WORTMANN FX 76-120 (fx76120-il)
WORTMANN FX 76-120 - Wortmann FX 76-120 symmetrical airfoil
| Details | Dat file | Parser | |
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(fx76120-il) WORTMANN FX 76-120 Wortmann FX 76-120 symmetrical airfoil Max thickness 12.1% 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 76-120 1.00000 0.00000 0.99893 0.00073 0.99572 0.00099 0.99039 0.00170 0.98296 0.00262 0.97347 0.00386 0.96194 0.00533 0.94844 0.00703 0.93301 0.00900 0.91573 0.01123 0.89668 0.01368 0.87592 0.01633 0.85355 0.01914 0.82967 0.02207 0.80438 0.02505 0.77779 0.02806 0.75000 0.03108 0.72114 0.03407 0.69134 0.03702 0.66072 0.03988 0.62941 0.04264 0.59755 0.04530 0.56526 0.04785 0.53270 0.05024 0.50000 0.05241 0.46730 0.05432 0.43474 0.05601 0.40245 0.05748 0.37059 0.05869 0.33928 0.05958 0.30866 0.06013 0.27886 0.06035 0.25000 0.06021 0.22221 0.05968 0.19562 0.05871 0.17033 0.05729 0.14645 0.05535 0.12408 0.05285 0.10332 0.04975 0.08427 0.04611 0.06699 0.04200 0.05156 0.03752 0.03806 0.03273 0.02653 0.02770 0.01704 0.02245 0.00961 0.01694 0.00428 0.01127 0.00107 0.00560 0.00000 0.00000 0.00107 -0.00560 0.00428 -0.01127 0.00961 -0.01694 0.01704 -0.02245 0.02653 -0.02770 0.03806 -0.03273 0.05156 -0.03752 0.06699 -0.04200 0.08427 -0.04611 0.10332 -0.04975 0.12408 -0.05285 0.14645 -0.05535 0.17033 -0.05729 0.19562 -0.05871 0.22221 -0.05968 0.25000 -0.06021 0.27886 -0.06035 0.30866 -0.06013 0.33928 -0.05958 0.37059 -0.05869 0.40245 -0.05748 0.43474 -0.05601 0.46730 -0.05432 0.50000 -0.05241 0.53270 -0.05024 0.56526 -0.04785 0.59755 -0.04530 0.62941 -0.04264 0.66072 -0.03988 0.69134 -0.03702 0.72114 -0.03407 0.75000 -0.03108 0.77779 -0.02806 0.80438 -0.02505 0.82967 -0.02207 0.85355 -0.01914 0.87592 -0.01633 0.89668 -0.01368 0.91573 -0.01123 0.93301 -0.00900 0.94844 -0.00703 0.96194 -0.00533 0.97347 -0.00386 0.98296 -0.00262 0.99039 -0.00170 0.99572 -0.00099 0.99893 -0.00073 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 76-120 (fx76120-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx76120-il | 50,000 | 9 | 25 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx76120-il | 50,000 | 5 | 26.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx76120-il | 100,000 | 9 | 35.9 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx76120-il | 100,000 | 5 | 37.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx76120-il | 200,000 | 9 | 49.3 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx76120-il | 200,000 | 5 | 49.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx76120-il | 500,000 | 9 | 67.9 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx76120-il | 500,000 | 5 | 64.2 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx76120-il | 1,000,000 | 9 | 78.9 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx76120-il | 1,000,000 | 5 | 76.8 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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