[Vasya]

ФМ для Гастава-6 с новым капотом без шишек
и с компрессором от DB-603.

BF-109G-6MOD-AS.fmd

[Aircraft]
  Type 1
  Crew 1
  Wingspan 9.924
  Length 8.94
  Seaplane 0
  Canard 0
  Jet 0
  JetHiV 0
[Mass]
  Empty 2704.0
  TakeOff 3221.0
  Oil 50.0
  Fuel 300.0
//  Nitro 70.0
[Controls]
  CAileron 1
  CAileronTrim 0
  CElevator 1
  CElevatorTrim 1
  CRudder 1
  CRudderTrim 0
  CFlap 1
  CFlapPos 3
  CDiveBrake 0
  CInterceptor 0
  CEngine 1
  CVectoredThrust 0
  CUndercarriage 1
  CLockTailwheel 1
  CStabilizer 1
  CArrestorHook 0
  CWingFold 0
  CCockpitDoor 1
  OnlineCockpitDoor 0
  CockpitDoorPeriod 2.0
  CAileronThreshold 460.0
  CRudderThreshold 550.0
  CElevatorThreshold 500.0
  DefaultAileronTrim 0.0074
  DefaultElevatorTrim -0.00
  DefaultRudderTrim 0.0578
[Squares]
  Wing 16.16
  Aileron 1.02
  Flap 2.00
  Stabilizer 1.90
  Elevator 1.20
  Keel 0.74
  Rudder 1.14
  Wing_In 3.00
  Wing_Mid 2.50
  Wing_Out 2.605
  AirbrakeCxS 0.00
[Arm]
  Aileron 4.03
  Flap 2.04
  Stabilizer 5.15
  Keel 5.18
  Elevator 5.35
  Rudder 5.45
  Wing_In 1.25
  Wing_Mid 2.50
  Wing_Out 4.10
  Wing_V 1.5
  GCenter 0.05
  GCenterZ 0.00
  GC_AOA_Shift 0.45
  GC_Flaps_Shift 0.20
  GC_Gear_Shift -0.45
[Toughness]
  AroneL 100
  AroneR 100
  CF 500
  Engine1 150
  Engine2 150
  Engine3 150
  Engine4 150
  GearL2 300
  GearR2 300
  Keel1 100
  Keel2 100
  Nose 100
  Oil 200
  Rudder1 100
  Rudder2 100
  StabL 100
  StabR 100
  Tail1 100
  Tail2 100
  Turret1 100
  Turret2 100
  Turret3 100
  Turret4 100
  Turret5 100
  Turret6 100
  VatorL 100
  VatorR 100
  WingLIn 100
  WingLMid 100
  WingLOut 100
  WingRIn 100
  WingRMid 100
  WingROut 100
  Flap01 100
  Flap02 100
  Flap03 100
  Flap04 100
[Engine]
  Engine0Family DB-601E-605DBC-HARTMANN:BF_109G_6_HARTMANN
  Engine0SubModel DB-605AS/C-3/MOD/NEW_REDUCTOR/BF-109G-6AS
[Gear]
  H 1.663372
  Pitch 12.850
  SinkFactor 800.0
  SpringsStiffness 0.6
  TailStiffness 0.5
[Params]
  CriticalAOA 21.00
  CriticalCy 01.82
  CxCurvature 00.80
  CxStraightness 00.00
  CriticalAOAFlap 21.00
  CriticalCyFlap 02.10
  SpinTailAlpha 17.00
  SpinCxLoss 0.06
  SpinCyLoss 0.03
  Vmin 160.0
  Vmax 535.0
  VmaxAllowed 860.0
  VmaxH 640.0
  HofVmax 6000.0
  VminFLAPS 135.0
  VmaxFLAPS 255.0
  VminFLAPS 140.0
  VmaxFLAPS 250.0
  Vz_climb 26.0
  V_climb 280.0
  T_turn 20.0
  V_turn 340.0
  K_max 15.0
  Cyo_max 0.15
  FlapsMult 1.0
  FlapsAngSh 3.0
  G_class_coeff 25.0
  G_class 12.0
  ReferenceWeight -50.0
  Range 600.0
  CruiseSpeed 350.0
  SensYaw 0.47
  SensPitch 0.68
  SensRoll 0.34
[Polares]
  lineCyCoeff 0.095
  AOAMinCx_Shift 0.2
  Cy0_0 0.15
  AOACritH_0 21.0
  AOACritL_0 -15.0
  CyCritH_0 1.386
  CyCritL_0 -0.89
  CxMin_0 0.0240
  parabCxCoeff_0 5.6E-4
  Cy0_1 0.63184977
  AOACritH_1 17.0
  AOACritL_1 -24.5
  CyCritH_1 1.64422
  CyCritL_1 -0.860845485
  CxMin_1 0.093913
  parabCxCoeff_1 8.2E-4
  parabAngle 5.0
  Decline 0.010
  maxDistAng 38.0
  draw_graphs 0
  mc3 -15.484,-5.4215,-14.124,-36.716,20.943,-35.766,14.986,-14.349
  mc4 38.145,14.707,50.771,282.28,212.08,256.62,-67.576,81.767
  mm 0.621,0.709,0.752,0.754,0.73,0.711,0.676,0.603
  mz 0.241,0.286,0.202,0.108,0.061,0.072,0.092,0.159
[SOUND]
  Engine bf_109
  Start e_start
  Turbine bf_turbo
  FeedType HYDRAULIC

На 75 проц. фм близка к дефолту.
Изменения:
реальный вес.,
триммер руля высоты на ноль.,
другое аэродинамическое качество крыла.,
снижено сопротивление для соответствия ттх реальным прототипам.
Надеюсь, что по ттх уложился на 95 проц.