WORTMANN FX M2 AIRFOIL (fxm2-il)
WORTMANN FX M2 AIRFOIL - Wortmann FX M2 airfoil
| Details | Dat file | Parser | |
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(fxm2-il) WORTMANN FX M2 AIRFOIL Wortmann FX M2 airfoil Max thickness 8.4% at 19.6% chord. Max camber 4.8% at 30.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
WORTMANN FX M2 AIRFOIL
49. 49.
0.000000 0.000000
0.001070 0.009680
0.004280 0.017740
0.009610 0.026500
0.017040 0.035190
0.026530 0.044500
0.038060 0.052020
0.051560 0.060500
0.066990 0.066550
0.084270 0.072500
0.103320 0.077390
0.124080 0.081500
0.146450 0.084210
0.170330 0.086000
0.195620 0.087500
0.222210 0.087190
0.250000 0.088090
0.278860 0.086800
0.308660 0.086500
0.339280 0.084370
0.370590 0.083060
0.402450 0.080260
0.434740 0.078220
0.467300 0.074930
0.500000 0.072280
0.532700 0.068650
0.565260 0.065610
0.597550 0.061820
0.629410 0.058580
0.660720 0.054710
0.691340 0.051280
0.721140 0.047370
0.750000 0.043810
0.777790 0.039930
0.804380 0.036250
0.829670 0.032390
0.853550 0.028720
0.875920 0.024990
0.896680 0.021460
0.915730 0.018020
0.933010 0.014820
0.948440 0.011760
0.961940 0.008940
0.973470 0.006320
0.982960 0.004060
0.990390 0.002270
0.995720 0.000970
0.998930 0.000240
1.000000 0.000000
0.000000 0.000000
0.001070 -0.003500
0.004280 -0.006800
0.009610 -0.009070
0.017040 -0.009800
0.026530 -0.008800
0.038060 -0.007000
0.051560 -0.005800
0.066990 -0.004430
0.084270 -0.002500
0.103320 -0.001450
0.124080 0.000100
0.146450 0.001500
0.170330 0.002800
0.195620 0.003500
0.222210 0.004730
0.250000 0.006940
0.278860 0.007310
0.308660 0.009190
0.339280 0.009500
0.370590 0.011100
0.402450 0.011310
0.434740 0.012600
0.467300 0.012720
0.500000 0.013700
0.532700 0.013710
0.565260 0.014440
0.597550 0.014340
0.629410 0.014780
0.660720 0.014550
0.691340 0.014730
0.721140 0.014380
0.750000 0.014240
0.777790 0.013560
0.804380 0.013020
0.829670 0.012170
0.853550 0.011440
0.875920 0.010480
0.896680 0.009590
0.915730 0.008510
0.933010 0.007460
0.948440 0.006310
0.961940 0.005160
0.973470 0.003910
0.982960 0.002680
0.990390 0.001600
0.995720 0.000730
0.998930 0.000200
1.000000 0.000000
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Polars for WORTMANN FX M2 AIRFOIL (fxm2-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fxm2-il | 50,000 | 9 | 31.6 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxm2-il | 50,000 | 5 | 35.7 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxm2-il | 100,000 | 9 | 45.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxm2-il | 100,000 | 5 | 50.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxm2-il | 200,000 | 9 | 65.1 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxm2-il | 200,000 | 5 | 68.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxm2-il | 500,000 | 9 | 94.4 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxm2-il | 500,000 | 5 | 86.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxm2-il | 1,000,000 | 9 | 103.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxm2-il | 1,000,000 | 5 | 100.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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