WORTMANN FX 73-170 A (fx73170a-il)
WORTMANN FX 73-170 A - Wortmann FX 73-170 A airfoil
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(fx73170a-il) WORTMANN FX 73-170 A Wortmann FX 73-170 A airfoil Max thickness 17.1% at 43.5% chord. Max camber 5.6% at 43.5% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
WORTMANN FX 73-170 A 1.00000 0.00000 0.99893 0.00129 0.99572 0.00223 0.99039 0.00378 0.98296 0.00578 0.97347 0.00836 0.96194 0.01147 0.94844 0.01514 0.93301 0.01946 0.91573 0.02450 0.89668 0.03028 0.87592 0.03681 0.85355 0.04403 0.82967 0.05191 0.80438 0.06037 0.77779 0.06935 0.75000 0.07880 0.72114 0.08847 0.69134 0.09808 0.66072 0.10726 0.62941 0.11577 0.59755 0.12345 0.56526 0.13002 0.53270 0.13527 0.50000 0.13903 0.46730 0.14124 0.43474 0.14195 0.40245 0.14130 0.37059 0.13949 0.33928 0.13666 0.30866 0.13292 0.27886 0.12834 0.25000 0.12299 0.22221 0.11695 0.19562 0.11030 0.17033 0.10310 0.14645 0.09542 0.12408 0.08736 0.10332 0.07898 0.08427 0.07038 0.06699 0.06164 0.05156 0.05285 0.03806 0.04411 0.02653 0.03557 0.01704 0.02738 0.00961 0.01965 0.00428 0.01222 0.00107 0.00547 0.00000 0.00000 0.00107 -0.00415 0.00428 -0.00722 0.00961 -0.00990 0.01704 -0.01239 0.02653 -0.01462 0.03806 -0.01670 0.05156 -0.01860 0.06699 -0.02035 0.08427 -0.02196 0.10332 -0.02342 0.12408 -0.02473 0.14645 -0.02588 0.17033 -0.02689 0.19562 -0.02775 0.22221 -0.02846 0.25000 -0.02902 0.27886 -0.02943 0.30866 -0.02970 0.33928 -0.02981 0.37059 -0.02976 0.40245 -0.02955 0.43474 -0.02917 0.46730 -0.02860 0.50000 -0.02781 0.53270 -0.02677 0.56526 -0.02550 0.59755 -0.02403 0.62941 -0.02234 0.66072 -0.02040 0.69134 -0.01813 0.72114 -0.01546 0.75000 -0.01248 0.77779 -0.00938 0.80438 -0.00643 0.82967 -0.00385 0.85355 -0.00175 0.87592 -0.00018 0.89668 0.00089 0.91573 0.00154 0.93301 0.00181 0.94844 0.00177 0.96194 0.00147 0.97347 0.00098 0.98296 0.00040 0.99039 -0.00022 0.99572 -0.00060 0.99893 -0.00091 1.00000 0.00000 |
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Polars for WORTMANN FX 73-170 A (fx73170a-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx73170a-il | 50,000 | 9 | 4.8 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx73170a-il | 50,000 | 5 | 11.1 at α=16° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx73170a-il | 100,000 | 9 | 18.1 at α=14.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx73170a-il | 100,000 | 5 | 17.4 at α=13.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx73170a-il | 200,000 | 9 | 31.2 at α=13° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx73170a-il | 200,000 | 5 | 51.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx73170a-il | 500,000 | 9 | 117.8 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx73170a-il | 500,000 | 5 | 110.3 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx73170a-il | 1,000,000 | 9 | 151.7 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx73170a-il | 1,000,000 | 5 | 144 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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