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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(wb140-il) WB-140/35/FB 14% | Woody Blanchard WB140/35/FB R/C sailplane airfoil Max thickness 13.9% at 30% chord Max camber 3.7% at 45% chord | Remove Airfoil details Airfoil plotter |
(goe16k-il) GOE 16K AIRFOIL | Gottingen 16K airfoil Max thickness 18.2% at 50% chord Max camber 4.1% at 50% chord | Remove Airfoil details Airfoil plotter |
(fx61184-il) FX 61-184 AIRFOIL | Wortmann FX 61-184 airfoil Max thickness 18.4% at 37.1% chord Max camber 3.1% at 62.9% chord | Remove Airfoil details Airfoil plotter |
(fx601261-il) WORTMANN FX 60-126/1 AIRFOIL | Wortmann FX 60-126/1 airfoil Max thickness 12.6% at 27.9% chord Max camber 4% at 56.5% chord | Remove Airfoil details Airfoil plotter |
(marske2-il) MARSKE PIONEER IA AIRFOIL (NACA 23112/43012A HYBRID) | Marske Pioneer IA airfoil (NACA 23112/43012A hybrid) Max thickness 12.1% at 25% chord Max camber 2.7% at 15% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (wb140-il,goe16k-il,fx61184-il,fx601261-il,marske2-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| wb140-il | 50,000 | 9 | 9.9 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb140-il | 50,000 | 5 | 31.9 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb140-il | 100,000 | 9 | 53.4 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb140-il | 100,000 | 5 | 52.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb140-il | 200,000 | 9 | 83.9 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb140-il | 200,000 | 5 | 62.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb140-il | 500,000 | 9 | 105.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb140-il | 500,000 | 5 | 64 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb140-il | 1,000,000 | 9 | 109.3 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb140-il | 1,000,000 | 5 | 74.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe16k-il | 50,000 | 9 | 21.5 at α=11.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe16k-il | 50,000 | 5 | 16.6 at α=11.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe16k-il | 100,000 | 9 | 26.4 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe16k-il | 100,000 | 5 | 23.7 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe16k-il | 200,000 | 9 | 35.9 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe16k-il | 500,000 | 9 | 69.2 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe16k-il | 500,000 | 5 | 50.6 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe16k-il | 1,000,000 | 9 | 80.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe16k-il | 1,000,000 | 5 | 70.9 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61184-il | 50,000 | 9 | 5.7 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61184-il | 50,000 | 5 | 15.2 at α=12° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61184-il | 100,000 | 9 | 39.8 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61184-il | 100,000 | 5 | 43.4 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61184-il | 200,000 | 9 | 69.5 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61184-il | 200,000 | 5 | 71.1 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61184-il | 500,000 | 9 | 104.9 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61184-il | 500,000 | 5 | 100.7 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61184-il | 1,000,000 | 9 | 131.1 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61184-il | 1,000,000 | 5 | 120.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx601261-il | 50,000 | 9 | 34.5 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx601261-il | 50,000 | 5 | 39.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx601261-il | 100,000 | 9 | 59.4 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx601261-il | 100,000 | 5 | 60.5 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx601261-il | 200,000 | 9 | 82.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx601261-il | 200,000 | 5 | 76.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx601261-il | 500,000 | 9 | 108.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx601261-il | 500,000 | 5 | 84.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx601261-il | 1,000,000 | 9 | 113.3 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx601261-il | 1,000,000 | 5 | 88.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske2-il | 50,000 | 9 | 18.9 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske2-il | 50,000 | 5 | 24 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske2-il | 100,000 | 9 | 28.8 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske2-il | 100,000 | 5 | 35.7 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske2-il | 200,000 | 9 | 43 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske2-il | 200,000 | 5 | 51.5 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske2-il | 500,000 | 9 | 72.4 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske2-il | 500,000 | 5 | 77.5 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske2-il | 1,000,000 | 9 | 99 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske2-il | 1,000,000 | 5 | 97 at α=10.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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