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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(fx63145-il) FX 63-145 AIRFOIL | Wortmann FX 63-145 airfoil Max thickness 14.5% at 30.9% chord Max camber 4% at 37.1% chord | Remove Airfoil details Airfoil plotter |
(fx60160-il) FX 60-160 AIRFOIL | Wortmann FX 60-160 airfoil Max thickness 15.6% at 40% chord Max camber 3.1% at 60% chord | Remove Airfoil details Airfoil plotter |
(fx61168-il) FX 61-168 AIRFOIL | Wortmann FX 61-168 airfoil Max thickness 16.8% at 37.1% chord Max camber 3% at 37.1% chord | Remove Airfoil details Airfoil plotter |
(fx63120-il) FX 63-120 AIRFOIL | Wortmann FX 63-120 airfoil Max thickness 12% at 30.8% chord Max camber 5.2% at 50% chord | Remove Airfoil details Airfoil plotter |
(fx63137-il) WORTMANN FX 63-137 AIRFOIL | Wortmann FX 63-137 human power aircraft airfoil (Liver Puffin) airfoil Max thickness 13.7% at 30.9% chord Max camber 6% at 53.3% chord | Remove Airfoil details Airfoil plotter |
(fx60157-il) FX 60-157 AIRFOIL | Wortmann FX 60-157 airfoil Max thickness 15.7% at 40.2% chord Max camber 2.7% at 75% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (fx63145-il,fx60160-il,fx61168-il,fx63120-il,fx63137-il,fx60157-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx63145-il | 50,000 | 9 | 13.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63145-il | 50,000 | 5 | 33.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63145-il | 100,000 | 9 | 56.8 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63145-il | 100,000 | 5 | 56.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63145-il | 200,000 | 9 | 75.6 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63145-il | 200,000 | 5 | 59.1 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63145-il | 500,000 | 9 | 75.7 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63145-il | 500,000 | 5 | 72.1 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63145-il | 1,000,000 | 9 | 86.9 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63145-il | 1,000,000 | 5 | 81.4 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx60160-il | 50,000 | 9 | 23.4 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx60160-il | 50,000 | 5 | 22.7 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx60160-il | 100,000 | 9 | 51 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx60160-il | 100,000 | 5 | 48.8 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx60160-il | 200,000 | 9 | 72.3 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx60160-il | 200,000 | 5 | 68.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx60160-il | 500,000 | 9 | 96.9 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx60160-il | 500,000 | 5 | 89 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx60160-il | 1,000,000 | 9 | 116.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx60160-il | 1,000,000 | 5 | 102.8 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61168-il | 50,000 | 9 | 5.1 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61168-il | 50,000 | 5 | 15.4 at α=12° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61168-il | 100,000 | 9 | 44.7 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61168-il | 100,000 | 5 | 48.4 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61168-il | 200,000 | 9 | 71 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61168-il | 200,000 | 5 | 73 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61168-il | 500,000 | 9 | 104.5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61168-il | 500,000 | 5 | 101.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx61168-il | 1,000,000 | 9 | 129.7 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx61168-il | 1,000,000 | 5 | 120.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63120-il | 50,000 | 9 | 36.7 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63120-il | 50,000 | 5 | 40 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63120-il | 100,000 | 9 | 64.7 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63120-il | 100,000 | 5 | 67.1 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63120-il | 200,000 | 9 | 93.7 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63120-il | 200,000 | 5 | 90 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63120-il | 500,000 | 9 | 125.7 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63120-il | 500,000 | 5 | 114.7 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63120-il | 1,000,000 | 9 | 147.6 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63120-il | 1,000,000 | 5 | 129.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63137-il | 50,000 | 9 | 26.8 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63137-il | 50,000 | 5 | 31.6 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63137-il | 100,000 | 9 | 62.1 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63137-il | 100,000 | 5 | 63.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63137-il | 200,000 | 9 | 90.6 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63137-il | 200,000 | 5 | 85.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63137-il | 500,000 | 9 | 119.1 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63137-il | 500,000 | 5 | 103.6 at α=1.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63137-il | 1,000,000 | 9 | 132.5 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63137-il | 1,000,000 | 5 | 105.7 at α=1.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx60157-il | 50,000 | 9 | 28.8 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx60157-il | 50,000 | 5 | 28.6 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx60157-il | 100,000 | 9 | 46.5 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx60157-il | 100,000 | 5 | 41.9 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx60157-il | 200,000 | 9 | 56.5 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx60157-il | 200,000 | 5 | 57.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx60157-il | 500,000 | 9 | 81.2 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx60157-il | 500,000 | 5 | 70 at α=0.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx60157-il | 1,000,000 | 9 | 95.8 at α=0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx60157-il | 1,000,000 | 5 | 72.8 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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