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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(mh110-il) MH 110 10.01% | Martin Hepperle MH 110 for stall controlled wind turbines (tip) Max thickness 10% at 23.9% chord Max camber 1% at 15.8% chord | Remove Airfoil details Airfoil plotter |
(goe571-il) GOE 571 AIRFOIL | Gottingen 571 airfoil Max thickness 24.9% at 29.4% chord Max camber 9.8% at 29.4% chord | Remove Airfoil details Airfoil plotter |
(goe798-il) GOE 798 AIRFOIL | Gottingen 798 airfoil Max thickness 20% at 30% chord Max camber 6% at 40% chord | Remove Airfoil details Airfoil plotter |
(l1003-il) LIEBECK L1003 AIRFOIL | Liebeck high lift airfoil Max thickness 17.7% at 30% chord Max camber 6.5% at 30% 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 |
(goe462-il) GOE 462 AIRFOIL | Gottingen 462 airfoil Max thickness 11% at 9.9% chord Max camber 13.4% at 29.9% chord | Remove Airfoil details Airfoil plotter |
(goe450-il) GOE 450 AIRFOIL | Gottingen 450 airfoil Max thickness 8.9% at 29.9% chord Max camber 5.2% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(naca633018-il) NACA 63(3)-018 | NACA 63(3)-018 airfoil Max thickness 18% at 33.9% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(wb140-il) WB-140/35/FB 14% | Woody Blanchard WB140/35/FB R/C sailplane airfoil Max thickness 13.9% at 30% chord Max camber 3.7% at 45% chord | Remove Airfoil details Airfoil plotter |
(mh121-il) MH 121 8.76% | Martin Hepperle MH 121 for tip section of a propeller Max thickness 8.8% at 37.9% chord Max camber 3% at 62.2% chord | Remove Airfoil details Airfoil plotter |
(naca641112-il) NACA 64(1)-112 | NACA 64(1)-112 airfoil Max thickness 12% at 40% chord Max camber 0.6% at 50% chord | Remove Airfoil details Airfoil plotter |
(goe685-il) GOE 685 AIRFOIL | Gottingen 685 airfoil Max thickness 13.1% at 19.6% chord Max camber 4.2% at 49.5% chord | Remove Airfoil details Airfoil plotter |
(goe507-il) GOE 507 AIRFOIL | Gottingen 507 airfoil Max thickness 8.7% at 30% chord Max camber 2.9% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe443-il) GOE 443 AIRFOIL | Gottingen 443 airfoil Max thickness 5% at 30% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(goe285-il) GOE 285 AIRFOIL | Gottingen 285 airfoil Max thickness 11.7% at 30% chord Max camber 3.7% at 30% chord | Remove Airfoil details Airfoil plotter |
(goe364-il) GOE 364 AIRFOIL | Gottingen 364 airfoil Max thickness 10.8% at 30% chord Max camber 6.5% at 30% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (mh110-il,goe571-il,goe798-il,l1003-il,mh43-il,goe462-il,goe450-il,naca633018-il,wb140-il,mh121-il,naca641112-il,goe685-il,goe507-il,goe443-il,goe285-il,goe364-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| mh110-il | 50,000 | 9 | 16.5 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh110-il | 50,000 | 5 | 25.2 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh110-il | 100,000 | 9 | 39 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh110-il | 100,000 | 5 | 41 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh110-il | 200,000 | 9 | 56.3 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh110-il | 200,000 | 5 | 56 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh110-il | 500,000 | 9 | 78.5 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh110-il | 500,000 | 5 | 75.9 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh110-il | 1,000,000 | 9 | 94.8 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh110-il | 1,000,000 | 5 | 88.9 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe571-il | 50,000 | 9 | 3.7 at α=-12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe571-il | 50,000 | 5 | 5.7 at α=-7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe571-il | 100,000 | 9 | 8.1 at α=-8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe571-il | 100,000 | 5 | 8.6 at α=0.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe571-il | 200,000 | 9 | 33.1 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe571-il | 200,000 | 5 | 34 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe571-il | 500,000 | 9 | 56.1 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe571-il | 500,000 | 5 | 42.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe571-il | 1,000,000 | 9 | 62.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe571-il | 1,000,000 | 5 | 52.5 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe798-il | 50,000 | 9 | 3.8 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe798-il | 50,000 | 5 | 10.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe798-il | 100,000 | 9 | 20.6 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe798-il | 100,000 | 5 | 31.9 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe798-il | 200,000 | 9 | 65.7 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe798-il | 200,000 | 5 | 61.7 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe798-il | 500,000 | 9 | 98.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe798-il | 500,000 | 5 | 83.8 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe798-il | 1,000,000 | 9 | 120 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe798-il | 1,000,000 | 5 | 84.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| l1003-il | 50,000 | 9 | 4.1 at α=14.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| l1003-il | 50,000 | 5 | 5.2 at α=17.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| l1003-il | 100,000 | 9 | 4.5 at α=14.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| l1003-il | 100,000 | 5 | 7 at α=17.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| l1003-il | 200,000 | 9 | 10.2 at α=18.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| l1003-il | 200,000 | 5 | 10.1 at α=15.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| l1003-il | 500,000 | 9 | 74.1 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| l1003-il | 500,000 | 5 | 68.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| l1003-il | 1,000,000 | 9 | 104.1 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| l1003-il | 1,000,000 | 5 | 68.8 at α=4° | 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 | |
| goe462-il | 50,000 | 9 | 8.9 at α=-0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe462-il | 50,000 | 5 | 29.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe462-il | 100,000 | 9 | 52.3 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe462-il | 100,000 | 5 | 46.4 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe462-il | 200,000 | 9 | 61.2 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe462-il | 200,000 | 5 | 62.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe462-il | 500,000 | 9 | 175.7 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe462-il | 500,000 | 5 | 88.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe462-il | 1,000,000 | 9 | 107.3 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe462-il | 1,000,000 | 5 | 111.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe450-il | 50,000 | 9 | 39.6 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe450-il | 50,000 | 5 | 40.1 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe450-il | 100,000 | 9 | 63.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe450-il | 100,000 | 5 | 64.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe450-il | 200,000 | 9 | 88.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe450-il | 200,000 | 5 | 85.6 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe450-il | 500,000 | 9 | 120.7 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe450-il | 500,000 | 5 | 108 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe450-il | 1,000,000 | 9 | 141.4 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe450-il | 1,000,000 | 5 | 118.9 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca633018-il | 50,000 | 9 | 23.4 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca633018-il | 50,000 | 5 | 20.6 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca633018-il | 100,000 | 9 | 40.7 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca633018-il | 100,000 | 5 | 36.4 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca633018-il | 200,000 | 9 | 53.3 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca633018-il | 200,000 | 5 | 50.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca633018-il | 500,000 | 9 | 73 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca633018-il | 500,000 | 5 | 61.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca633018-il | 1,000,000 | 9 | 83 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca633018-il | 1,000,000 | 5 | 65.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb140-il | 50,000 | 9 | 9.9 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb140-il | 50,000 | 5 | 31.9 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb140-il | 100,000 | 9 | 53.4 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb140-il | 100,000 | 5 | 52.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb140-il | 200,000 | 9 | 83.9 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb140-il | 200,000 | 5 | 62.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb140-il | 500,000 | 9 | 105.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb140-il | 500,000 | 5 | 64 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| wb140-il | 1,000,000 | 9 | 109.3 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| wb140-il | 1,000,000 | 5 | 74.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh121-il | 50,000 | 9 | 31.9 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh121-il | 50,000 | 5 | 35.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh121-il | 100,000 | 9 | 53.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh121-il | 100,000 | 5 | 57.9 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh121-il | 200,000 | 9 | 84 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh121-il | 200,000 | 5 | 82.4 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh121-il | 500,000 | 9 | 125.8 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh121-il | 500,000 | 5 | 107.8 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh121-il | 1,000,000 | 9 | 139.1 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh121-il | 1,000,000 | 5 | 117.7 at α=1.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca641112-il | 50,000 | 9 | 29.7 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca641112-il | 50,000 | 5 | 29.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca641112-il | 100,000 | 9 | 44.1 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca641112-il | 100,000 | 5 | 40 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca641112-il | 200,000 | 9 | 54.4 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca641112-il | 200,000 | 5 | 47.8 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca641112-il | 500,000 | 9 | 68.3 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca641112-il | 500,000 | 5 | 56 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca641112-il | 1,000,000 | 9 | 76.6 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca641112-il | 1,000,000 | 5 | 69.6 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe685-il | 50,000 | 9 | 25.3 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe685-il | 50,000 | 5 | 33.9 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe685-il | 100,000 | 9 | 52.5 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe685-il | 100,000 | 5 | 54.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe685-il | 200,000 | 9 | 73.4 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe685-il | 200,000 | 5 | 71.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe685-il | 500,000 | 9 | 100.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe685-il | 500,000 | 5 | 87.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe685-il | 1,000,000 | 9 | 119.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe685-il | 1,000,000 | 5 | 96.3 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe507-il | 50,000 | 9 | 37.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe507-il | 50,000 | 5 | 38 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe507-il | 100,000 | 9 | 55.4 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe507-il | 100,000 | 5 | 53.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe507-il | 200,000 | 9 | 73.8 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe507-il | 200,000 | 5 | 67.4 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe507-il | 500,000 | 9 | 95.1 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe507-il | 500,000 | 5 | 82 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe507-il | 1,000,000 | 9 | 106.1 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe507-il | 1,000,000 | 5 | 89.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe443-il | 50,000 | 9 | 16.1 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe443-il | 50,000 | 5 | 16 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe443-il | 100,000 | 9 | 20.3 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe443-il | 100,000 | 5 | 26.2 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe443-il | 200,000 | 9 | 34 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe443-il | 200,000 | 5 | 32.2 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe443-il | 500,000 | 9 | 44.5 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe443-il | 500,000 | 5 | 32 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe443-il | 1,000,000 | 9 | 43.3 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe443-il | 1,000,000 | 5 | 60.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe285-il | 50,000 | 9 | 26.1 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe285-il | 50,000 | 5 | 34.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe285-il | 100,000 | 9 | 47.2 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe285-il | 100,000 | 5 | 50.1 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe285-il | 200,000 | 9 | 65.2 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe285-il | 200,000 | 5 | 65.2 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe285-il | 500,000 | 9 | 89.3 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe285-il | 500,000 | 5 | 87 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe285-il | 1,000,000 | 9 | 109.1 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe285-il | 1,000,000 | 5 | 103.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe364-il | 50,000 | 9 | 13.5 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe364-il | 50,000 | 5 | 34.8 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe364-il | 100,000 | 9 | 52.5 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe364-il | 100,000 | 5 | 57 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe364-il | 200,000 | 9 | 76.4 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe364-il | 200,000 | 5 | 76.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe364-il | 500,000 | 9 | 107.8 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe364-il | 500,000 | 5 | 104 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe364-il | 1,000,000 | 9 | 133.4 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe364-il | 1,000,000 | 5 | 124.5 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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