Airfoil Comparison
Select airfoils from the airfoil database or add your own airfoils and compare the airfoil shape and lift/drag polars.
| Open full size plan in new window | Open paginated plan in new window | |
| Download PDF file | SVG image as text file | |
| Clear all | ||
(hs1404-il) HAM-STD HS1-404 AIRFOIL | HS1 family of prop airfoils from US Patent No. 4 Max thickness 4% at 18% chord Max camber 3.1% at 46% chord | Remove Airfoil details Airfoil plotter |
(goe08k-il) GOE 8K AIRFOIL | Gottingen 8K airfoil Max thickness 14.9% at 50% chord Max camber 6.1% at 50% chord | Remove Airfoil details Airfoil plotter |
(e182-il) E182 (8.47%) | Eppler E182 low Reynolds number airfoil Max thickness 8.5% at 32.4% chord Max camber 1.2% at 37.5% chord | Remove Airfoil details Airfoil plotter |
(s808-nr) NREL's S808 Airfoil | NREL HAWT airfoil S808 root Max thickness 21% at 24.4% chord Max camber 2.4% at 72.9% chord | Remove Airfoil details Airfoil plotter |
(goe596-il) GOE 596 AIRFOIL | Gottingen 596 airfoil Max thickness 9.8% at 30% chord Max camber 4% at 40% chord | Remove Airfoil details Airfoil plotter |
(e176-il) E176 (8.83%) | Eppler E176 low Reynolds number airfoil Max thickness 8.8% at 30.5% chord Max camber 2.9% at 44.2% chord | Remove Airfoil details Airfoil plotter |
(nacam2-il) NACA M2 | NACA M2 airfoil Max thickness 8.1% at 30% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(goe564-il) GOE 564 AIRFOIL | Gottingen 564 airfoil Max thickness 8.2% at 30% chord Max camber 2.7% at 40% chord | Remove Airfoil details Airfoil plotter |
(n64015-il) NACA 642-015 AIRFOIL | NACA 64(2)-015 airfoil Max thickness 15% at 35% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(naca23015-il) NACA 23015 | NACA 23015 airfoil Max thickness 15% at 30% chord Max camber 1.8% at 15% chord | Remove Airfoil details Airfoil plotter |
(e228-il) E10(08%) | Eppler E228 low Reynolds number airfoil Max thickness 10.1% at 31.9% chord Max camber 0.3% at 31.9% chord | Remove Airfoil details Airfoil plotter |
(fg3-il) Fage & Collins 3 | Fage & Collins 3 airfoil Max thickness 10.1% at 30% chord Max camber 4.3% at 30% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (hs1404-il,goe08k-il,e182-il,s808-nr,goe596-il,e176-il,nacam2-il,goe564-il,n64015-il,naca23015-il,e228-il,fg3-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| hs1404-il | 50,000 | 9 | 42.1 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hs1404-il | 50,000 | 5 | 42.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hs1404-il | 100,000 | 5 | 59.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hs1404-il | 200,000 | 9 | 84.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hs1404-il | 200,000 | 5 | 78.6 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hs1404-il | 500,000 | 9 | 114.7 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hs1404-il | 500,000 | 5 | 102.2 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hs1404-il | 1,000,000 | 9 | 134.6 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hs1404-il | 1,000,000 | 5 | 113.3 at α=1.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe08k-il | 50,000 | 9 | 18 at α=14° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe08k-il | 50,000 | 5 | 15.7 at α=12.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe08k-il | 100,000 | 9 | 26.9 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe08k-il | 100,000 | 5 | 24.1 at α=11.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe08k-il | 200,000 | 9 | 44.4 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe08k-il | 200,000 | 5 | 43.5 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe08k-il | 500,000 | 9 | 103.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe08k-il | 500,000 | 5 | 96.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe08k-il | 1,000,000 | 9 | 143.1 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe08k-il | 1,000,000 | 5 | 122 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e182-il | 50,000 | 9 | 32.8 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e182-il | 50,000 | 5 | 34.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e182-il | 100,000 | 9 | 48.5 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e182-il | 100,000 | 5 | 47 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e182-il | 200,000 | 9 | 64.1 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e182-il | 200,000 | 5 | 58.8 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e182-il | 500,000 | 9 | 81.9 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e182-il | 500,000 | 5 | 71.3 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e182-il | 1,000,000 | 9 | 92.7 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e182-il | 1,000,000 | 5 | 78.2 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s808-nr | 50,000 | 9 | 8.2 at α=0° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s808-nr | 50,000 | 5 | 24.6 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s808-nr | 100,000 | 9 | 36.5 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s808-nr | 100,000 | 5 | 41.4 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s808-nr | 200,000 | 9 | 55.1 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s808-nr | 200,000 | 5 | 56 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s808-nr | 500,000 | 9 | 78.9 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s808-nr | 500,000 | 5 | 76.6 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s808-nr | 1,000,000 | 9 | 98.5 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s808-nr | 1,000,000 | 5 | 92.8 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe596-il | 50,000 | 9 | 35.5 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe596-il | 50,000 | 5 | 37 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe596-il | 100,000 | 9 | 56.6 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe596-il | 100,000 | 5 | 57.4 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe596-il | 200,000 | 9 | 77.5 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe596-il | 200,000 | 5 | 75.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe596-il | 500,000 | 9 | 105.7 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe596-il | 500,000 | 5 | 97.2 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe596-il | 1,000,000 | 9 | 125.7 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe596-il | 1,000,000 | 5 | 112.5 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e176-il | 50,000 | 9 | 37.7 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e176-il | 50,000 | 5 | 38.7 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e176-il | 100,000 | 9 | 59.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e176-il | 100,000 | 5 | 58.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e176-il | 200,000 | 9 | 81.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e176-il | 200,000 | 5 | 78.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e176-il | 500,000 | 9 | 110.7 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e176-il | 500,000 | 5 | 103.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e176-il | 1,000,000 | 9 | 132.9 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e176-il | 1,000,000 | 5 | 119.6 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nacam2-il | 50,000 | 9 | 25.5 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nacam2-il | 50,000 | 5 | 23.6 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nacam2-il | 100,000 | 9 | 33.2 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nacam2-il | 100,000 | 5 | 27.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nacam2-il | 200,000 | 9 | 38.6 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nacam2-il | 200,000 | 5 | 36.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nacam2-il | 500,000 | 9 | 44.5 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nacam2-il | 500,000 | 5 | 54.4 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nacam2-il | 1,000,000 | 9 | 60.3 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nacam2-il | 1,000,000 | 5 | 70.5 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe564-il | 50,000 | 9 | 37.1 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe564-il | 50,000 | 5 | 37.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe564-il | 100,000 | 9 | 56 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe564-il | 100,000 | 5 | 52.6 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe564-il | 200,000 | 9 | 75.4 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe564-il | 200,000 | 5 | 65.6 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe564-il | 500,000 | 9 | 95.7 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe564-il | 500,000 | 5 | 77.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe564-il | 1,000,000 | 9 | 103.8 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe564-il | 1,000,000 | 5 | 89.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64015-il | 50,000 | 9 | 27.6 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64015-il | 50,000 | 5 | 27 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64015-il | 100,000 | 9 | 40.3 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64015-il | 100,000 | 5 | 35.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64015-il | 200,000 | 9 | 48.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64015-il | 200,000 | 5 | 45 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64015-il | 500,000 | 9 | 65.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64015-il | 500,000 | 5 | 52.6 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64015-il | 1,000,000 | 9 | 72.4 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64015-il | 1,000,000 | 5 | 65 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23015-il | 50,000 | 9 | 21 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23015-il | 50,000 | 5 | 27.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23015-il | 100,000 | 9 | 33.7 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23015-il | 100,000 | 5 | 39.1 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23015-il | 200,000 | 9 | 48.4 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23015-il | 200,000 | 5 | 52.6 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23015-il | 500,000 | 9 | 72 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23015-il | 500,000 | 5 | 74.8 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca23015-il | 1,000,000 | 9 | 91 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca23015-il | 1,000,000 | 5 | 91.3 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e228-il | 50,000 | 9 | 27 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e228-il | 50,000 | 5 | 28.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e228-il | 100,000 | 9 | 39.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e228-il | 100,000 | 5 | 38.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e228-il | 200,000 | 9 | 51.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e228-il | 200,000 | 5 | 48.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e228-il | 500,000 | 9 | 66.2 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e228-il | 500,000 | 5 | 61.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e228-il | 1,000,000 | 9 | 75.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e228-il | 1,000,000 | 5 | 71.6 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fg3-il | 50,000 | 9 | 32.7 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fg3-il | 50,000 | 5 | 35.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fg3-il | 100,000 | 9 | 48.8 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fg3-il | 100,000 | 5 | 49.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fg3-il | 200,000 | 9 | 65.1 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fg3-il | 200,000 | 5 | 65.3 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fg3-il | 500,000 | 9 | 90.4 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fg3-il | 500,000 | 5 | 89 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fg3-il | 1,000,000 | 9 | 111.9 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fg3-il | 1,000,000 | 5 | 108.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| Reynolds number calculator | |||||||