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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(e471-il) E471 (6.25%) | Eppler E471 airfoil Max thickness 6.3% at 29.8% chord Max camber 4.5% at 53.5% chord | Remove Airfoil details Airfoil plotter |
(nacam18-il) NACA M18 | NACA M18 airfoil Max thickness 12% at 30% chord Max camber 4.1% at 30% chord | Remove Airfoil details Airfoil plotter |
(goe360-il) GOE 360 AIRFOIL | Gottingen 360 airfoil Max thickness 9.7% at 29.9% chord Max camber 5.9% at 29.9% chord | Remove Airfoil details Airfoil plotter |
(fx62k153-il) FX 62-K-153/20 AIRFOIL | Wortmann FX 62-K-153/20 airfoil Max thickness 15.3% at 40.2% chord Max camber 4.1% at 62.9% chord | Remove Airfoil details Airfoil plotter |
(goe280-il) GOE 280 (DAIMLER XI) AIRFOIL | Gottingen 280 (DAIMLER XI) airfoil Max thickness 7.9% at 30% chord Max camber 4.5% at 30% 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 |
(s3010-il) S3010-103-84 | Selig S3010 low Reynolds number airfoil Max thickness 10.3% at 25% chord Max camber 2.3% at 43.3% chord | Remove Airfoil details Airfoil plotter |
(fxl142k-il) FX LIII-142 K 25 AIRFOIL | Wortmann FX LIII-142 K 25 airfoil Max thickness 14.2% at 30.9% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(e335-il) EPPLER 335 AIRFOIL | Eppler E335 flying wing airfoil Max thickness 12.6% at 29% chord Max camber 2.3% at 19.9% chord | Remove Airfoil details Airfoil plotter |
(e856-il) EPPLER 856 AIRFOIL | Eppler E856 propeller airfoil Max thickness 18.2% at 31.9% chord Max camber 4.2% at 50.2% chord | Remove Airfoil details Airfoil plotter |
(la5055-il) LIEBECK LA5055 AIRFOIL | Liebeck high lift airfoil Max thickness 15.9% at 35% chord Max camber 5.9% at 40% chord | Remove Airfoil details Airfoil plotter |
(fx79l100-il) FX 79-L-100 | Wortmann FX 79-L-100 symmetrical airfoil Max thickness 10.1% at 33.9% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(e212-il) E212 (10.55%) | Eppler E212 low Reynolds number airfoil Max thickness 10.6% at 27.5% chord Max camber 2.5% at 61.3% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (e471-il,nacam18-il,goe360-il,fx62k153-il,goe280-il,fx63158-il,s3010-il,fxl142k-il,e335-il,e856-il,la5055-il,fx79l100-il,e212-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e471-il | 50,000 | 9 | 46.4 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e471-il | 50,000 | 5 | 46.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e471-il | 100,000 | 9 | 73 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e471-il | 100,000 | 5 | 72 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e471-il | 200,000 | 9 | 105.5 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e471-il | 200,000 | 5 | 101.1 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e471-il | 500,000 | 9 | 153.7 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e471-il | 500,000 | 5 | 138.5 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e471-il | 1,000,000 | 9 | 189.5 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e471-il | 1,000,000 | 5 | 152 at α=1.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nacam18-il | 50,000 | 9 | 10.2 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nacam18-il | 50,000 | 5 | 26.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nacam18-il | 100,000 | 9 | 47.9 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nacam18-il | 100,000 | 5 | 50.8 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nacam18-il | 200,000 | 9 | 71.7 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nacam18-il | 200,000 | 5 | 72.3 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nacam18-il | 500,000 | 9 | 102.6 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nacam18-il | 500,000 | 5 | 99.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nacam18-il | 1,000,000 | 9 | 125.1 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nacam18-il | 1,000,000 | 5 | 114 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe360-il | 50,000 | 9 | 20.7 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe360-il | 50,000 | 5 | 36.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe360-il | 100,000 | 9 | 51.4 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe360-il | 100,000 | 5 | 56.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe360-il | 200,000 | 9 | 73.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe360-il | 200,000 | 5 | 76.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe360-il | 500,000 | 9 | 105.3 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe360-il | 500,000 | 5 | 104.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe360-il | 1,000,000 | 9 | 131.2 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe360-il | 1,000,000 | 5 | 127.3 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k153-il | 50,000 | 9 | 26.9 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx62k153-il | 50,000 | 5 | 23 at α=10.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k153-il | 100,000 | 9 | 45.3 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx62k153-il | 100,000 | 5 | 44.1 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k153-il | 200,000 | 9 | 77.5 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx62k153-il | 200,000 | 5 | 79.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k153-il | 500,000 | 9 | 124.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx62k153-il | 500,000 | 5 | 122.8 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k153-il | 1,000,000 | 9 | 161.9 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx62k153-il | 1,000,000 | 5 | 151.3 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe280-il | 50,000 | 9 | 37.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe280-il | 50,000 | 5 | 41.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe280-il | 100,000 | 9 | 55.5 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe280-il | 100,000 | 5 | 56.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe280-il | 200,000 | 9 | 72.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe280-il | 200,000 | 5 | 70.2 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe280-il | 500,000 | 9 | 91.6 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe280-il | 500,000 | 5 | 79.6 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe280-il | 1,000,000 | 9 | 98.7 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe280-il | 1,000,000 | 5 | 87.3 at α=4.75° | 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 | |
| s3010-il | 50,000 | 9 | 28.5 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s3010-il | 50,000 | 5 | 36.2 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s3010-il | 100,000 | 9 | 50.2 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s3010-il | 100,000 | 5 | 52.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s3010-il | 200,000 | 9 | 70 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s3010-il | 200,000 | 5 | 68.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s3010-il | 500,000 | 9 | 95.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s3010-il | 500,000 | 5 | 89.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s3010-il | 1,000,000 | 9 | 113.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s3010-il | 1,000,000 | 5 | 104.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxl142k-il | 50,000 | 9 | 27.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxl142k-il | 50,000 | 5 | 28.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxl142k-il | 100,000 | 9 | 42.1 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxl142k-il | 100,000 | 5 | 39.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxl142k-il | 200,000 | 9 | 54.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxl142k-il | 200,000 | 5 | 47.5 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxl142k-il | 500,000 | 9 | 63.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxl142k-il | 500,000 | 5 | 60.6 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fxl142k-il | 1,000,000 | 9 | 75.2 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fxl142k-il | 1,000,000 | 5 | 72.1 at α=11.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e335-il | 50,000 | 9 | 15.9 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e335-il | 50,000 | 5 | 25.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e335-il | 100,000 | 9 | 38.3 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e335-il | 100,000 | 5 | 44.2 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e335-il | 200,000 | 9 | 60.4 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e335-il | 200,000 | 5 | 58.7 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e335-il | 500,000 | 9 | 81.3 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e335-il | 500,000 | 5 | 72 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e335-il | 1,000,000 | 9 | 90.1 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e335-il | 1,000,000 | 5 | 88.7 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e856-il | 50,000 | 9 | 4.6 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e856-il | 50,000 | 5 | 18.8 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e856-il | 100,000 | 9 | 28.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e856-il | 100,000 | 5 | 46.3 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e856-il | 200,000 | 9 | 64.8 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e856-il | 200,000 | 5 | 70.1 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e856-il | 500,000 | 9 | 100.8 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e856-il | 500,000 | 5 | 99.7 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e856-il | 1,000,000 | 9 | 128.9 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e856-il | 1,000,000 | 5 | 118.5 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la5055-il | 50,000 | 9 | 4.9 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la5055-il | 50,000 | 5 | 8.7 at α=13.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la5055-il | 100,000 | 9 | 18.7 at α=15.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la5055-il | 100,000 | 5 | 15.5 at α=13.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la5055-il | 200,000 | 9 | 24.7 at α=13.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la5055-il | 200,000 | 5 | 46.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la5055-il | 500,000 | 9 | 116.3 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la5055-il | 500,000 | 5 | 104.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| la5055-il | 1,000,000 | 9 | 149.6 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| la5055-il | 1,000,000 | 5 | 83.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx79l100-il | 50,000 | 9 | 27.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx79l100-il | 50,000 | 5 | 27 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx79l100-il | 100,000 | 9 | 38.6 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx79l100-il | 100,000 | 5 | 35.9 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx79l100-il | 200,000 | 9 | 50.1 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx79l100-il | 200,000 | 5 | 41.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx79l100-il | 500,000 | 9 | 58 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx79l100-il | 500,000 | 5 | 58.1 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx79l100-il | 1,000,000 | 9 | 70.6 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx79l100-il | 1,000,000 | 5 | 72.7 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e212-il | 50,000 | 9 | 38.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e212-il | 50,000 | 5 | 40.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e212-il | 100,000 | 9 | 59.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e212-il | 100,000 | 5 | 58.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e212-il | 200,000 | 9 | 81.7 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e212-il | 200,000 | 5 | 75.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e212-il | 500,000 | 9 | 108.4 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e212-il | 500,000 | 5 | 91.7 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e212-il | 1,000,000 | 9 | 119.8 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e212-il | 1,000,000 | 5 | 101 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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