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 |
(ag37-il) AG37 | Drela AG37 airfoil Max thickness 7.7% at 26.5% chord Max camber 2.1% at 35.5% chord | Remove Airfoil details Airfoil plotter |
(fx63158-il) FX 63-158 AIRFOIL | Wortmann FX 63-158 airfoil Max thickness 15.8% at 33.9% chord Max camber 3.8% at 37.1% chord | Remove Airfoil details Airfoil plotter |
(fx63143-il) FX 63-143 AIRFOIL | Wortmann FX 63-143 airfoil Max thickness 14.3% at 33.9% chord Max camber 3.1% at 30.9% chord | Remove Airfoil details Airfoil plotter |
(goe12k-il) GOE 12K AIRFOIL | Gottingen 12K airfoil Max thickness 11.1% at 50% chord Max camber 4.1% at 60% 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 |
Drawing Options
Polars for (fx63145-il,ag37-il,fx63158-il,fx63143-il,goe12k-il,fx63120-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 | |
| ag37-il | 50,000 | 9 | 32.9 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag37-il | 50,000 | 5 | 36.4 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag37-il | 100,000 | 9 | 49.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag37-il | 100,000 | 5 | 49.8 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag37-il | 200,000 | 9 | 65.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag37-il | 200,000 | 5 | 62.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag37-il | 500,000 | 9 | 85.2 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag37-il | 500,000 | 5 | 78.6 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag37-il | 1,000,000 | 9 | 98.9 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag37-il | 1,000,000 | 5 | 89.7 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63158-il | 50,000 | 9 | 6.7 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63158-il | 50,000 | 5 | 18.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63158-il | 100,000 | 9 | 47.5 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63158-il | 100,000 | 5 | 51.4 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63158-il | 200,000 | 9 | 72.4 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63158-il | 200,000 | 5 | 67.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63158-il | 500,000 | 9 | 76.9 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63158-il | 500,000 | 5 | 70.4 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63158-il | 1,000,000 | 9 | 85 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63158-il | 1,000,000 | 5 | 81.9 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63143-il | 50,000 | 9 | 10.7 at α=-1° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63143-il | 50,000 | 5 | 24 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63143-il | 100,000 | 9 | 46.5 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63143-il | 100,000 | 5 | 49.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63143-il | 200,000 | 9 | 72.8 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63143-il | 200,000 | 5 | 65.8 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63143-il | 500,000 | 9 | 71 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63143-il | 500,000 | 5 | 64.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx63143-il | 1,000,000 | 9 | 79.4 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx63143-il | 1,000,000 | 5 | 78.7 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe12k-il | 50,000 | 9 | 28.9 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe12k-il | 50,000 | 5 | 27.3 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe12k-il | 100,000 | 9 | 42.3 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe12k-il | 100,000 | 5 | 40.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe12k-il | 200,000 | 9 | 66.2 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe12k-il | 200,000 | 5 | 65.1 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe12k-il | 500,000 | 9 | 114 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe12k-il | 500,000 | 5 | 104.2 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe12k-il | 1,000,000 | 9 | 146.7 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe12k-il | 1,000,000 | 5 | 84.6 at α=2.25° | 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 | |
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