FX 84-W-097 (fx84w097-il)
FX 84-W-097 - Wortmann FX 84-W-097 airfoil for use on wind turbines (W)
| Details | Dat file | Parser | |
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(fx84w097-il) FX 84-W-097 Wortmann FX 84-W-097 airfoil for use on wind turbines (W) Max thickness 9.7% at 33.9% chord. Max camber 2.8% at 37.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
FX 84-W-097 1.00000 0.00000 0.99893 0.00006 0.99572 0.00028 0.99039 0.00069 0.98296 0.00135 0.97347 0.00230 0.96194 0.00359 0.94844 0.00524 0.93301 0.00726 0.91573 0.00968 0.89668 0.01250 0.87592 0.01571 0.85355 0.01929 0.82967 0.02320 0.80438 0.02739 0.77779 0.03182 0.75000 0.03643 0.72114 0.04113 0.69134 0.04584 0.66072 0.05050 0.62941 0.05499 0.59755 0.05926 0.56526 0.06322 0.53270 0.06677 0.50000 0.06988 0.46730 0.07247 0.43474 0.07445 0.40245 0.07583 0.37059 0.07654 0.33928 0.07659 0.30866 0.07599 0.27886 0.07469 0.25000 0.07276 0.22221 0.07023 0.19562 0.06711 0.17033 0.06353 0.14645 0.05948 0.12408 0.05502 0.10332 0.05020 0.08427 0.04511 0.06699 0.03985 0.05156 0.03449 0.03806 0.02911 0.02653 0.02376 0.01704 0.01854 0.00961 0.01347 0.00428 0.00867 0.00107 0.00419 0.00000 0.00000 0.00107 -0.00387 0.00428 -0.00742 0.00961 -0.01056 0.01704 -0.01329 0.02653 -0.01563 0.03806 -0.01761 0.05156 -0.01923 0.06699 -0.02052 0.08427 -0.02151 0.10332 -0.02221 0.12408 -0.02267 0.14645 -0.02292 0.17033 -0.02298 0.19562 -0.02288 0.22221 -0.02264 0.25000 -0.02230 0.27886 -0.02188 0.30866 -0.02138 0.33928 -0.02081 0.37059 -0.02019 0.40245 -0.01950 0.43474 -0.01876 0.46730 -0.01797 0.50000 -0.01711 0.53270 -0.01620 0.56526 -0.01521 0.59755 -0.01416 0.62941 -0.01305 0.66072 -0.01188 0.69134 -0.01068 0.72114 -0.00944 0.75000 -0.00819 0.77779 -0.00694 0.80438 -0.00574 0.82967 -0.00460 0.85355 -0.00354 0.87592 -0.00258 0.89668 -0.00175 0.91573 -0.00106 0.93301 -0.00052 0.94844 -0.00014 0.96194 0.00011 0.97347 0.00024 0.98296 0.00026 0.99039 0.00021 0.99572 0.00012 0.99893 0.00003 1.00000 0.00000 |
No parser warnings |
Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
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Polars for FX 84-W-097 (fx84w097-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx84w097-il | 50,000 | 9 | 36.1 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w097-il | 50,000 | 5 | 36.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w097-il | 100,000 | 9 | 56.5 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w097-il | 100,000 | 5 | 55.6 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w097-il | 200,000 | 9 | 76.9 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w097-il | 200,000 | 5 | 73.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w097-il | 500,000 | 9 | 104.3 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w097-il | 500,000 | 5 | 96.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w097-il | 1,000,000 | 9 | 123.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w097-il | 1,000,000 | 5 | 112.1 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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