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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(mh81-il) MH 81 13% | Martin Hepperle MH 81 for flying wings (hang glider) Max thickness 12.9% at 25.4% chord Max camber 3.3% at 25.4% chord | Remove Airfoil details Airfoil plotter |
(mh24-il) MH 24 9.01% | Martin Hepperle MH 24 for F3D Pylon Racing (extended laminar flow) Max thickness 9% at 37.3% chord Max camber 1.2% at 37.3% 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 |
(mh42-il) MH 42 8.94% | Martin Hepperle MH 42 low Reynolds number airfoil Max thickness 8.9% at 31.3% chord Max camber 1.8% at 36.3% chord | Remove Airfoil details Airfoil plotter |
(mh83-il) MH 83 13.29% | Martin Hepperle MH 83 for flying wings (hang glider) Max thickness 13.3% at 20.6% chord Max camber 4.5% at 32.6% 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 |
(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 |
(mh30-il) MH 30 7.84% | Martin Hepperle MH 30 for F3E and F3B Max thickness 7.8% at 31% chord Max camber 1.7% at 46.4% chord | Remove Airfoil details Airfoil plotter |
(mh82-il) MH 82 13.31% | Martin Hepperle MH 82 for flying wings (hang glider) Max thickness 13.3% at 24.6% chord Max camber 3.9% at 24.6% chord | Remove Airfoil details Airfoil plotter |
(mh200-il) MH 200 12.97% | Martin Hepperle MH 200 for a canard airplane (main wing) Max thickness 13% at 39.5% chord Max camber 2.1% at 49.8% chord | Remove Airfoil details Airfoil plotter |
(mh60-il) MH 60 10.08% | Martin Hepperle MH 60 for flying wings Max thickness 10.1% at 26.9% chord Max camber 1.7% at 36.6% chord | Remove Airfoil details Airfoil plotter |
(mh43-il) MH 43 8.5% | Martin Hepperle MH 43 for F3B and F3E Max thickness 8.5% at 31.4% chord Max camber 1.7% at 36.4% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (mh81-il,mh24-il,mh44-il,mh42-il,mh83-il,mh112-il,mh46-il,mh30-il,mh82-il,mh200-il,mh60-il,mh43-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh81-il | 50,000 | 9 | 11.8 at α=1° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh81-il | 50,000 | 5 | 23 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh81-il | 100,000 | 9 | 28.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh81-il | 100,000 | 5 | 41 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh81-il | 200,000 | 9 | 52 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh81-il | 200,000 | 5 | 60.1 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh81-il | 500,000 | 9 | 85.1 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh81-il | 500,000 | 5 | 88.3 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh81-il | 1,000,000 | 9 | 112.7 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh81-il | 1,000,000 | 5 | 111.9 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh24-il | 50,000 | 9 | 34.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh24-il | 50,000 | 5 | 33 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh24-il | 100,000 | 9 | 50.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh24-il | 100,000 | 5 | 47 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh24-il | 200,000 | 9 | 68.4 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh24-il | 200,000 | 5 | 59.2 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh24-il | 500,000 | 9 | 79.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh24-il | 500,000 | 5 | 61.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh24-il | 1,000,000 | 9 | 74.5 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh24-il | 1,000,000 | 5 | 70.4 at α=7° | 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 | |
| mh42-il | 50,000 | 9 | 32.7 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh42-il | 50,000 | 5 | 35.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh42-il | 100,000 | 9 | 49.9 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh42-il | 100,000 | 5 | 49.6 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh42-il | 200,000 | 9 | 67 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh42-il | 200,000 | 5 | 62.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh42-il | 500,000 | 9 | 88.1 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh42-il | 500,000 | 5 | 78.5 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh42-il | 1,000,000 | 9 | 102 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh42-il | 1,000,000 | 5 | 89.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh83-il | 50,000 | 9 | 12.8 at α=1° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh83-il | 50,000 | 5 | 26.7 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh83-il | 100,000 | 9 | 34.1 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh83-il | 100,000 | 5 | 46.6 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh83-il | 200,000 | 9 | 59.1 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh83-il | 200,000 | 5 | 67.1 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh83-il | 500,000 | 9 | 94.1 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh83-il | 500,000 | 5 | 97.6 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh83-il | 1,000,000 | 9 | 123.8 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh83-il | 1,000,000 | 5 | 123.9 at α=8.5° | 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 | |
| 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 | |
| mh30-il | 50,000 | 9 | 34.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh30-il | 50,000 | 5 | 35.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh30-il | 100,000 | 9 | 51.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh30-il | 100,000 | 5 | 48.5 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh30-il | 200,000 | 9 | 67.1 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh30-il | 200,000 | 5 | 59.8 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh30-il | 500,000 | 9 | 85.1 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh30-il | 500,000 | 5 | 73.8 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh30-il | 1,000,000 | 9 | 95.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh30-il | 1,000,000 | 5 | 84.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh82-il | 50,000 | 9 | 11.1 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh82-il | 50,000 | 5 | 23.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh82-il | 100,000 | 9 | 29.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh82-il | 100,000 | 5 | 42.1 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh82-il | 200,000 | 9 | 53.7 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh82-il | 200,000 | 5 | 61.7 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh82-il | 500,000 | 9 | 87.1 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh82-il | 500,000 | 5 | 90.5 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh82-il | 1,000,000 | 9 | 115.3 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh82-il | 1,000,000 | 5 | 115.2 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh200-il | 50,000 | 9 | 33.7 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh200-il | 50,000 | 5 | 32.3 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh200-il | 100,000 | 9 | 53.4 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh200-il | 100,000 | 5 | 51 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh200-il | 200,000 | 9 | 76.1 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh200-il | 200,000 | 5 | 66.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh200-il | 500,000 | 9 | 98.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh200-il | 500,000 | 5 | 85.7 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh200-il | 1,000,000 | 9 | 117 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh200-il | 1,000,000 | 5 | 93.7 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh60-il | 50,000 | 9 | 27.5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh60-il | 50,000 | 5 | 32.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh60-il | 100,000 | 9 | 45 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh60-il | 100,000 | 5 | 46.6 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh60-il | 200,000 | 9 | 61.4 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh60-il | 200,000 | 5 | 60 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh60-il | 500,000 | 9 | 82.8 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh60-il | 500,000 | 5 | 77.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh60-il | 1,000,000 | 9 | 98.3 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh60-il | 1,000,000 | 5 | 91 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh43-il | 50,000 | 9 | 33.4 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh43-il | 50,000 | 5 | 35.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh43-il | 100,000 | 9 | 50.1 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh43-il | 100,000 | 5 | 49.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh43-il | 200,000 | 9 | 66.7 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh43-il | 200,000 | 5 | 61.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh43-il | 500,000 | 9 | 86.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh43-il | 500,000 | 5 | 76.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh43-il | 1,000,000 | 9 | 100 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh43-il | 1,000,000 | 5 | 85.6 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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