FX 83-W-108 (fx83w108-il)
FX 83-W-108 - Wortmann FX 83-W-108 airfoil for use on wind turbines (W)
| Details | Dat file | Parser | |
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(fx83w108-il) FX 83-W-108 Wortmann FX 83-W-108 airfoil for use on wind turbines (W) Max thickness 10.9% at 30.9% chord. Max camber 4.2% at 53.3% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
FX 83-W-108 1.00000 0.00000 0.99893 0.00106 0.99572 0.00205 0.99039 0.00367 0.98296 0.00585 0.97347 0.00855 0.96194 0.01168 0.94844 0.01515 0.93301 0.01888 0.91573 0.02293 0.89668 0.02728 0.87592 0.03197 0.85355 0.03690 0.82967 0.04206 0.80438 0.04735 0.77779 0.05279 0.75000 0.05820 0.72114 0.06358 0.69134 0.06875 0.66072 0.07366 0.62941 0.07809 0.59755 0.08200 0.56526 0.08526 0.53270 0.08784 0.50000 0.08974 0.46730 0.09093 0.43474 0.09142 0.40245 0.09128 0.37059 0.09045 0.33928 0.08903 0.30866 0.08703 0.27886 0.08453 0.25000 0.08156 0.22221 0.07816 0.19562 0.07436 0.17033 0.07019 0.14645 0.06571 0.12408 0.06092 0.10332 0.05590 0.08427 0.05066 0.06699 0.04530 0.05156 0.03975 0.03806 0.03416 0.02653 0.02843 0.01704 0.02279 0.00961 0.01704 0.00428 0.01135 0.00107 0.00550 0.00000 0.00000 0.00107 -0.00420 0.00428 -0.00876 0.00961 -0.01252 0.01704 -0.01574 0.02653 -0.01841 0.03806 -0.02073 0.05156 -0.02267 0.06699 -0.02437 0.08427 -0.02577 0.10332 -0.02687 0.12408 -0.02762 0.14645 -0.02803 0.17033 -0.02803 0.19562 -0.02760 0.22221 -0.02675 0.25000 -0.02545 0.27886 -0.02376 0.30866 -0.02165 0.33928 -0.01916 0.37059 -0.01638 0.40245 -0.01358 0.43474 -0.01072 0.46730 -0.00804 0.50000 -0.00548 0.53270 -0.00312 0.56526 -0.00097 0.59755 0.00095 0.62941 0.00267 0.66072 0.00408 0.69134 0.00529 0.72114 0.00622 0.75000 0.00695 0.77779 0.00734 0.80438 0.00754 0.82967 0.00746 0.85355 0.00724 0.87592 0.00680 0.89668 0.00624 0.91573 0.00549 0.93301 0.00467 0.94844 0.00375 0.96194 0.00283 0.97347 0.00193 0.98296 0.00113 0.99039 0.00043 0.99572 -0.00014 0.99893 -0.00055 1.00000 0.00000 |
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Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
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Polars for FX 83-W-108 (fx83w108-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx83w108-il | 50,000 | 9 | 36.8 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx83w108-il | 50,000 | 5 | 34.5 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx83w108-il | 100,000 | 9 | 61 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx83w108-il | 100,000 | 5 | 60.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx83w108-il | 200,000 | 9 | 90.5 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx83w108-il | 200,000 | 5 | 86.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx83w108-il | 500,000 | 9 | 129.6 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx83w108-il | 500,000 | 5 | 117.7 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx83w108-il | 1,000,000 | 9 | 157.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx83w108-il | 1,000,000 | 5 | 115.4 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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