FX 79-W-151 A (fx79w151a-il)
FX 79-W-151 A - Wortmann FX 79-W-151 airfoil for use on wind turbines (W) A
| Details | Dat file | Parser | |
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(fx79w151a-il) FX 79-W-151 A Wortmann FX 79-W-151 airfoil for use on wind turbines (W) A Max thickness 15.2% at 33.9% chord. Max camber 3.8% at 37.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
FX 79-W-151 A 1.00000 0.00000 0.99893 0.00082 0.99572 0.00095 0.99039 0.00148 0.98296 0.00238 0.97347 0.00388 0.96194 0.00595 0.94844 0.00861 0.93301 0.01186 0.91573 0.01569 0.89668 0.02007 0.87592 0.02495 0.85355 0.03033 0.82967 0.03613 0.80438 0.04229 0.77779 0.04872 0.75000 0.05531 0.72114 0.06201 0.69134 0.06869 0.66072 0.07528 0.62941 0.08162 0.59755 0.08764 0.56526 0.09327 0.53270 0.09841 0.50000 0.10297 0.46730 0.10679 0.43474 0.10980 0.40245 0.11192 0.37059 0.11308 0.33928 0.11327 0.30866 0.11245 0.27886 0.11059 0.25000 0.10763 0.22221 0.10355 0.19562 0.09846 0.17033 0.09256 0.14645 0.08600 0.12408 0.07892 0.10332 0.07141 0.08427 0.06358 0.06699 0.05554 0.05156 0.04741 0.03806 0.03930 0.02653 0.03133 0.01704 0.02365 0.00961 0.01648 0.00428 0.01010 0.00107 0.00465 0.00000 0.00000 0.00107 -0.00439 0.00428 -0.00891 0.00961 -0.01360 0.01704 -0.01824 0.02653 -0.02258 0.03806 -0.02659 0.05156 -0.03013 0.06699 -0.03306 0.08427 -0.03531 0.10332 -0.03697 0.12408 -0.03819 0.14645 -0.03907 0.17033 -0.03965 0.19562 -0.03997 0.22221 -0.04003 0.25000 -0.03988 0.27886 -0.03954 0.30866 -0.03903 0.33928 -0.03837 0.37059 -0.03757 0.40245 -0.03662 0.43474 -0.03552 0.46730 -0.03428 0.50000 -0.03293 0.53270 -0.03147 0.56526 -0.02995 0.59755 -0.02837 0.62941 -0.02675 0.66072 -0.02509 0.69134 -0.02338 0.72114 -0.02165 0.75000 -0.01992 0.77779 -0.01821 0.80438 -0.01654 0.82967 -0.01490 0.85355 -0.01331 0.87592 -0.01175 0.89668 -0.01025 0.91573 -0.00880 0.93301 -0.00742 0.94844 -0.00618 0.96194 -0.00489 0.97347 -0.00359 0.98296 -0.00258 0.99039 -0.00191 0.99572 -0.00151 0.99893 -0.00104 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 79-W-151 A (fx79w151a-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx79w151a-il | 50,000 | 9 | 4.8 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx79w151a-il | 50,000 | 5 | 19.1 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx79w151a-il | 100,000 | 9 | 35.6 at α=12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx79w151a-il | 100,000 | 5 | 47 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx79w151a-il | 200,000 | 9 | 69.8 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx79w151a-il | 200,000 | 5 | 71.4 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx79w151a-il | 500,000 | 9 | 104.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx79w151a-il | 500,000 | 5 | 102 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx79w151a-il | 1,000,000 | 9 | 132.2 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx79w151a-il | 1,000,000 | 5 | 126.1 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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