Ещё раз пристально посмотрел на каждую цифру в фм Мессеров.
Думаю вот так будет самый оптимальный вариант.
Например Густав-6 поздний.
Код:
[Aircraft]
Type 1
Crew 1
Wingspan 9.924
Length 8.94
Seaplane 0
Canard 0
Jet 0
JetHiV 0
[Mass]
Empty 2679.0
TakeOff 3196.0
Oil 50.0
Fuel 300.0
[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 0.0085
DefaultElevatorTrim -0.00
DefaultRudderTrim 0.0553
[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 5.5
GCenter 0.1
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-NEW:BF_109_HARTMANN_NEW
Engine0SubModel DB-605A/MOD/NEW_REDUCTOR/BF-109G-4-LATE
[Gear]
H 1.663372
Pitch 12.850
SinkFactor 800.0
SpringsStiffness 0.6
TailStiffness 0.5
[Params]
CriticalAOA 20.00 // дефолт Bf-109G-14.fmd
CriticalCy 01.82 // дефолт Bf-109G-14.fmd
CxCurvature 00.90 // дефолт Bf-109F-4.fmd
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 14.0
Cyo_max 0.15
FlapsMult 1.0
FlapsAngSh 3.0
G_class_coeff 25.0
G_class 12.0
ReferenceWeight -25.0
Range 600.0
CruiseSpeed 350.0
SensYaw 0.47
SensPitch 0.68
SensRoll 0.34
[Polares]
lineCyCoeff 0.096 // дефолт Bf-109F-4.fmd
AOAMinCx_Shift 0.6 // дефолт Bf-109F-4.fmd
Cy0_0 0.15 // дефолт Bf-109G-14.fmd
AOACritH_0 21.00 // дефолт Bf-109G-14.fmd
AOACritL_0 -15.00 // дефолт Bf-109G-14.fmd
CyCritH_0 1.2875855 // расчёт для Су 0.7
CyCritL_0 -0.89 // расчёт для Су -0.26
CxMin_0 0.02461 // расчёт для параболы Cx 0.18 + 2 ящика водо-радиаторов
parabCxCoeff_0 5.4E-4 // дефолт Bf-109F-4.fmd
Cy0_1 0.63184977 // дефолт Bf-109G-14.fmd
AOACritH_1 17.0 // дефолт Bf-109G-14.fmd
AOACritL_1 -27.0 // приблизительный посадочный критический угол
CyCritH_1 1.67 // среднее значение между дефолтом - 0.62-0.72
CyCritL_1 -0.721605 // 162:70=2.314285(коэфициент для 1.67)
CxMin_1 0.0963 // приблизительный Сх для соотношения(0.12376) площади флап и крыла
parabCxCoeff_1 8.2E-4 // дефолт Bf-109F-4.fmd
parabAngle 5.0 // парабола для угла -15.00
Decline 0.010
maxDistAng 35.0
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
Тут:
http://forum.aviaskins.com/showpost....postcount=9025