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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(goe593-il) GOE 593 AIRFOIL | Gottingen 593 airfoil Max thickness 11.9% at 30% chord Max camber 4.1% at 40% chord | Remove Airfoil details Airfoil plotter |
(nplx-il) NPL AIRFOIL FROM ARC CP 1372 | NPL transonic airfoil FROM ARC CP 1372 Max thickness 10.7% at 35.8% chord Max camber 1.1% at 73.7% chord | Remove Airfoil details Airfoil plotter |
(m665-il) M6 (65%) | NACA/Munk M6 (65%) Max thickness 7.8% at 30% chord Max camber 1.4% at 30% chord | Remove Airfoil details Airfoil plotter |
(goe795sm-il) GOE 795 smoothed | Gottingen 795 airfoil (smoothed) Max thickness 8% at 30.9% chord Max camber 2.4% at 43.5% chord | Remove Airfoil details Airfoil plotter |
(fx711525-il) FX 71-L-150/25 AIRFOIL | Wortmann FX 71-L-150/25 airfoil Max thickness 15% at 33.9% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(goe501-il) GOE 501 AIRFOIL | Gottingen 501 airfoil Max thickness 12.8% at 30% chord Max camber 6.3% at 50% chord | Remove Airfoil details Airfoil plotter |
(goe324-il) GOE 324 (HANSA-BRANDENBURG) AIRFOIL | Gottingen 324 (Hansa-Brandenburg) airfoil Max thickness 13.1% at 29.8% chord Max camber 5.9% at 29.8% chord | Remove Airfoil details Airfoil plotter |
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Polars for (goe593-il,nplx-il,m665-il,goe795sm-il,fx711525-il,goe501-il,goe324-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe593-il | 50,000 | 9 | 24.3 at α=12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe593-il | 50,000 | 5 | 35.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe593-il | 100,000 | 9 | 52.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe593-il | 100,000 | 5 | 53.2 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe593-il | 200,000 | 9 | 74.6 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe593-il | 200,000 | 5 | 69.9 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe593-il | 500,000 | 9 | 101.4 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe593-il | 500,000 | 5 | 88.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe593-il | 1,000,000 | 9 | 117.1 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe593-il | 1,000,000 | 5 | 107.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nplx-il | 50,000 | 9 | 22 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nplx-il | 50,000 | 5 | 22.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nplx-il | 100,000 | 9 | 28.8 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nplx-il | 100,000 | 5 | 28.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nplx-il | 200,000 | 9 | 41 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nplx-il | 200,000 | 5 | 38.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nplx-il | 500,000 | 9 | 49.1 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nplx-il | 500,000 | 5 | 54.6 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| nplx-il | 1,000,000 | 9 | 62.8 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| nplx-il | 1,000,000 | 5 | 70.6 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m665-il | 50,000 | 9 | 33.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m665-il | 50,000 | 5 | 33.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m665-il | 100,000 | 9 | 47.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m665-il | 100,000 | 5 | 44.8 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m665-il | 200,000 | 9 | 60.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m665-il | 200,000 | 5 | 55.4 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m665-il | 500,000 | 9 | 74.7 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m665-il | 500,000 | 5 | 61.9 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| m665-il | 1,000,000 | 9 | 78.6 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| m665-il | 1,000,000 | 5 | 73.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe795sm-il | 50,000 | 9 | 37.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe795sm-il | 50,000 | 5 | 38 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe795sm-il | 100,000 | 9 | 56.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe795sm-il | 100,000 | 5 | 54.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe795sm-il | 200,000 | 9 | 76.5 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe795sm-il | 200,000 | 5 | 69.7 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe795sm-il | 500,000 | 9 | 101.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe795sm-il | 500,000 | 5 | 86.2 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe795sm-il | 1,000,000 | 9 | 116.2 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe795sm-il | 1,000,000 | 5 | 96.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx711525-il | 50,000 | 9 | 27.4 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx711525-il | 50,000 | 5 | 26.8 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx711525-il | 100,000 | 9 | 38.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx711525-il | 100,000 | 5 | 34.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx711525-il | 200,000 | 9 | 46.1 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx711525-il | 200,000 | 5 | 39.1 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx711525-il | 500,000 | 9 | 50.5 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx711525-il | 500,000 | 5 | 48.3 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx711525-il | 1,000,000 | 9 | 58.2 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx711525-il | 1,000,000 | 5 | 57.4 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe501-il | 50,000 | 9 | 9.4 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe501-il | 50,000 | 5 | 29.7 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe501-il | 100,000 | 9 | 56.5 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe501-il | 100,000 | 5 | 60.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe501-il | 200,000 | 9 | 85.4 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe501-il | 200,000 | 5 | 80.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe501-il | 500,000 | 9 | 113.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe501-il | 500,000 | 5 | 106.2 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe501-il | 1,000,000 | 9 | 137.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe501-il | 1,000,000 | 5 | 113.9 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe324-il | 50,000 | 9 | 8.3 at α=-3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe324-il | 50,000 | 5 | 20 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe324-il | 100,000 | 9 | 33.6 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe324-il | 100,000 | 5 | 49.6 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe324-il | 200,000 | 9 | 70.6 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe324-il | 200,000 | 5 | 74.2 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe324-il | 500,000 | 9 | 108.8 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe324-il | 500,000 | 5 | 104.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe324-il | 1,000,000 | 9 | 136.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe324-il | 1,000,000 | 5 | 124 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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