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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(n0012-il) NACA 0012 AIRFOILS | NACA 0012 airfoil Max thickness 12% at 30% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(marske7-il) RONCZ LOW DRAG FLYING WING AIRFOIL | Roncz/Marske-7 low drag flying wing airfoil Max thickness 12.1% at 42.8% chord Max camber 2.8% at 39.1% chord | Remove Airfoil details Airfoil plotter |
(mue139-il) MUE 139 | MUE 139 airfoil Max thickness 13.9% at 22.2% chord Max camber 4.7% at 30.9% chord | Remove Airfoil details Airfoil plotter |
(marske2-il) MARSKE PIONEER IA AIRFOIL (NACA 23112/43012A HYBRID) | Marske Pioneer IA airfoil (NACA 23112/43012A hybrid) Max thickness 12.1% at 25% chord Max camber 2.7% at 15% chord | Remove Airfoil details Airfoil plotter |
(ma409sm-il) MA409 (smoothed) | Michael Achterberg MA409 F1C class free flight airfoil (smoothed) Max thickness 6.7% at 23.8% chord Max camber 3.3% at 49.3% chord | Remove Airfoil details Airfoil plotter |
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Polars for (n0012-il,marske7-il,mue139-il,marske2-il,ma409sm-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| n0012-il | 50,000 | 9 | 25.7 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n0012-il | 50,000 | 5 | 26.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n0012-il | 100,000 | 9 | 36.7 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n0012-il | 100,000 | 5 | 36.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n0012-il | 200,000 | 9 | 47.4 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n0012-il | 200,000 | 5 | 45.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n0012-il | 500,000 | 9 | 61.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n0012-il | 500,000 | 5 | 61.7 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n0012-il | 1,000,000 | 9 | 75.6 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n0012-il | 1,000,000 | 5 | 75.4 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske7-il | 50,000 | 9 | 27.4 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske7-il | 50,000 | 5 | 24 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske7-il | 100,000 | 9 | 43.2 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske7-il | 100,000 | 5 | 43.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske7-il | 200,000 | 9 | 72 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske7-il | 200,000 | 5 | 67.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske7-il | 500,000 | 9 | 103.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske7-il | 500,000 | 5 | 90.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske7-il | 1,000,000 | 9 | 120.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske7-il | 1,000,000 | 5 | 96.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mue139-il | 50,000 | 9 | 15.7 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mue139-il | 50,000 | 5 | 27.3 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mue139-il | 100,000 | 9 | 35.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mue139-il | 100,000 | 5 | 44.9 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mue139-il | 200,000 | 9 | 58.3 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mue139-il | 200,000 | 5 | 63.5 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mue139-il | 500,000 | 9 | 89.2 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mue139-il | 500,000 | 5 | 90.9 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mue139-il | 1,000,000 | 9 | 116.5 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mue139-il | 1,000,000 | 5 | 115.3 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske2-il | 50,000 | 9 | 18.9 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske2-il | 50,000 | 5 | 24 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske2-il | 100,000 | 9 | 28.8 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske2-il | 100,000 | 5 | 35.7 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske2-il | 200,000 | 9 | 43 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske2-il | 200,000 | 5 | 51.5 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske2-il | 500,000 | 9 | 72.4 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske2-il | 500,000 | 5 | 77.5 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| marske2-il | 1,000,000 | 9 | 99 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| marske2-il | 1,000,000 | 5 | 97 at α=10.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ma409sm-il | 50,000 | 9 | 43.5 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ma409sm-il | 50,000 | 5 | 43.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ma409sm-il | 100,000 | 9 | 64.2 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ma409sm-il | 100,000 | 5 | 62.4 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ma409sm-il | 200,000 | 9 | 88.6 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ma409sm-il | 200,000 | 5 | 81.2 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ma409sm-il | 500,000 | 9 | 121.6 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ma409sm-il | 500,000 | 5 | 100.9 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ma409sm-il | 1,000,000 | 9 | 140.9 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ma409sm-il | 1,000,000 | 5 | 112.2 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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