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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(naca664221-il) NACA 66(4)-221 | NACA 66(4)-221 airfoil Max thickness 21% at 45% chord Max camber 1.1% at 50% chord | Remove Airfoil details Airfoil plotter |
(mh62-il) MH 62 9.3% | Martin Hepperle MH 62 for flying wings Max thickness 9.3% at 26.9% chord Max camber 1.6% at 36.6% chord | Remove Airfoil details Airfoil plotter |
(nl722343-il) NLR-7223-43 AIRFOIL | NLR NLR-7223-43 transonic rotorcraft airfoil Max thickness 8.6% at 38% chord Max camber 1.3% at 74% chord | Remove Airfoil details Airfoil plotter |
(n64215-il) NACA 64-215 AIRFOIL | NACA 64(2)-215 airfoil Max thickness 15% at 34.9% chord Max camber 1.1% at 50% chord | Remove Airfoil details Airfoil plotter |
(naca66206-il) NACA 66-206 | NACA 66-206 airfoil Max thickness 6% at 45% chord Max camber 1.1% at 50% chord | Remove Airfoil details Airfoil plotter |
(goe318-il) GOE 318 (HANSA-BRANDENBURG VI.5) AIRFOIL | Gottingen 318 (Hansa-Brandenburg VI.5) airfoil Max thickness 9.1% at 29.9% chord Max camber 4.3% at 29.9% chord | Remove Airfoil details Airfoil plotter |
(naca16009-il) NACA 16009 | NACA 16009 airfoil Max thickness 9% at 50% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(goe803h-il) GOE 803 (HACKLINGER) AIRFOIL | Gottingen 803 (Hacklinger) airfoil Max thickness 6.3% at 15% chord Max camber 6.6% at 40% chord | Remove Airfoil details Airfoil plotter |
(mh93-il) MH 93 15.98% | Martin Hepperle MH 93 parafoil Max thickness 16% at 27.6% chord Max camber 1.4% at 15.2% chord | Remove Airfoil details Airfoil plotter |
(naca0021-il) NACA 0021 | NACA 0021 airfoil Max thickness 21% at 30% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(mh114-il) MH 114 13.02% | Martin Hepperle MH 114 for a propeller for ultralight Max thickness 13% at 28.1% chord Max camber 6.4% at 50% chord | Remove Airfoil details Airfoil plotter |
(mh106-il) MH 106 13.07% | Martin Hepperle MH 106 for stall controlled wind turbines Max thickness 13.1% at 27.4% chord Max camber 0.9% at 27.4% chord | Remove Airfoil details Airfoil plotter |
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Polars for (naca664221-il,mh62-il,nl722343-il,n64215-il,naca66206-il,goe318-il,naca16009-il,goe803h-il,mh93-il,naca0021-il,mh114-il,mh106-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| naca664221-il | 50,000 | 9 | 16.5 at α=12.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca664221-il | 50,000 | 5 | 12.2 at α=11.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca664221-il | 100,000 | 9 | 19.1 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca664221-il | 100,000 | 5 | 18.1 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca664221-il | 200,000 | 9 | 29.6 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca664221-il | 200,000 | 5 | 30.5 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca664221-il | 500,000 | 9 | 68.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca664221-il | 500,000 | 5 | 69.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca664221-il | 1,000,000 | 9 | 100.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca664221-il | 1,000,000 | 5 | 91.7 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh62-il | 50,000 | 9 | 28.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh62-il | 50,000 | 5 | 33.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh62-il | 100,000 | 9 | 45 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh62-il | 100,000 | 5 | 46 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh62-il | 200,000 | 9 | 60.4 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh62-il | 200,000 | 5 | 58.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh62-il | 500,000 | 9 | 80.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh62-il | 500,000 | 5 | 75 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh62-il | 1,000,000 | 9 | 94.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh62-il | 1,000,000 | 5 | 87.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nl722343-il | 50,000 | 9 | 30.4 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nl722343-il | 50,000 | 5 | 29.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nl722343-il | 100,000 | 9 | 42.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nl722343-il | 100,000 | 5 | 41.4 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nl722343-il | 200,000 | 9 | 53.6 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nl722343-il | 200,000 | 5 | 53.1 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nl722343-il | 500,000 | 9 | 70.2 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nl722343-il | 500,000 | 5 | 67.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nl722343-il | 1,000,000 | 9 | 82.6 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nl722343-il | 1,000,000 | 5 | 78.1 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64215-il | 50,000 | 9 | 28.3 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64215-il | 50,000 | 5 | 26.6 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64215-il | 100,000 | 9 | 47.6 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64215-il | 100,000 | 5 | 44.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64215-il | 200,000 | 9 | 63.1 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64215-il | 200,000 | 5 | 58.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64215-il | 500,000 | 9 | 85.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64215-il | 500,000 | 5 | 73.7 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64215-il | 1,000,000 | 9 | 99.2 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64215-il | 1,000,000 | 5 | 79.3 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca66206-il | 50,000 | 9 | 20.9 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca66206-il | 50,000 | 5 | 22.6 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca66206-il | 100,000 | 9 | 28.4 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca66206-il | 100,000 | 5 | 35.9 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca66206-il | 200,000 | 9 | 52.9 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca66206-il | 200,000 | 5 | 50.7 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca66206-il | 500,000 | 9 | 71.7 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca66206-il | 500,000 | 5 | 59.4 at α=1.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca66206-il | 1,000,000 | 9 | 76.3 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca66206-il | 1,000,000 | 5 | 66.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe318-il | 50,000 | 9 | 20.7 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe318-il | 50,000 | 5 | 35.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe318-il | 100,000 | 9 | 50.4 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe318-il | 100,000 | 5 | 53.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe318-il | 200,000 | 9 | 69 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe318-il | 200,000 | 5 | 70 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe318-il | 500,000 | 9 | 93.3 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe318-il | 500,000 | 5 | 92.1 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe318-il | 1,000,000 | 9 | 113.9 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe318-il | 1,000,000 | 5 | 111 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca16009-il | 50,000 | 9 | 18 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca16009-il | 50,000 | 5 | 19.8 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca16009-il | 100,000 | 9 | 25.1 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca16009-il | 100,000 | 5 | 28.8 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca16009-il | 200,000 | 9 | 39.4 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca16009-il | 200,000 | 5 | 34.6 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca16009-il | 500,000 | 9 | 44.6 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca16009-il | 500,000 | 5 | 38 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca16009-il | 1,000,000 | 9 | 47 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca16009-il | 1,000,000 | 5 | 47.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe803h-il | 50,000 | 9 | 40 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe803h-il | 50,000 | 5 | 48.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe803h-il | 100,000 | 9 | 69.1 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe803h-il | 100,000 | 5 | 69.7 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe803h-il | 200,000 | 9 | 95.6 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe803h-il | 200,000 | 5 | 85.8 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe803h-il | 500,000 | 9 | 112.9 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe803h-il | 500,000 | 5 | 103.6 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe803h-il | 1,000,000 | 9 | 128.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe803h-il | 1,000,000 | 5 | 122.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh93-il | 50,000 | 9 | 14.6 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh93-il | 50,000 | 5 | 24.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh93-il | 100,000 | 9 | 33.4 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh93-il | 100,000 | 5 | 39.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh93-il | 200,000 | 9 | 52.5 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh93-il | 200,000 | 5 | 53.2 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh93-il | 500,000 | 9 | 74.4 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh93-il | 500,000 | 5 | 71.3 at α=10.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh93-il | 1,000,000 | 9 | 92 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh93-il | 1,000,000 | 5 | 88.9 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca0021-il | 50,000 | 9 | 19.1 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca0021-il | 50,000 | 5 | 25.2 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca0021-il | 100,000 | 9 | 36.6 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca0021-il | 100,000 | 5 | 35.6 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca0021-il | 200,000 | 9 | 48 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca0021-il | 200,000 | 5 | 43.6 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca0021-il | 500,000 | 9 | 60.6 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca0021-il | 500,000 | 5 | 56.8 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca0021-il | 1,000,000 | 9 | 74.7 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca0021-il | 1,000,000 | 5 | 71 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh114-il | 50,000 | 9 | 9.4 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh114-il | 50,000 | 5 | 26 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh114-il | 100,000 | 9 | 56.2 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh114-il | 100,000 | 5 | 60.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh114-il | 200,000 | 9 | 89.7 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh114-il | 200,000 | 5 | 88.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh114-il | 500,000 | 9 | 131.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh114-il | 500,000 | 5 | 121 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh114-il | 1,000,000 | 9 | 161 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh114-il | 1,000,000 | 5 | 140.6 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh106-il | 50,000 | 9 | 14.9 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh106-il | 50,000 | 5 | 27.3 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh106-il | 100,000 | 9 | 42.1 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh106-il | 100,000 | 5 | 44.6 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh106-il | 200,000 | 9 | 61.4 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh106-il | 200,000 | 5 | 60.6 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh106-il | 500,000 | 9 | 86.6 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh106-il | 500,000 | 5 | 79.7 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh106-il | 1,000,000 | 9 | 103.6 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh106-il | 1,000,000 | 5 | 87.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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