[Vasya]

ФМ для Яка предварительно пока такая.

[Aircraft]
Type 1
Crew 1
Wingspan 7.30
Length 5.75
Seaplane 0
Canard 0
Jet 0
JetHiV 0
[Mass]
Empty 429.0
TakeOff 600.0
Oil 13.5
Fuel 62.5
[Controls]
CAileron 1
CAileronTrim 0
CElevator 1
CElevatorTrim 1
CRudder 1
CRudderTrim 1
CFlap 0
CFlapPos 0
CDiveBrake 0
CInterceptor 0
CEngine 1
CVectoredThrust 0
CUndercarriage 0
CLockTailwheel 1
CStabilizer 0
CArrestorHook 0
CWingFold 0
CCockpitDoor 1
CAileronThreshold 320.0
CRudderThreshold 320.0
CElevatorThreshold 360.0
DefaultAileronTrim 0.008
DefaultElevatorTrim 0.05
DefaultRudderTrim 0.044
[Squares]
Wing 9.58
Aileron 0.354
Flap 0.01
Stabilizer 0.6
Elevator 0.45
Keel 0.32
Rudder 0.58
Wing_In 0.01
Wing_Mid 2.45
Wing_Out 2.33 // 2.08
AirbrakeCxS 0.0
[Arm]
Aileron 3.4
Flap 1.0
Stabilizer 3.4
Keel 3.25
Elevator 3.59
Rudder 3.69
Wing_In 1.0
Wing_Mid 1.97
Wing_Out 3.72
Wing_V 1.9
GCenter -0.072
GCenterZ 0.00
GC_AOA_Shift 0.40
GC_Flaps_Shift 0.15
GC_Gear_Shift -0.60
[Toughness]
AroneL 40
AroneR 40
CF 300
Engine1 100
Engine2 150
Engine3 150
Engine4 150
GearL2 150
GearR2 150
Keel1 50
Keel2 50
Nose 50
Oil 50
Rudder1 50
Rudder2 50
StabL 50
StabR 50
Tail1 50
Tail2 50
Turret1B 100
Turret2B 100
Turret3B 100
Turret4B 100
Turret5B 100
Turret6B 100
VatorL 50
VatorR 50
WingLIn 90
WingLMid 75
WingLOut 50
WingRIn 90
WingRMid 75
WingROut 50
Flap01 50
Flap02 50
Flap03 50
Flap04 50
[Engine]
Engine0Family M-11_Series(MOD):UT1_FM
Engine0SubModel M-11E/150HP
[Gear]
H 0.7
Pitch 14.754
SinkFactor 1000.0
[Params]
CriticalAOA 16.00
CriticalCy 01.46
CxCurvature 00.60
CxStraightness 00.07
CriticalAOAFlap 17.00
CriticalCyFlap 01.65
SpinTailAlpha 17.00
SpinCxLoss 0.07
SpinCyLoss 0.02
Vmin 80.0
Vmax 240.0
VmaxAllowed 450.0
VmaxH 257.0
HofVmax 4000.0
VminFLAPS 100.0
VmaxFLAPS 220.0
Vz_climb 6.8
V_climb 170.0
T_turn 13.0
V_turn 200.0
K_max 10.0
Cy0_max 0.15
G_class_coeff 20.0
G_class 12.0
ReferenceWeight 20.0
Range 670.0
CruiseSpeed 400.0
SensYaw 0.42
SensPitch 0.60
SensRoll 0.28
[Polares]
lineCyCoeff 0.090
AOAMinCx_Shift 0.65
Cy0_0 0.20
AOACritH_0 17.5
AOACritL_0 -13.5
CyCritH_0 1.18
CyCritL_0 -0.6941
CxMin_0 0.035
parabCxCoeff_0 3.9E-4
Cy0_1 0.20
AOACritH_1 17.5
AOACritL_1 -13.5
CyCritH_1 1.18
CyCritL_1 -0.6941
CxMin_1 0.035
parabCxCoeff_1 3.9E-4
parabAngle 4.0
Decline 0.0010
maxDistAng 30.0
draw_graphs 0
mc3 -19.824,-5.7687,-4.6966,-18.391,-6.7342,-17.841,-56.258,-6.6673
mc4 41.96,13.37,11.049,95.584,74.334,192.8,454.62,31.5 25
mm 0.607,0.697,0.788,0.748,0.734,0.699,0.652,0.616
mz 0.263,0.304,0.318,0.158,0.142,0.097,0.087,0.213
[SOUND]
Engine Std

Не нашёл в интернете вес топлива.
Какая у него должна быть максималка у земли с мотором 115 лошадей?
Смущает V - 1.9 крила.
На чертежах/картинках спереди крыло не более загнуто вверх, чем Ишак.
Ещё нужно провести тест на сопротивление и скороподъёмность.