FX 84-W-175 (fx84w175-il)
FX 84-W-175 - Wortmann FX 84-W-175 airfoil for use on wind turbines (W)
| Details | Dat file | Parser | |
|
(fx84w175-il) FX 84-W-175 Wortmann FX 84-W-175 airfoil for use on wind turbines (W) Max thickness 17.6% at 37.1% chord. Max camber 4.4% at 43.5% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
FX 84-W-175 1.00000 0.00000 0.99893 0.00016 0.99572 0.00068 0.99039 0.00168 0.98296 0.00321 0.97347 0.00536 0.96194 0.00817 0.94844 0.01169 0.93301 0.01594 0.91573 0.02092 0.89668 0.02661 0.87592 0.03295 0.85355 0.03988 0.82967 0.04731 0.80438 0.05512 0.77779 0.06320 0.75000 0.07140 0.72114 0.07958 0.69134 0.08758 0.66072 0.09526 0.62941 0.10249 0.59755 0.10912 0.56526 0.11505 0.53270 0.12016 0.50000 0.12438 0.46730 0.12762 0.43474 0.12985 0.40245 0.13103 0.37059 0.13114 0.33928 0.13019 0.30866 0.12818 0.27886 0.12516 0.25000 0.12119 0.22221 0.11632 0.19562 0.11067 0.17033 0.10432 0.14645 0.09734 0.12408 0.08980 0.10332 0.08179 0.08427 0.07342 0.06699 0.06483 0.05156 0.05612 0.03806 0.04740 0.02653 0.03876 0.01704 0.03029 0.00961 0.02210 0.00428 0.01431 0.00107 0.00696 0.00000 0.00000 0.00107 -0.00658 0.00428 -0.01269 0.00961 -0.01823 0.01704 -0.02317 0.02653 -0.02754 0.03806 -0.03140 0.05156 -0.03476 0.06699 -0.03763 0.08427 -0.04005 0.10332 -0.04205 0.12408 -0.04367 0.14645 -0.04493 0.17033 -0.04586 0.19562 -0.04649 0.22221 -0.04684 0.25000 -0.04694 0.27886 -0.04680 0.30866 -0.04643 0.33928 -0.04581 0.37059 -0.04495 0.40245 -0.04384 0.43474 -0.04246 0.46730 -0.04082 0.50000 -0.03891 0.53270 -0.03674 0.56526 -0.03431 0.59755 -0.03165 0.62941 -0.02879 0.66072 -0.02578 0.69134 -0.02265 0.72114 -0.01949 0.75000 -0.01634 0.77779 -0.01330 0.80438 -0.01041 0.82967 -0.00776 0.85355 -0.00541 0.87592 -0.00338 0.89668 -0.00172 0.91573 -0.00044 0.93301 0.00047 0.94844 0.00102 0.96194 0.00126 0.97347 0.00124 0.98296 0.00103 0.99039 0.00072 0.99572 0.00037 0.99893 0.00011 1.00000 0.00000 |
No parser warnings |
Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
Similar airfoils
|
Polars for FX 84-W-175 (fx84w175-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx84w175-il | 50,000 | 9 | 4.5 at α=12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w175-il | 50,000 | 5 | 10.3 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w175-il | 100,000 | 9 | 26.6 at α=14° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w175-il | 100,000 | 5 | 34.1 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w175-il | 200,000 | 9 | 68.4 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w175-il | 200,000 | 5 | 69.8 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w175-il | 500,000 | 9 | 108.6 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w175-il | 500,000 | 5 | 100.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w175-il | 1,000,000 | 9 | 135.1 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w175-il | 1,000,000 | 5 | 124 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| Reynolds number calculator | |||||||