Хотел поставить себе Р-38 с Дабл-Уосп, а зацепился за Спитфайр.
Нашлась книженция по аэродинамике Спитфайра.
https://www.cfdsupport.com/download/...Case-Study.pdf
Насколько понял - перевёл данные графиков в иловский формат.
Ближе всего к этим графикам были старые фм из патча 4.09.
Имею в виду полётную часть поляры.
Вот так
перенёс цифры с графиков.
Spitfire-F-VA-M45-09.fmd
(Собранный вариант фм на 10-07-2021 года)
Код:
[Aircraft]
Type 1
Crew 1
Wingspan 11.23
Length 9.12
Seaplane 0
Canard 0
Jet 0
JetHiV 0
[Mass]
Empty 2250.0
TakeOff 2829
Oil 25.0
Fuel 280.0
[Controls]
CAileron 1
CAileronTrim 0
CElevator 1
CElevatorTrim 1
CRudder 1
CRudderTrim 1
CFlap 1
CFlapPos 2
CDiveBrake 0
CInterceptor 0
CEngine 1
CVectoredThrust 0
CUndercarriage 1
CLockTailwheel 1
CStabilizer 1
CArrestorHook 0
CWingFold 0
CCockpitDoor 0
CAileronThreshold 280.0
CRudderThreshold 420.0
CElevatorThreshold 420.0
DefaultAileronTrim 0.005
DefaultElevatorTrim -0.00
DefaultRudderTrim 0.0445
[Squares]
Wing 22.48
Aileron 1.74
Flap 1.46
Stabilizer 1.90
Elevator 1.16
Keel 0.85
Rudder 0.80
Wing_In 4.0
Wing_Mid 3.84
Wing_Out 3.4
AirbrakeCxS 0.0
[Arm]
Aileron 3.8
Flap 1.3
Stabilizer 4.3
Keel 4.4
Elevator 4.8
Rudder 5.1
Wing_In 1.2
Wing_Mid 2.6
Wing_Out 4.3
Wing_V 5.0
GCenter 0.10
GCenterZ 0.00
GC_AOA_Shift 0.50
GC_Flaps_Shift 0.20
GC_Gear_Shift -0.05
[Toughness]
AroneL 50
AroneR 50
CF 400
Engine1 70
Engine2 70
Engine3 70
Engine4 70
GearL2 150
GearR2 150
Keel1 70
Keel2 70
Nose 100
Oil 70
Rudder1 50
Rudder2 50
StabL 70
StabR 70
Tail1 100
Tail2 100
Turret1B 100
Turret2B 100
Turret3B 100
Turret4B 100
Turret5B 100
Turret6B 100
VatorL 50
VatorR 50
WingLIn 100
WingLMid 90
WingLOut 50
WingRIn 100
WingRMid 90
WingROut 50
Flap01 50
Flap02 50
Flap03 50
Flap04 50
[Engine]
Engine0Family Rolls-Royce(Spitfire_Pack):Spitfire_Pack-FM
Engine0SubModel Merlin-45/9lbs/NEW
[Gear]
H 1.614541
Pitch 11.842
SinkFactor 1000.0
SpringsStiffness 0.6
TailStiffness 0.5
[Params]
CriticalAOA 16.80
CriticalCy 01.40
CxCurvature 00.90
CxStraightness 00.08
CriticalAOAFlap 15.00
CriticalCyFlap 01.55
SpinTailAlpha 13.00
SpinCxLoss 0.032
SpinCyLoss 0.012
Vyfac 1.0
Tfac 1.0
Vmin 142.0
Vmax 474.0
VmaxAllowed 720.0
VmaxH 576.0
HofVmax 6100.0
VminFLAPS 129.0
VmaxFLAPS 250.0
Vz_climb 16.0
V_climb 250.0
T_turn 18.8
V_turn 235.0
K_max 12.6
Cy0_max 0.14
FlapsMult 0.9
FlapsAngSh 10.0
G_class_coeff 20.0
G_class 12.0
Range 726.0
CruiseSpeed 300.0
SensYaw 0.52
SensPitch 0.60
SensRoll 0.36
[Polares]
lineCyCoeff 0.09125 // 0.29:5*=0.058 / 0.73:8*=0.09125
AOAMinCx_Shift 0.81
Cy0_0 0.10 // Cy0 0.10 = 1* / Cy0 0.20 = +2*
AOACritH_0 16.8 // AOACrit 14.0* = CyCrit 1.2775
AOACritL_0 -15.0
CyCritH_0 1.366 // CyCrit 1.366 = AOACrit 16.8*
CyCritL_0 -0.98
CxMin_0 0.018375 // Cx 0.018375 - по данным продувки
parabCxCoeff_0 5.3E-4
Cy0_1 0.59
AOACritH_1 15.0
AOACritL_1 -20.0
CyCritH_1 1.55
CyCritL_1 -0.63
CxMin_1 0.077175 // 0.09576 при CxMin_0 0.0228
parabCxCoeff_1 6.0E-4
parabAngle 4.0
Decline 0.10
maxDistAng 45.0
draw_graphs 0
mc3 -26.464,-13.497,-12.705,-72.354,-66.117,-36.136,-60.497,-17.971
mc4 59.294,34.677,38.145,665.61,454.62,233.29,375.72,175.28
mm 0.644,0.714,0.785,0.781,0.785,0.732,0.679,0.613
mz 0.251,0.254,0.239,0.086,0.09,0.11,0.097,0.09
[SOUND]
Engine Std
Некоторые цифры брал из поляры Spitfire-F-II-M12-12.fmd
из САСовского баттонза - выделил жирным.
А вот так у меня было раньше - чисто мои фантазии порысовать цифрами.
Код:
[Polares]
lineCyCoeff 0.06159
AOAMinCx_Shift 0.88
Cy0_0 0.17
AOACritH_0 16.0
AOACritL_0 -14.0
CyCritH_0 1.34
CyCritL_0 -0.925
CxMin_0 0.0229
parabCxCoeff_0 4.5E-4
Cy0_1 0.97
AOACritH_1 14.0
AOACritL_1 -19.0
CyCritH_1 1.65
CyCritL_1 -0.63
CxMin_1 0.095722
parabCxCoeff_1 5.2E-4
parabAngle 5.0
Decline 0.010
maxDistAng 50.0
draw_graphs 0
Некоторые мои предположения близки
к графикам, Cx -дефолт.