[BlackBerry]

Bf-109-G2
[Mass] kg
Empty 2320.0
TakeOff 2830.0

[Squares] m^2
Wing 16.16
Aileron 1.02
Flap 2.00
Stabilizer 1.90
Elevator 1.20
Keel 0.70
Rudder 1.10

[Polares]
lineCyCoeff 0.094
Cy0_0 0.15.............................................. .
AOACritH_0 21.0............................................
AOACritL_0 -16.0...........................................
CyCritH_0 1.48.............................................. .
CyCritL_0 -1.0230048.....................................
CxMin_0 0.027............................................. ..
parabCxCoeff_0 6.7E-4....................................

Spitfire.LF.IXC
[Mass]
Empty 2650.0
TakeOff 3300.0

[Squares]
Wing 19.0
Aileron 1.32
Flap 2.125
Stabilizer 1.90
Elevator 1.20
Keel 0.85
Rudder 1.10

[Polares]
lineCyCoeff 0.092
AOAMinCx_Shift 0.0
Cy0_0 0.1
AOACritH_0 16.0
AOACritL_0 -17.0
CyCritH_0 1.4
CyCritL_0 -0.7
CxMin_0 0.0232
parabCxCoeff_0 5.4E-4


P-47D-27
[Mass]
Empty 4630.0
TakeOff 6583.0

[Squares]
Wing 25.87
Aileron 1.45
Flap 2.76
Stabilizer 3.50
Elevator 2.05
Keel 1.30
Rudder 1.10

[Polares]
lineCyCoeff 0.092
AOAMinCx_Shift 0.9
Cy0_0 0.17
AOACritH_0 16.0
AOACritL_0 -15.0
CyCritH_0 1.25
CyCritL_0 -0.8
CxMin_0 0.0256
parabCxCoeff_0 4.8E-4


Bf-109G-2 = 0.027 * 16.16 = 0.43632
Spitfire.LF.IXC = 0.0232 * 19.0 = 0.4408
P-47D-27 = 0.0256 * 25.87 = 0.662272


Bf-109G-2
0.43632/2830 = 1.5417667844522968197879858657244e-4

Spitfire.LF.IXC
0.4408/3300 = 1.3357575757575757575757575757576e-4

P-47D-27
0.662272/6583 = 1.0060337232264924806319307306699e-4