FX 75-VG-166/22 (fx75vg166-il)
FX 75-VG-166/22 - Wortmann FX 75-VG-166/22 variable geometry airfoil
| Details | Dat file | Parser | |
|
(fx75vg166-il) FX 75-VG-166/22 Wortmann FX 75-VG-166/22 variable geometry airfoil Max thickness 16.7% at 43.5% chord. Max camber 2.4% at 40.2% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
FX 75-VG-166/22 1.00000 0.00000 0.99893 0.00122 0.99572 0.00204 0.99039 0.00331 0.98296 0.00506 0.97347 0.00719 0.96194 0.00961 0.94844 0.01225 0.93301 0.01501 0.91573 0.01796 0.89668 0.02080 0.87592 0.02447 0.85355 0.02826 0.82967 0.03234 0.80438 0.03754 0.77779 0.04396 0.75000 0.05289 0.72114 0.06225 0.69134 0.07252 0.66072 0.08149 0.62941 0.08906 0.59755 0.09496 0.56526 0.09987 0.53270 0.10333 0.50000 0.10585 0.46730 0.10726 0.43474 0.10788 0.40245 0.10758 0.37059 0.10660 0.33928 0.10479 0.30866 0.10237 0.27886 0.09931 0.25000 0.09563 0.22221 0.09139 0.19562 0.08666 0.17033 0.08152 0.14645 0.07596 0.12408 0.07014 0.10332 0.06401 0.08427 0.05770 0.06699 0.05107 0.05156 0.04431 0.03806 0.03739 0.02653 0.03059 0.01704 0.02389 0.00961 0.01766 0.00428 0.01171 0.00107 0.00614 0.00000 0.00000 0.00107 -0.00474 0.00428 -0.00891 0.00961 -0.01286 0.01704 -0.01655 0.02653 -0.02026 0.03806 -0.02381 0.05156 -0.02739 0.06699 -0.03080 0.08427 -0.03416 0.10332 -0.03734 0.12408 -0.04043 0.14645 -0.04332 0.17033 -0.04603 0.19562 -0.04853 0.22221 -0.05082 0.25000 -0.05289 0.27886 -0.05467 0.30866 -0.05622 0.33928 -0.05745 0.37059 -0.05843 0.40245 -0.05902 0.43474 -0.05938 0.46730 -0.05927 0.50000 -0.05893 0.53270 -0.05802 0.56526 -0.05689 0.59755 -0.05506 0.62941 -0.05297 0.66072 -0.04995 0.69134 -0.04641 0.72114 -0.04163 0.75000 -0.03634 0.77779 -0.02844 0.80438 -0.02136 0.82967 -0.01506 0.85355 -0.01029 0.87592 -0.00636 0.89668 -0.00330 0.91573 -0.00145 0.93301 -0.00010 0.94844 0.00064 0.96194 0.00088 0.97347 0.00073 0.98296 0.00027 0.99039 -0.00028 0.99572 -0.00063 0.99893 -0.00087 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 75-VG-166/22 (fx75vg166-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx75vg166-il | 50,000 | 9 | 20.6 at α=11.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx75vg166-il | 50,000 | 5 | 17.2 at α=11.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx75vg166-il | 100,000 | 9 | 28.7 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx75vg166-il | 100,000 | 5 | 25.7 at α=10.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx75vg166-il | 200,000 | 9 | 43.1 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx75vg166-il | 200,000 | 5 | 45 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx75vg166-il | 500,000 | 9 | 82.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx75vg166-il | 500,000 | 5 | 84 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx75vg166-il | 1,000,000 | 9 | 107.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx75vg166-il | 1,000,000 | 5 | 103.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| Reynolds number calculator | |||||||