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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(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 |
(mh44-il) MH 44 9.66% | Martin Hepperle MH 44 for flying wings Max thickness 9.6% at 27.1% chord Max camber 1.5% at 36.9% chord | Remove Airfoil details Airfoil plotter |
(mh20-il) MH 20 9.01% | Martin Hepperle MH 20 for F3D Pylon Racing Max thickness 9% at 32.2% chord Max camber 1.9% at 37.3% chord | Remove Airfoil details Airfoil plotter |
(mh46-il) MH 46 9.1% | Martin Hepperle MH 46 for flying wings Max thickness 9.1% at 27.1% chord Max camber 1.4% at 36.9% 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 |
(n13-il) N-13 | N-13 airfoil Max thickness 11.8% at 30% chord Max camber 0.1% at 95% chord | Remove Airfoil details Airfoil plotter |
(n11-il) N-11 | N-11 airfoil Max thickness 10.9% at 30% chord Max camber 4.4% at 40% chord | Remove Airfoil details Airfoil plotter |
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Polars for (mh112-il,mh44-il,mh20-il,mh46-il,mh93-il,n13-il,n11-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| 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 | |
| mh44-il | 50,000 | 9 | 29.1 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh44-il | 50,000 | 5 | 32.8 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh44-il | 100,000 | 9 | 44.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh44-il | 100,000 | 5 | 45.6 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh44-il | 200,000 | 9 | 60.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh44-il | 200,000 | 5 | 58.1 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh44-il | 500,000 | 9 | 80.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh44-il | 500,000 | 5 | 74.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh44-il | 1,000,000 | 9 | 94.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh44-il | 1,000,000 | 5 | 87.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh20-il | 50,000 | 9 | 33.7 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh20-il | 50,000 | 5 | 34.9 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh20-il | 100,000 | 9 | 50.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh20-il | 100,000 | 5 | 50.1 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh20-il | 200,000 | 9 | 68.7 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh20-il | 200,000 | 5 | 64.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh20-il | 500,000 | 9 | 91.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh20-il | 500,000 | 5 | 81.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh20-il | 1,000,000 | 9 | 105.5 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh20-il | 1,000,000 | 5 | 93.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh46-il | 50,000 | 9 | 30.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh46-il | 50,000 | 5 | 33.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh46-il | 100,000 | 9 | 46 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh46-il | 100,000 | 5 | 46.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh46-il | 200,000 | 9 | 61.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh46-il | 200,000 | 5 | 58.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh46-il | 500,000 | 9 | 81.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh46-il | 500,000 | 5 | 74.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh46-il | 1,000,000 | 9 | 94.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh46-il | 1,000,000 | 5 | 85.3 at α=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 | |
| n13-il | 50,000 | 9 | 29 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n13-il | 50,000 | 5 | 27.7 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n13-il | 100,000 | 9 | 41.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n13-il | 100,000 | 5 | 37.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n13-il | 200,000 | 9 | 49.4 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n13-il | 200,000 | 5 | 45.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n13-il | 500,000 | 9 | 60.2 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n13-il | 500,000 | 5 | 60.8 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n13-il | 1,000,000 | 9 | 73.1 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n13-il | 1,000,000 | 5 | 71 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n11-il | 50,000 | 9 | 27.1 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n11-il | 50,000 | 5 | 38.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n11-il | 100,000 | 9 | 54.6 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n11-il | 100,000 | 5 | 56.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n11-il | 200,000 | 9 | 75.6 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n11-il | 200,000 | 5 | 72 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n11-il | 500,000 | 9 | 100.9 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n11-il | 500,000 | 5 | 93.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n11-il | 1,000,000 | 9 | 118.4 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n11-il | 1,000,000 | 5 | 111.6 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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