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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(goe362-il) GOE 362 AIRFOIL | Gottingen 362 airfoil Max thickness 6.6% at 20% chord Max camber 5.3% at 40% chord | Remove Airfoil details Airfoil plotter |
(e68-il) EPPLER 68 AIRFOIL | Eppler E68 low Reynolds number airfoil Max thickness 13.1% at 32% chord Max camber 3.3% at 50.9% chord | Remove Airfoil details Airfoil plotter |
(e423-il) E423 | Eppler E423 high lift airfoil Max thickness 12.5% at 23.7% chord Max camber 9.5% at 41.4% chord | Remove Airfoil details Airfoil plotter |
(e205-il) E205 (10.48%) | Eppler E205 low Reynolds number airfoil Max thickness 10.5% at 29.7% chord Max camber 2.5% at 38.7% chord | Remove Airfoil details Airfoil plotter |
(mh112-il) MH 112 Airfoil | Martin Hepperle MH 112 for a propeller for ultralight (root) Max thickness 16.2% at 31.8% chord Max camber 6.7% at 48.5% chord | Remove Airfoil details Airfoil plotter |
(miley-il) MILEY M06-13-128 | Miley MO6-13-128 airfoil Max thickness 12.9% at 35% chord Max camber 4.9% at 35% chord | Remove Airfoil details Airfoil plotter |
(e562-il) EPPLER 562 AIRFOIL | Eppler E562 general aviation airfoil Max thickness 15% at 27.6% chord Max camber 4% at 50.8% chord | Remove Airfoil details Airfoil plotter |
(rg1410-il) RG 14 10% AIRFOIL | Rolf Girsberger RG 14 (10%) airfoil Max thickness 10% at 31% chord Max camber 1.6% at 36% chord | Remove Airfoil details Airfoil plotter |
(goe322-il) GOE 322 (HANSA-BRANDENBURG IV.1) AIRFOIL | Gottingen 322 (Hansa-Brandenburg IV.1) airfoil Max thickness 13.1% at 29.8% chord Max camber 6% at 29.8% chord | Remove Airfoil details Airfoil plotter |
(s2060-il) S2060 8% | Selig S2060 low Reynolds number airfoil Max thickness 8% at 30.2% chord Max camber 1.6% at 49.7% chord | Remove Airfoil details Airfoil plotter |
(raf48-il) RAF-48 AIRFOIL | RAF-48 airfoil Max thickness 15% at 30% chord Max camber 2.9% at 40% chord | Remove Airfoil details Airfoil plotter |
(e379-il) EPPLER 379 AIRFOIL | Eppler E379 ultralight airfoil Max thickness 2.2% at 5.8% chord Max camber 8% at 31.8% chord | Remove Airfoil details Airfoil plotter |
(goe527-il) GOE 527 AIRFOIL | Gottingen 527 airfoil Max thickness 16.5% at 29.5% chord Max camber 5.8% at 39.5% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (goe362-il,e68-il,e423-il,e205-il,mh112-il,miley-il,e562-il,rg1410-il,goe322-il,s2060-il,raf48-il,e379-il,goe527-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe362-il | 50,000 | 9 | 37.3 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe362-il | 50,000 | 5 | 43.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe362-il | 100,000 | 9 | 58.4 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe362-il | 100,000 | 5 | 63.3 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe362-il | 200,000 | 9 | 79.6 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe362-il | 200,000 | 5 | 81.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe362-il | 500,000 | 9 | 109.4 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe362-il | 500,000 | 5 | 108.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe362-il | 1,000,000 | 9 | 131.4 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe362-il | 1,000,000 | 5 | 127.7 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e68-il | 50,000 | 9 | 33.7 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e68-il | 50,000 | 5 | 32.7 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e68-il | 100,000 | 9 | 56.8 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e68-il | 100,000 | 5 | 56.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e68-il | 200,000 | 9 | 82.2 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e68-il | 200,000 | 5 | 78.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e68-il | 500,000 | 9 | 114.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e68-il | 500,000 | 5 | 102.6 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e68-il | 1,000,000 | 9 | 136.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e68-il | 1,000,000 | 5 | 114.1 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e423-il | 50,000 | 9 | 6 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e423-il | 50,000 | 5 | 13.9 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e423-il | 100,000 | 9 | 12.5 at α=0.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e423-il | 100,000 | 5 | 51.9 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e423-il | 200,000 | 9 | 73.7 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e423-il | 200,000 | 5 | 84.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e423-il | 500,000 | 9 | 123.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e423-il | 500,000 | 5 | 120.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e423-il | 1,000,000 | 9 | 156.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e423-il | 1,000,000 | 5 | 145.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e205-il | 50,000 | 9 | 32.6 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e205-il | 50,000 | 5 | 34.5 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e205-il | 100,000 | 9 | 53.9 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e205-il | 100,000 | 5 | 54.9 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e205-il | 200,000 | 9 | 75.6 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e205-il | 200,000 | 5 | 74 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e205-il | 500,000 | 9 | 105.4 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e205-il | 500,000 | 5 | 98.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e205-il | 1,000,000 | 9 | 128.3 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e205-il | 1,000,000 | 5 | 116.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh112-il | 50,000 | 9 | 5.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh112-il | 50,000 | 5 | 14.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh112-il | 100,000 | 9 | 37.5 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh112-il | 100,000 | 5 | 48.6 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh112-il | 200,000 | 9 | 80 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh112-il | 200,000 | 5 | 79.4 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh112-il | 500,000 | 9 | 120 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh112-il | 500,000 | 5 | 109.7 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh112-il | 1,000,000 | 9 | 147.7 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh112-il | 1,000,000 | 5 | 126.6 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| miley-il | 50,000 | 9 | 5.8 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| miley-il | 50,000 | 5 | 11 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| miley-il | 100,000 | 9 | 23.5 at α=13° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| miley-il | 100,000 | 5 | 23.2 at α=12.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| miley-il | 200,000 | 9 | 61.2 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| miley-il | 200,000 | 5 | 62.8 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| miley-il | 500,000 | 9 | 122.8 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| miley-il | 500,000 | 5 | 121.4 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| miley-il | 1,000,000 | 9 | 168 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| miley-il | 1,000,000 | 5 | 157.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e562-il | 50,000 | 9 | 11.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e562-il | 50,000 | 5 | 33.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e562-il | 100,000 | 9 | 49.3 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e562-il | 100,000 | 5 | 55.3 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e562-il | 200,000 | 9 | 73.8 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e562-il | 200,000 | 5 | 74.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e562-il | 500,000 | 9 | 104.9 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e562-il | 500,000 | 5 | 100.7 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e562-il | 1,000,000 | 9 | 129.4 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e562-il | 1,000,000 | 5 | 115.1 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rg1410-il | 50,000 | 9 | 32.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rg1410-il | 50,000 | 5 | 33.6 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rg1410-il | 100,000 | 9 | 48.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rg1410-il | 100,000 | 5 | 46.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rg1410-il | 200,000 | 9 | 63.5 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rg1410-il | 200,000 | 5 | 58.1 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rg1410-il | 500,000 | 9 | 82.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rg1410-il | 500,000 | 5 | 71.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rg1410-il | 1,000,000 | 9 | 89.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rg1410-il | 1,000,000 | 5 | 85.5 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe322-il | 50,000 | 9 | 9.2 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe322-il | 50,000 | 5 | 28.9 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe322-il | 100,000 | 9 | 49.9 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe322-il | 100,000 | 5 | 53.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe322-il | 200,000 | 9 | 75.2 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe322-il | 200,000 | 5 | 73.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe322-il | 500,000 | 9 | 104.8 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe322-il | 500,000 | 5 | 95.7 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe322-il | 1,000,000 | 9 | 123.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe322-il | 1,000,000 | 5 | 114.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2060-il | 50,000 | 9 | 36.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2060-il | 50,000 | 5 | 36.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2060-il | 100,000 | 9 | 53.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2060-il | 100,000 | 5 | 50.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2060-il | 200,000 | 9 | 70.9 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2060-il | 200,000 | 5 | 62.9 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2060-il | 500,000 | 9 | 91 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2060-il | 500,000 | 5 | 75.1 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2060-il | 1,000,000 | 9 | 101.5 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2060-il | 1,000,000 | 5 | 79 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf48-il | 50,000 | 9 | 7.4 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf48-il | 50,000 | 5 | 25.8 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf48-il | 100,000 | 9 | 45.6 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf48-il | 100,000 | 5 | 49.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf48-il | 200,000 | 9 | 68.5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf48-il | 200,000 | 5 | 67.8 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf48-il | 500,000 | 9 | 97.8 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf48-il | 500,000 | 5 | 93.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf48-il | 1,000,000 | 9 | 121.8 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf48-il | 1,000,000 | 5 | 108.1 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e379-il | 50,000 | 9 | 23.2 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e379-il | 50,000 | 5 | 40.6 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e379-il | 100,000 | 9 | 74.6 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e379-il | 100,000 | 5 | 66.8 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e379-il | 200,000 | 9 | 117.8 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e379-il | 200,000 | 5 | 91.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e379-il | 500,000 | 9 | 128 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e379-il | 500,000 | 5 | 118.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e379-il | 1,000,000 | 0 | 135.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe527-il | 50,000 | 9 | 4.3 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe527-il | 50,000 | 5 | 15.9 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe527-il | 100,000 | 9 | 36.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe527-il | 100,000 | 5 | 47 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe527-il | 200,000 | 9 | 69.5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe527-il | 200,000 | 5 | 69.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe527-il | 500,000 | 9 | 102.3 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe527-il | 500,000 | 5 | 96.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe527-il | 1,000,000 | 9 | 128.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe527-il | 1,000,000 | 5 | 116.9 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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