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#1
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![]() Quote:
I have a question, does bf109g6as outdive spitfire IX or fw190A8 during the initial phase in 4.11m? |
#2
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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 |
#3
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![]() Quote:
Excess thrust......not the same! ![]() |
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