threshold 400 kmh Rudder Slider Threshold 400 kmh AileronTrim Nil Default 0.017 ElevatorTrim Slider Range -0.5 to 0.5 Default 0.25 RudderTrim Nil Default 0.06 EngineThrottle Slider EnginePitch Slider EngineMagneto Switch M0 M1 M2 M12 EngineRadiator Rocker EngineOilRadiator Slider EngineMix Toggle EngineWEP PushButton EngineMix Toggle LandingFlaps Rocker Undercarriage Switch Up Neutral Down UndercarriageEmergency ExpendableSwitch Close Open WheelBrakes Slider Fenster Toggle AltimeterPinion Rocker Range 795 to 1040 Default 1000 mbar Puppet0PriPitLight Slider Puppet0SightLight Slider NavSecFrequency Rocker Timer0 CyclicSwitch AcemakerSight Dimmer Toggle TankSelector0 Toggle Off On Parked 0 Cruise 1 Selection 0 Flow FuelTank 1 to FuelTank 0 at 1 kg per second Selection 1 Flow FuelTank 1 to FuelTank 0 at 1 kg per second + FuelTank 0 to Engine 0 HydraulicsHandPump PushButton PitotHeater Toggle Timer0 CyclicSwitch Puppet0Hatch Toggle Close Open Selection 0 Closes Hatch 0 Selection 1 Opens Hatch 0 Puppet0Jettison ExpendableSwitch Off On Selection 1 Sheds Hatch 0 Hatch 1 ; [Instruments] ; EngineFuelPress Hydraulic Range 0 to 2 kgcm2 EngineOilPress Hydraulic Range 0 to 10 kgcm2 EngineOilTemp Electrical Range 0 to 120 C EngineWaterTemp Electrical Range 0 to 120 C EngineManifoldPress Mechanical Range 0.6 to 1.8 bar EngineRPM Electrical Range 600 to 3600 RPM EnginePropPitch Mechanical Range 0 to 12 hour Speedometer Mechanical Range 0 to 800 kmh Pitot Kollsman Altimeter Mechanical Dimension m MagneticCompass Mechanical JamAngle 90.0 deg SlipIndicator Mechanical Amplitude 12.0 deg TurnIndicator Mechanical Source Primary NominalTurnTime 2 min FuelReserve Electrical Range 0 to 400 litre ArtificialHorizon Mechanical Source Primary Pitch Range -45 to 45 deg Roll Range -181 to 181 deg GyroFeed Primary Electrical Secondary Nil ; [Mass] ; Empty 2060 kg TakeOff 2600 kg Fuel 300 kg FuelTanks Aluminum 100 kg Aluminum 200 kg FuelFillingOrder Tank 0 Tank 1 ; [Squares] ; Wing 16.4 m2 Aileron 1.1 m2 Flap 2.0 m2 Stabilizer 1.90 m2 Elevator 1.20 m2 Keel 1.00 m2 Rudder 1.10 m2 ; [Arm] ; Aileron 2.03 m Flap 2.04 m Stabilizer 5.15 m Keel 5.18 m Elevator 5.35 m Rudder 5.45 m Wing_In 1.25 m Wing_Mid 2.50 m Wing_Out 4.10 m GCenter 0.05 m GCenterZ 0.00 m GC_AOA_Shift 0.45 m GC_Flaps_Shift 0.20 m GC_Gear_Shift 0.05 m Wing_V 1.5 ; [Params] ; SpinCxLoss 0.06 SpinCyLoss 0.03 Vmin 170.0 kmh Vmax 470.0 kmh VmaxAllowed 750.0 kmh VmaxH 560.0 kmh at 4500.0 m VminFLAPS 130.0 kmh VmaxFLAPS 250.0 kmh Vz_climb 20.0 ms V_climb 270.0 kmh T_turn 25.0 sec V_turn 340.0 kmh K_max 13.0 FlapsMult 1.0 FlapsAngSh 10.0 RangeAbility 480 km SensYaw 0.6 SensPitch 0.7 SensRoll 0.32 ; [Polares] ; lineCyCoeff 0.091 AOAMinCx_Shift 0.2 Cy0_0 0.15 AOACritH_0 18.0 AOACritL_0 -15.0 CyCritH_0 1.3 CyCritL_0 -0.64417434 CxMin_0 0.0275 parabCxCoeff_0 6.2E-4 Cy0_1 0.55 AOACritH_1 17.0 AOACritL_1 -19.0 CyCritH_1 1.62 CyCritL_1 -0.7 CxMin_1 0.11 parabCxCoeff_1 8.7E-4 slatAOACritHInc 3.0 slatCyCritHInc 1.3 slatParabCxCoeffInc 0.8E-4 parabAngle 5.0 Decline 0.010 maxDistAng 35.0 ; ------------------------------------------------------------------------------ [DB601A] ; ------------------------------------------------------------------------------ General MaximalPower 1020 sPS DryWeight 590 kg Displacement 33.9 litre Cylinders 12 Bore 150 mm Stroke 160 mm Compression 6.9 Reliability Lifetime 100 h FailureProbability 0.0 RPM Minimal 500 Nominal 2200 Maximal 2326 Saturated 9999 Continuous 2326 Limiting 3000 Direction Right Intake Ramming 0.5 Exhaust PlainBackpipe Supercharger SingleStageHydroCoupling Efficiency 0.23 LimiterInput Manifold NominalPressure 1.35 bar ContinuousPressure 1.2 bar WEPPressure 1.45 bar NominalAltitude 4500 m Valvetrain Generic SlowRunningEfficiency 0.1 FuelPump Pushrod NominalPressure 3 bar at 500 RPM Carburettor GenericDirectInjection OrificeSlowFast 0.05 sec Dresser ThrottleDriven Input 0.75 to 1.0 Output 1.0 to 1.2 Starter Mechanical Ignition DualMagneto FrontEfficiency 0.57 Throttle Slider Translation Linear Bore 7.9 cm IdleOpening 0.05 WEPType ClockworkWEPModeToggle OperatingTime 1 min CooldownTime 10 sec Pitch Slider Angle Min 82 deg Max 26 deg WEP 40 deg Feathering Nil Mix Slider Multiplier Range 0.7 to 1.0 CylinderHead Material CastIron Temperatures Min 120 C Nominal 140 C Max 160 C AirRadiator Tunnel Louvre Nil FlowControl Nil Water Material Glycol Reserve 75 kg Temperatures Min 40 C Nominal 94 C Max 115 C WaterRadiator ThermostatedTunnel Pressurized Louvre Mechanical OpensAt 80 C FlowControl Manual ContinuousAt 0.25 MinimalDragAt 0.25 MaxDragEquivalentS 100 cm2 Oil Material Oil Reserve 8.5 gal Pressure 70 lbsqin at 600 RPM Temperatures Min 30 C Nominal 75 C Max 105 C OilRadiator ThermostatedTunnel Louvre Mechanical OpensAt 20 C FlowControl Manual ContinuousAt 0.25 MinimalDragAt 0.25 MaxDragEquivalentS 100 cm2 Propellor Reductor 0.64516129 Governor VariablePitch BladeAngleSpeed 1 degsec SoundName motor.merlin ; [Generic] ; Construction VisualModel VDM Diameter 3100 mm Blades 3 BladeBreadthK 0.8 Mass 140 kg AngleRange 26 deg to 82 deg DeIcing Nil lineCyCoeff 0.07 AOAMinCx_Shift 0.0 Cy0_0 0.0 AOACritH_0 24.0 AOACritL_0 -22.0 CyCritH_0 1.3 CyCritL_0 -0.8 CxMin_0 0.02 parabCxCoeff_0 3.8E-4 parabAngle 7.0 Decline 0.002 maxDistAng 40.0 ; Last edited by Hunin; 04-12-2011 at 01:37 AM. |
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#8
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#9
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@ICDP probably you're right!
__________________
![]() A whole generation of pilots learned to treasure the Spitfire for its delightful response to aerobatic manoeuvres and its handiness as a dogfighter. Iit is odd that they had continued to esteem these qualities over those of other fighters in spite of the fact that they were of only secondary importance tactically.Thus it is doubly ironic that the Spitfire’s reputation would habitually be established by reference to archaic, non-tactical criteria. |
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#10
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