WORTMANN FX 77-080 (fx77080-il)
WORTMANN FX 77-080 - Wortmann FX 77-080 symmetrical airfoil
| Details | Dat file | Parser | |
|
(fx77080-il) WORTMANN FX 77-080 Wortmann FX 77-080 symmetrical airfoil Max thickness 8% 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 77-080 1.00000 0.00000 0.99893 0.00079 0.99572 0.00099 0.99039 0.00150 0.98296 0.00211 0.97347 0.00293 0.96194 0.00390 0.94844 0.00502 0.93301 0.00631 0.91573 0.00777 0.89668 0.00937 0.87592 0.01111 0.85355 0.01294 0.82967 0.01485 0.80438 0.01680 0.77779 0.01877 0.75000 0.02074 0.72114 0.02270 0.69134 0.02463 0.66072 0.02651 0.62941 0.02832 0.59755 0.03007 0.56526 0.03175 0.53270 0.03333 0.50000 0.03477 0.46730 0.03605 0.43474 0.03718 0.40245 0.03817 0.37059 0.03900 0.33928 0.03963 0.30866 0.04004 0.27886 0.04024 0.25000 0.04021 0.22221 0.03994 0.19562 0.03941 0.17033 0.03861 0.14645 0.03756 0.12408 0.03625 0.10332 0.03461 0.08427 0.03254 0.06699 0.02998 0.05156 0.02697 0.03806 0.02362 0.02653 0.02002 0.01704 0.01627 0.00961 0.01234 0.00428 0.00828 0.00107 0.00415 0.00000 0.00000 0.00107 -0.00415 0.00428 -0.00828 0.00961 -0.01234 0.01704 -0.01627 0.02653 -0.02002 0.03806 -0.02362 0.05156 -0.02697 0.06699 -0.02998 0.08427 -0.03254 0.10332 -0.03461 0.12408 -0.03625 0.14645 -0.03756 0.17033 -0.03861 0.19562 -0.03941 0.22221 -0.03994 0.25000 -0.04021 0.27886 -0.04024 0.30866 -0.04004 0.33928 -0.03963 0.37059 -0.03900 0.40245 -0.03817 0.43474 -0.03718 0.46730 -0.03605 0.50000 -0.03477 0.53270 -0.03333 0.56526 -0.03175 0.59755 -0.03007 0.62941 -0.02832 0.66072 -0.02651 0.69134 -0.02463 0.72114 -0.02270 0.75000 -0.02074 0.77779 -0.01877 0.80438 -0.01680 0.82967 -0.01485 0.85355 -0.01294 0.87592 -0.01111 0.89668 -0.00937 0.91573 -0.00777 0.93301 -0.00631 0.94844 -0.00502 0.96194 -0.00390 0.97347 -0.00293 0.98296 -0.00211 0.99039 -0.00150 0.99572 -0.00099 0.99893 -0.00079 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 WORTMANN FX 77-080 (fx77080-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx77080-il | 50,000 | 9 | 24.7 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx77080-il | 50,000 | 5 | 23.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx77080-il | 100,000 | 9 | 33.7 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx77080-il | 100,000 | 5 | 33.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx77080-il | 200,000 | 9 | 42 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx77080-il | 200,000 | 5 | 43.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx77080-il | 500,000 | 9 | 58.4 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx77080-il | 500,000 | 5 | 58.6 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx77080-il | 1,000,000 | 9 | 71.2 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx77080-il | 1,000,000 | 5 | 72.7 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| Reynolds number calculator | |||||||