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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(goe371-il) GOE 371 AIRFOIL | Gottingen 371 airfoil Max thickness 7% at 29.9% chord Max camber 4.6% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(naca1410-il) NACA 1410 | NACA 1410 airfoil Max thickness 10% at 29.9% chord Max camber 1% at 50% chord | Remove Airfoil details Airfoil plotter |
(goe388-il) GOE 388 AIRFOIL | Gottingen 388 airfoil Max thickness 10.2% at 29.9% chord Max camber 5.4% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(mh26-il) MH 26 10.99% | Martin Hepperle MH 26 for F3D Pylon Racing (extended laminar flow) Max thickness 11% at 42.3% chord Max camber 1.4% at 42.3% 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 |
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Polars for (goe371-il,naca1410-il,goe388-il,mh26-il,nacam18-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe371-il | 50,000 | 9 | 37.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe371-il | 50,000 | 5 | 43.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe371-il | 100,000 | 9 | 61.1 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe371-il | 100,000 | 5 | 62.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe371-il | 200,000 | 9 | 82 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe371-il | 200,000 | 5 | 80 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe371-il | 500,000 | 9 | 108.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe371-il | 500,000 | 5 | 103.9 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe371-il | 1,000,000 | 9 | 129.8 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe371-il | 1,000,000 | 5 | 120.9 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca1410-il | 50,000 | 9 | 31.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca1410-il | 50,000 | 5 | 31.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca1410-il | 100,000 | 9 | 44.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca1410-il | 100,000 | 5 | 42.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca1410-il | 200,000 | 9 | 56.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca1410-il | 200,000 | 5 | 50.6 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca1410-il | 500,000 | 9 | 70.8 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca1410-il | 500,000 | 5 | 63.6 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca1410-il | 1,000,000 | 9 | 78.9 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca1410-il | 1,000,000 | 5 | 78.3 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe388-il | 50,000 | 9 | 41.4 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe388-il | 50,000 | 5 | 36.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe388-il | 100,000 | 9 | 55.8 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe388-il | 100,000 | 5 | 37.6 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe388-il | 200,000 | 9 | 34.7 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe388-il | 200,000 | 5 | 36.2 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe388-il | 500,000 | 9 | 40.2 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe388-il | 500,000 | 5 | 41.6 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe388-il | 1,000,000 | 9 | 53.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe388-il | 1,000,000 | 5 | 67.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh26-il | 50,000 | 9 | 34.3 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh26-il | 50,000 | 5 | 32 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh26-il | 100,000 | 9 | 51.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh26-il | 100,000 | 5 | 47.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh26-il | 200,000 | 9 | 71.2 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh26-il | 200,000 | 5 | 57.8 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh26-il | 500,000 | 9 | 77.8 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh26-il | 500,000 | 5 | 58.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh26-il | 1,000,000 | 9 | 74.8 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh26-il | 1,000,000 | 5 | 66.2 at α=7.5° | 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 | |
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