WORTMANN FX 76-100 (fx76100-il)
WORTMANN FX 76-100 - Wortmann FX 76-100 symmetrical airfoil
| Details | Dat file | Parser | |
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(fx76100-il) WORTMANN FX 76-100 Wortmann FX 76-100 symmetrical airfoil Max thickness 10.1% at 27.9% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
WORTMANN FX 76-100 1.00000 0.00000 0.99893 0.00076 0.99572 0.00100 0.99039 0.00161 0.98296 0.00239 0.97347 0.00343 0.96194 0.00466 0.94844 0.00609 0.93301 0.00773 0.91573 0.00959 0.89668 0.01163 0.87592 0.01383 0.85355 0.01617 0.82967 0.01859 0.80438 0.02107 0.77779 0.02357 0.75000 0.02607 0.72114 0.02855 0.69134 0.03099 0.66072 0.03336 0.62941 0.03565 0.59755 0.03786 0.56526 0.03997 0.53270 0.04195 0.50000 0.04375 0.46730 0.04534 0.43474 0.04674 0.40245 0.04795 0.37059 0.04896 0.33928 0.04969 0.30866 0.05015 0.27886 0.05033 0.25000 0.05021 0.22221 0.04976 0.19562 0.04896 0.17033 0.04777 0.14645 0.04615 0.12408 0.04406 0.10332 0.04148 0.08427 0.03844 0.06699 0.03502 0.05156 0.03128 0.03806 0.02730 0.02653 0.02310 0.01704 0.01872 0.00961 0.01414 0.00428 0.00940 0.00107 0.00467 0.00000 0.00000 0.00107 -0.00467 0.00428 -0.00940 0.00961 -0.01414 0.01704 -0.01872 0.02653 -0.02310 0.03806 -0.02730 0.05156 -0.03128 0.06699 -0.03502 0.08427 -0.03844 0.10332 -0.04148 0.12408 -0.04406 0.14645 -0.04615 0.17033 -0.04777 0.19562 -0.04896 0.22221 -0.04976 0.25000 -0.05021 0.27886 -0.05033 0.30866 -0.05015 0.33928 -0.04969 0.37059 -0.04896 0.40245 -0.04795 0.43474 -0.04674 0.46730 -0.04534 0.50000 -0.04375 0.53270 -0.04195 0.56526 -0.03997 0.59755 -0.03786 0.62941 -0.03565 0.66072 -0.03336 0.69134 -0.03099 0.72114 -0.02855 0.75000 -0.02607 0.77779 -0.02357 0.80438 -0.02107 0.82967 -0.01859 0.85355 -0.01617 0.87592 -0.01383 0.89668 -0.01163 0.91573 -0.00959 0.93301 -0.00773 0.94844 -0.00609 0.96194 -0.00466 0.97347 -0.00343 0.98296 -0.00239 0.99039 -0.00161 0.99572 -0.00100 0.99893 -0.00076 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 WORTMANN FX 76-100 (fx76100-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx76100-il | 50,000 | 9 | 25.6 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx76100-il | 50,000 | 5 | 26.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx76100-il | 100,000 | 9 | 35.4 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx76100-il | 100,000 | 5 | 36.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx76100-il | 200,000 | 9 | 47.1 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx76100-il | 200,000 | 5 | 46.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx76100-il | 500,000 | 9 | 62.9 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx76100-il | 500,000 | 5 | 61.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx76100-il | 1,000,000 | 9 | 75.1 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx76100-il | 1,000,000 | 5 | 75.4 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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