[Vasya]

Делаю вот по этому документу.
http://www.wwiiaircraftperformance.o...cification.pdf
С фм, которые в моде не сходится по весу, меняю почти всё.

[Aircraft]
  Type 1
  Crew 1
  Wingspan 13.06     #41 feet = 12.496 8 meter
  Length 10.302   #33.8 feet = 10.302 24 meter
  Seaplane 0
  Canard 0
  Jet 0
  JetHiV 0
[Mass]
  Empty 4192.1    
  TakeOff 6136.65                       
  Oil 80.0
  Fuel 1045.0
  Nitro 46.0
[Controls]
  CAileron 1
  CAileronTrim 1
  CElevator 1
  CElevatorTrim 1
  CRudder 1
  CRudderTrim 1
  CFlap 1
  CFlapPos 3
  CDiveBrake 1
  CInterceptor 0
  CEngine 1
  CVectoredThrust 0
  CUndercarriage 1
  CLockTailwheel 1
  CStabilizer 1
  CArrestorHook 1
  CWingFold 1
  CCockpitDoor 1  
  CockpitDoorPeriod 3.0
  CAileronThreshold 440.0
  CRudderThreshold 400.0
  CElevatorThreshold 400.0
  DefaultAileronTrim -0.006
  DefaultElevatorTrim -0.0125
  DefaultRudderTrim 0.066
  GearPeriod 10.0
  WingPeriod 10.0
  AirbrakePeriod 10.0
[Squares]
  Wing 29.17155456
  Aileron 1.681545024
  Flap 3.38167
  Stabilizer 3.3445
  Elevator 2.034576576
  Keel 0.83612736
  Rudder 1.20774
  Wing_In 4.58577728
  Wing_Mid 5.0
  Wing_Out 5.0
  AirbrakeCxS 0.0
[Arm]
  Aileron 4.16
  Flap 1.67  
  Keel 4.6
  Rudder 5.45  
  Stabilizer 5.4
  Elevator 5.80
  Wing_In 1.65
  Wing_Mid 4.16
  Wing_Out 5.41
  Wing_V 8.5
  GCenter 0.080
  GCenterZ 0.00
  GC_AOA_Shift 0.545
  GC_Flaps_Shift 0.20
  GC_Gear_Shift 0.06
[Toughness]
  AroneL 50
  AroneR 50
  CF 600
  Engine1 350
  Engine2 350
  Engine3 350
  Engine4 350
  GearL2 200
  GearR2 200
  Keel1 100
  Keel2 100
  Nose 100
  Oil 50
  Rudder1 100
  Rudder2 100
  StabL 100
  StabR 100
  Tail1 200
  Tail2 200
  Turret1B 100
  Turret2B 100
  Turret3B 100
  Turret4B 100
  Turret5B 100
  Turret6B 100
  VatorL 80
  VatorR 80
  WingLIn 200
  WingLMid 150
  WingLOut 100
  WingRIn 200
  WingRMid 150
  WingROut 100
  Flap01 50
  Flap02 50
  Flap03 50
  Flap04 50
[Engine]
  Engine0Family PrattWhitney_R-2000_Series(MOD):F4ULate_FM
  Engine0SubModel Pratt-Whitney-R-2800-18W/DFL/F4U-4
[Gear]
  H 1.614541
  Pitch 11.842
  SinkFactor 1200.0
  SpringsStiffness 0.7
  TailStiffness 0.6
[Params]
  CriticalAOA 16.00
  CriticalCy 01.50
  CxCurvature 00.80
  CxStraightness 00.13
  CriticalAOAFlap 18.00   
  CriticalCyFlap 01.95
  SpinTailAlpha 17.00
  SpinCxLoss 0.015
  SpinCyLoss 0.01
  Vyfac 0.95
  Tfac 0.98
  Vmin 160.0
  Vmax 528.0
  VmaxAllowed 800.0
  VmaxH 720.0
  HofVmax 9000.0
  VminFLAPS 135.0
  VmaxFLAPS 260.0
  Vz_climb 14.0
  V_climb 270.0
  T_turn 30.0
  V_turn 350.0
  K_max 12.0
  Cy0_max 0.15
  FlapsMult 1.0
  FlapsAngSh 4.0
  G_class_coeff 25.0
  G_class 12.0
  ReferenceWeight 39.7
  Range 1500.0
  CruiseSpeed 310.0
  SensYaw 0.50
  SensPitch 0.403
  SensRoll 0.33
[Polares]
  lineCyCoeff 0.0705
  AOAMinCx_Shift 0.8
  Cy0_0  0.1912             
  AOACritH_0 18.0
  AOACritL_0 -15.0
  CyCritH_0 1.3077
  CyCritL_0 -0.83
  CxMin_0 0.0190
  parabCxCoeff_0 4.2E-4
  Cy0_1 0.8912              // 0.6912
  AOACritH_1 16.0
  AOACritL_1 -25.3
  CyCritH_1 1.70
  CyCritL_1 -0.80
  CxMin_1 0.08142857143
  parabCxCoeff_1 5.8E-4
  parabAngle 5.0
  Decline 0.010
  maxDistAng 35.0
  draw_graphs 0
  mc3 -17.274,-11.427,-14.994,-8.5414,-9.8375,-3.3144,1.1456,-4.9505
  mc4 35.874,28.861,81.767,175.28,74.334,41.96,21.532,61.433
  mm 0.682,0.742,0.777,0.777,0.762,0.703,0.648,0.583
  mz 0.288,0.274,0.164,0.099,0.136,0.149,0.154,0.117
[SOUND]
  Engine Std