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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(naca001064-il) NACA 0010-64 | NACA 0010-64 airfoil Max thickness 10% at 40% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(fx62k131-il) WORTMANN FX 62-K-131 AIRFOIL | Wortmann FX 62-K-131/17 airfoil Max thickness 13.1% at 40.2% chord Max camber 3.9% at 53.3% chord | Remove Airfoil details Airfoil plotter |
(fx84w097-il) FX 84-W-097 | Wortmann FX 84-W-097 airfoil for use on wind turbines (W) Max thickness 9.7% at 33.9% chord Max camber 2.8% at 37.1% chord | Remove Airfoil details Airfoil plotter |
(eh1590-il) EH 1.5/9.0 | John Yost EH 1.5/9.0 for tailless R/C aircraft Max thickness 9% at 28.7% chord Max camber 1.5% at 25.9% chord | Remove Airfoil details Airfoil plotter |
(fx84w150-il) FX 84-W-150 | Wortmann FX 84-W-150 airfoil for use on wind turbines (W) Max thickness 15% at 37.1% chord Max camber 4.2% at 40.2% chord | Remove Airfoil details Airfoil plotter |
(sa7026-il) SA7026 | Selig / Ashok Gopalarathnam SA7026 low Reynolds number airfoil Max thickness 9% at 32.9% chord Max camber 3.8% at 47.1% 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 |
(ec863914-il) EPPLER EC 86(-3)-914 AIRFOIL | Eppler EC 86(-3)-914 airfoil Max thickness 14.3% at 35.5% chord Max camber 4.4% at 71.2% chord | Remove Airfoil details Airfoil plotter |
(ah79100a-il) AH 79-100 A AIRFOIL | Althaus AH 79-100A airfoil Max thickness 10% at 27.9% chord Max camber 3.6% at 56.5% chord | Remove Airfoil details Airfoil plotter |
(ys900-il) YS-900 | YS900 hyrdofoil (Shen / Eppler) Max thickness 9% at 52.5% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (naca001064-il,fx62k131-il,fx84w097-il,eh1590-il,fx84w150-il,sa7026-il,fx63137-il,ec863914-il,ah79100a-il,ys900-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| naca001064-il | 50,000 | 9 | 25.8 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca001064-il | 50,000 | 5 | 25.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca001064-il | 100,000 | 9 | 36.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca001064-il | 100,000 | 5 | 31.7 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca001064-il | 200,000 | 9 | 43.3 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca001064-il | 200,000 | 5 | 38.7 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca001064-il | 500,000 | 9 | 49.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca001064-il | 500,000 | 5 | 53.7 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca001064-il | 1,000,000 | 9 | 62.5 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca001064-il | 1,000,000 | 5 | 71.6 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k131-il | 50,000 | 5 | 29 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k131-il | 50,000 | 0 | 30.5 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx62k131-il | 100,000 | 5 | 55.1 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k131-il | 100,000 | 0 | 56.4 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx62k131-il | 200,000 | 5 | 84.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k131-il | 200,000 | 0 | 83.7 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx62k131-il | 500,000 | 5 | 125.5 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k131-il | 500,000 | 0 | 124 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx62k131-il | 1,000,000 | 5 | 153.3 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k131-il | 1,000,000 | 0 | 162.4 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w097-il | 50,000 | 9 | 36.1 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w097-il | 50,000 | 5 | 36.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w097-il | 100,000 | 9 | 56.5 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w097-il | 100,000 | 5 | 55.6 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w097-il | 200,000 | 9 | 76.9 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w097-il | 200,000 | 5 | 73.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w097-il | 500,000 | 9 | 104.3 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w097-il | 500,000 | 5 | 96.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w097-il | 1,000,000 | 9 | 123.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w097-il | 1,000,000 | 5 | 112.1 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| eh1590-il | 50,000 | 9 | 30.5 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| eh1590-il | 50,000 | 5 | 32.3 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| eh1590-il | 100,000 | 9 | 45.6 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| eh1590-il | 100,000 | 5 | 45.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| eh1590-il | 200,000 | 9 | 60.2 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| eh1590-il | 200,000 | 5 | 58.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| eh1590-il | 500,000 | 9 | 80.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| eh1590-il | 500,000 | 5 | 76 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| eh1590-il | 1,000,000 | 9 | 94.7 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| eh1590-il | 1,000,000 | 5 | 83.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w150-il | 50,000 | 9 | 5.5 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w150-il | 50,000 | 5 | 14.6 at α=13.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w150-il | 100,000 | 9 | 42.2 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w150-il | 100,000 | 5 | 47.4 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w150-il | 200,000 | 9 | 77.3 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w150-il | 200,000 | 5 | 77.4 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w150-il | 500,000 | 9 | 116 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w150-il | 500,000 | 5 | 111 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w150-il | 1,000,000 | 9 | 146.3 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w150-il | 1,000,000 | 5 | 133.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7026-il | 50,000 | 9 | 38.4 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7026-il | 50,000 | 5 | 40.6 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7026-il | 100,000 | 9 | 61.8 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7026-il | 100,000 | 5 | 61.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7026-il | 200,000 | 9 | 87.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7026-il | 200,000 | 5 | 82.8 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7026-il | 500,000 | 9 | 121.1 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7026-il | 500,000 | 5 | 106.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7026-il | 1,000,000 | 9 | 143.1 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7026-il | 1,000,000 | 5 | 120.7 at α=2.75° | 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 | |
| ec863914-il | 50,000 | 9 | 34.9 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ec863914-il | 50,000 | 5 | 32.3 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ec863914-il | 100,000 | 9 | 50.4 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ec863914-il | 100,000 | 5 | 44.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ec863914-il | 200,000 | 9 | 62.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ec863914-il | 200,000 | 5 | 63 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ec863914-il | 500,000 | 9 | 103.4 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ec863914-il | 500,000 | 5 | 98.1 at α=0.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ec863914-il | 1,000,000 | 9 | 150.9 at α=1° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ec863914-il | 1,000,000 | 5 | 101 at α=-0.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah79100a-il | 50,000 | 9 | 39.8 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah79100a-il | 50,000 | 5 | 41.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah79100a-il | 100,000 | 9 | 61.9 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah79100a-il | 100,000 | 5 | 62.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah79100a-il | 200,000 | 9 | 85.5 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah79100a-il | 200,000 | 5 | 81.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah79100a-il | 500,000 | 9 | 116.2 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah79100a-il | 500,000 | 5 | 103.7 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah79100a-il | 1,000,000 | 9 | 137 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah79100a-il | 1,000,000 | 5 | 107.4 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ys900-il | 50,000 | 9 | 17.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ys900-il | 50,000 | 5 | 17.4 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ys900-il | 100,000 | 9 | 21 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ys900-il | 100,000 | 5 | 21.8 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ys900-il | 200,000 | 9 | 21.5 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ys900-il | 200,000 | 5 | 21.6 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ys900-il | 500,000 | 9 | 24.2 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ys900-il | 500,000 | 5 | 33.4 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ys900-il | 1,000,000 | 9 | 22.7 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ys900-il | 1,000,000 | 5 | 49 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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