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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(mrc-16-il) MRC-16 | Drela MRC-16 Max thickness 13.9% at 34.6% chord Max camber 3% at 40.3% chord | Remove Airfoil details Airfoil plotter |
(mh70-il) MH 70 11.08% | Martin Hepperle MH 70 for fying wing (full size) Max thickness 11.1% at 29.4% chord Max camber 3% at 39.6% chord | Remove Airfoil details Airfoil plotter |
(griffith30symsuction-il) Griffith 30% Suction Airfoil | Griffith 30% suction airfoil Max thickness 30.6% at 49.3% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(mh33-il) MH33 | Martin Hepperle MH 33 for F3E and F3B Max thickness 7.3% at 29.3% chord Max camber 1.1% at 43.9% chord | Remove Airfoil details Airfoil plotter |
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Polars for (mrc-16-il,mh70-il,griffith30symsuction-il,mh33-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mrc-16-il | 50,000 | 9 | 23.1 at α=12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mrc-16-il | 50,000 | 5 | 31.2 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mrc-16-il | 100,000 | 9 | 50.5 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mrc-16-il | 100,000 | 5 | 52.5 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mrc-16-il | 200,000 | 9 | 73.1 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mrc-16-il | 200,000 | 5 | 71.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mrc-16-il | 500,000 | 9 | 102.1 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mrc-16-il | 500,000 | 5 | 94.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mrc-16-il | 1,000,000 | 9 | 124.1 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mrc-16-il | 1,000,000 | 5 | 110.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh70-il | 50,000 | 9 | 27.4 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh70-il | 50,000 | 5 | 35.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh70-il | 100,000 | 9 | 50.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh70-il | 100,000 | 5 | 52.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh70-il | 200,000 | 9 | 70.3 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh70-il | 200,000 | 5 | 67.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh70-il | 500,000 | 9 | 95 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh70-il | 500,000 | 5 | 87.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh70-il | 1,000,000 | 9 | 112.4 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh70-il | 1,000,000 | 5 | 103.8 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| griffith30symsuction-il | 50,000 | 9 | 4.7 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| griffith30symsuction-il | 50,000 | 5 | 10.8 at α=14.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| griffith30symsuction-il | 100,000 | 9 | 17.2 at α=14° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| griffith30symsuction-il | 100,000 | 5 | 11 at α=15.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| griffith30symsuction-il | 200,000 | 9 | 13.5 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| griffith30symsuction-il | 200,000 | 5 | 10.7 at α=15.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| griffith30symsuction-il | 500,000 | 9 | 15 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| griffith30symsuction-il | 500,000 | 5 | 12.5 at α=14.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| griffith30symsuction-il | 1,000,000 | 9 | 17.3 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| griffith30symsuction-il | 1,000,000 | 5 | 15.3 at α=13.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh33-il | 50,000 | 9 | 32.3 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh33-il | 50,000 | 5 | 31.9 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh33-il | 100,000 | 9 | 46.1 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh33-il | 100,000 | 5 | 42.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh33-il | 200,000 | 9 | 59.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh33-il | 200,000 | 5 | 51.2 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh33-il | 500,000 | 9 | 72.9 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh33-il | 500,000 | 5 | 64.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh33-il | 1,000,000 | 9 | 81.2 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh33-il | 1,000,000 | 5 | 74.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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