FX 84-W-150 (fx84w150-il)
FX 84-W-150 - Wortmann FX 84-W-150 airfoil for use on wind turbines (W)
| Details | Dat file | Parser | |
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(fx84w150-il) FX 84-W-150 Wortmann FX 84-W-150 airfoil for use on wind turbines (W) Max thickness 15% at 37.1% chord. Max camber 4.2% at 40.2% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
FX 84-W-150 1.00000 0.00000 0.99893 0.00014 0.99572 0.00062 0.99039 0.00150 0.98296 0.00285 0.97347 0.00475 0.96194 0.00724 0.94844 0.01036 0.93301 0.01411 0.91573 0.01850 0.89668 0.02351 0.87592 0.02910 0.85355 0.03522 0.82967 0.04178 0.80438 0.04870 0.77779 0.05585 0.75000 0.06315 0.72114 0.07044 0.69134 0.07759 0.66072 0.08450 0.62941 0.09100 0.59755 0.09700 0.56526 0.10241 0.53270 0.10707 0.50000 0.11096 0.46730 0.11400 0.43474 0.11608 0.40245 0.11725 0.37059 0.11745 0.33928 0.11665 0.30866 0.11494 0.27886 0.11226 0.25000 0.10872 0.22221 0.10439 0.19562 0.09929 0.17033 0.09360 0.14645 0.08735 0.12408 0.08058 0.10332 0.07339 0.08427 0.06590 0.06699 0.05823 0.05156 0.05049 0.03806 0.04277 0.02653 0.03516 0.01704 0.02775 0.00961 0.02064 0.00428 0.01379 0.00107 0.00729 0.00000 0.00131 0.00107 -0.00413 0.00428 -0.00900 0.00961 -0.01343 0.01704 -0.01743 0.02653 -0.02090 0.03806 -0.02389 0.05156 -0.02643 0.06699 -0.02855 0.08427 -0.03028 0.10332 -0.03165 0.12408 -0.03271 0.14645 -0.03348 0.17033 -0.03400 0.19562 -0.03429 0.22221 -0.03439 0.25000 -0.03432 0.27886 -0.03409 0.30866 -0.03370 0.33928 -0.03315 0.37059 -0.03244 0.40245 -0.03156 0.43474 -0.03051 0.46730 -0.02929 0.50000 -0.02788 0.53270 -0.02629 0.56526 -0.02452 0.59755 -0.02258 0.62941 -0.02049 0.66072 -0.01828 0.69134 -0.01598 0.72114 -0.01366 0.75000 -0.01135 0.77779 -0.00910 0.80438 -0.00698 0.82967 -0.00502 0.85355 -0.00329 0.87592 -0.00181 0.89668 -0.00061 0.91573 0.00029 0.93301 0.00091 0.94844 0.00126 0.96194 0.00136 0.97347 0.00125 0.98296 0.00101 0.99039 0.00068 0.99572 0.00034 0.99893 0.00010 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-150 (fx84w150-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx84w150-il | 50,000 | 9 | 5.5 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w150-il | 50,000 | 5 | 14.6 at α=13.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w150-il | 100,000 | 9 | 42.2 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w150-il | 100,000 | 5 | 47.4 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w150-il | 200,000 | 9 | 77.3 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w150-il | 200,000 | 5 | 77.4 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w150-il | 500,000 | 9 | 116 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w150-il | 500,000 | 5 | 111 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w150-il | 1,000,000 | 9 | 146.3 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w150-il | 1,000,000 | 5 | 133.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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