Airfoil Comparison
Select airfoils from the airfoil database or add your own airfoils and compare the airfoil shape and lift/drag polars.
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(fx80080-il) WORTMANN FX 80-080 | Wortmann FX 80-080 airfoil Max thickness 8.1% at 40.2% chord Max camber 2.2% at 50% chord | Remove Airfoil details Airfoil plotter |
(fx63100-il) FX 63-100 AIRFOIL | Wortmann FX 63-100 airfoil Max thickness 9.9% at 30.8% chord Max camber 4.3% at 50% chord | Remove Airfoil details Airfoil plotter |
(fxlv152-il) WORTMANN FX L V-152 AIRFOIL | Wortmann FX L V-152 airfoil Max thickness 15.3% at 33.9% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(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 | Remove Airfoil details Airfoil plotter |
(fx74modsm-il) FX 74-Cl5-140 MOD (smoothed) | Modified Wortmann FX 74-CL5-140 high lift airfoil Max thickness 13.1% at 27.1% chord Max camber 9.7% at 41.6% chord | Remove Airfoil details Airfoil plotter |
(fx75193-il) WORTMANN FX 75-193 | Wortmann FX 75-193 airfoil Max thickness 19.3% at 40.2% chord Max camber 3.7% at 69.1% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (fx80080-il,fx63100-il,fxlv152-il,fx77080-il,fx74modsm-il,fx75193-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx80080-il | 50,000 | 9 | 33.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx80080-il | 50,000 | 5 | 36.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx80080-il | 100,000 | 9 | 57.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx80080-il | 100,000 | 5 | 55.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx80080-il | 200,000 | 9 | 80.4 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx80080-il | 200,000 | 5 | 74.7 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx80080-il | 500,000 | 9 | 113.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx80080-il | 500,000 | 5 | 90.5 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx80080-il | 1,000,000 | 9 | 123.6 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx80080-il | 1,000,000 | 5 | 98 at α=1.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63100-il | 50,000 | 9 | 43 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63100-il | 50,000 | 5 | 44.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63100-il | 100,000 | 9 | 67 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63100-il | 100,000 | 5 | 67.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63100-il | 200,000 | 9 | 92.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63100-il | 200,000 | 5 | 90 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63100-il | 500,000 | 9 | 121.7 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63100-il | 500,000 | 5 | 106.2 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63100-il | 1,000,000 | 9 | 136.5 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63100-il | 1,000,000 | 5 | 115.4 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxlv152-il | 50,000 | 9 | 27.1 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxlv152-il | 50,000 | 5 | 27.4 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxlv152-il | 100,000 | 9 | 42.6 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxlv152-il | 100,000 | 5 | 38.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxlv152-il | 200,000 | 9 | 52.3 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxlv152-il | 200,000 | 5 | 45.3 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxlv152-il | 500,000 | 9 | 59.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxlv152-il | 500,000 | 5 | 53.9 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxlv152-il | 1,000,000 | 9 | 66.8 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxlv152-il | 1,000,000 | 5 | 62.6 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| 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 | |
| fx74modsm-il | 50,000 | 9 | 6.2 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx74modsm-il | 50,000 | 5 | 28.8 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx74modsm-il | 100,000 | 9 | 41.7 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx74modsm-il | 100,000 | 5 | 58.1 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx74modsm-il | 200,000 | 9 | 76.4 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx74modsm-il | 200,000 | 5 | 84.1 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx74modsm-il | 500,000 | 9 | 118.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx74modsm-il | 500,000 | 5 | 119.7 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx74modsm-il | 1,000,000 | 9 | 152.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx74modsm-il | 1,000,000 | 5 | 149.8 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx75193-il | 50,000 | 9 | 4.2 at α=12.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx75193-il | 50,000 | 5 | 11.7 at α=14.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx75193-il | 100,000 | 9 | 23.4 at α=12.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx75193-il | 100,000 | 5 | 22.9 at α=11.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx75193-il | 200,000 | 9 | 43.4 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx75193-il | 200,000 | 5 | 44.1 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx75193-il | 500,000 | 9 | 91.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx75193-il | 500,000 | 5 | 93.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx75193-il | 1,000,000 | 9 | 122.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx75193-il | 1,000,000 | 5 | 120.1 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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