; ================================================== ============================
; A6M2-21 Flightmodel - v 1.0 - COPY OF A6M2 BUT THE HOOK CONTROL
; ================================================== ============================
; ================================================== ============================
[Aircraft]
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Type = 1
Crew = 1
Wingspan = 9.6
Length = 8.71
Seaplane = 0
Canard = 0
Jet = 0
JetHiV = 0
; ================================================== ============================
[Mass]
; ================================================== ============================
Empty = 1820.0
TakeOff = 2433.7
Oil = 30.0
Fuel = 400.0
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[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 = 0
CArrestorHook = 1
CWingFold = 1
CCockpitDoor = 1
CockpitDoorPeriod = 1.5
CAileronThreshold = 280.0
CRudderThreshold = 320.0
CElevatorThreshold = 360.0
DefaultAileronTrim =0.008
DefaultElevatorTrim =-0.09
DefaultRudderTrim =0.065
; ================================================== ============================
[Squares]
; ================================================== ============================
Wing = 22.12
Aileron = 1.5
Flap = 0.01
Stabilizer = 1.90
Elevator = 1.10
Keel = 0.90
Rudder = 1.10
Wing_In = 4.0
Wing_Mid = 4.0
Wing_Out = 3.06
AirbrakeCxS = 0.0
; ================================================== ============================
[Arm]
; ================================================== ============================
Aileron = 3.84
Flap = 1.70
Stabilizer = 5.10
Keel = 5.40
Elevator = 5.48
Rudder = 5.72
Wing_In = 1.0
Wing_Mid = 2.28
Wing_Out = 3.98
Wing_V = 1.5
GCenter = 0.05
GCenterZ = 0.00
GC_AOA_Shift = 0.40
GC_Flaps_Shift = 0.15
GC_Gear_Shift = 0.05
; ================================================== ============================
[Toughness]
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AroneL = 40
AroneR = 40
CF = 300
Engine1 = 200
Engine2 = 200
Engine3 = 200
Engine4 = 200
GearL2 = 300
GearR2 = 300
Keel1 = 50
Keel2 = 50
Nose = 50
Oil = 50
Rudder1 = 50
Rudder2 = 50
StabL = 50
StabR = 50
Tail1 = 100
Tail2 = 100
Turret1B = 100
Turret2B = 100
Turret3B = 100
Turret4B = 100
Turret5B = 100
Turret6B = 100
VatorL = 40
VatorR = 40
WingLIn = 100
WingLMid = 75
WingLOut = 60
WingRIn = 100
WingRMid = 75
WingROut = 60
Flap01 = 50
Flap02 = 50
Flap03 = 50
Flap04 = 50
; ================================================== ============================
[Engine]
; ================================================== ============================
Engine0Family=Nakajima
Engine0SubModel=Sakae-12
; ================================================== ============================
[Gear]
; ================================================== ============================
H = 1.593106
Pitch = 12.089
SinkFactor = 700.0
SpringsStiffness = 0.8
TailStiffness = 0.3
; ================================================== ============================
[Params]
; ================================================== ============================
CriticalAOA = 20.00
CriticalCy = 01.80
CxCurvature = 00.80
CxStraightness = 00.20
CriticalAOAFlap = 22.00
CriticalCyFlap = 02.10
SpinTailAlpha = 17.00
;LeadingEdgeSlats = 0 yet unused
SpinCxLoss = 0.06
SpinCyLoss = 0.02
Vyfac = 0.90
Tfac = 1.02
Vmin = 150.0
;462.0
Vmax = 462.0
VmaxAllowed = 630.0
VmaxH = 555.0
HofVmax = 6000.0
VminFLAPS = 125.0
VmaxFLAPS = 250.0
Vz_climb = 20.0
V_climb = 220.0
T_turn = 15.0
V_turn = 290.0
K_max = 14.0
Cy0_max = 0.15
FlapsMult = 1.0
FlapsAngSh = 12.0
Range = 1400.0
CruiseSpeed = 340.0
SensYaw = 0.44
SensPitch = 0.66
SensRoll = 0.35
; ================================================== ============================
[Polares]
; ================================================== ============================
lineCyCoeff = 0.085
AOAMinCx_Shift = 0.0
Cy0_0 = 0.14
AOACritH_0 = 17.0
AOACritL_0 = -15.0
CyCritH_0 = 1.2058289
CyCritL_0 = -0.81926084
CxMin_0 = 0.0245
parabCxCoeff_0 = 5.0E-4
Cy0_1 = 0.6668992
AOACritH_1 = 15.5
AOACritL_1 = -20.0
CyCritH_1 = 1.5688039
CyCritL_1 = -0.8
CxMin_1 = 0.08129228
parabCxCoeff_1 = 6.0E-4
parabAngle = 4.0
Decline = 0.006
maxDistAng = 40.0
draw_graphs = 0
; ================================================== ============================
[SOUND]
; ================================================== ============================
Engine = fw_190
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