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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(goe275-il) GOE 275 (DAIMLER VI) AIRFOIL | Gottingen 275 (DAIMLER VI) airfoil Max thickness 7.7% at 19.9% chord Max camber 4.7% at 29.9% chord | Remove Airfoil details Airfoil plotter |
(goe269-il) GOE 269 AIRFOIL | Gottingen 269 airfoil Max thickness 6.6% at 29.9% chord Max camber 5% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(goe243-il) GOE 243 (MVA PR.3) AIRFOIL | Gottingen 243 (MVA PR.3) airfoil Max thickness 19% at 29.3% chord Max camber 8.4% at 59.4% chord | Remove Airfoil details Airfoil plotter |
(goe411-il) GOE 411 AIRFOIL | Gottingen 411 airfoil Max thickness 13.2% at 30% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(goe460-il) GOE 460 AIRFOIL | Gottingen 460 airfoil Max thickness 20.5% at 30% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(goe533-il) GOE 533 AIRFOIL | Gottingen 533 airfoil Max thickness 13.7% at 30% chord Max camber 4.7% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe769-il) GOE 769 AIRFOIL | Gottingen 769 airfoil Max thickness 13.8% at 20% chord Max camber 4.8% at 30% chord | Remove Airfoil details Airfoil plotter |
(goe758-il) GOE 758 AIRFOIL | Gottingen 758 airfoil Max thickness 13.9% at 30% chord Max camber 4.7% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe180-il) GOE 180 (MVA H.26) AIRFOIL | Gottingen 180 (MVA H.26) airfoil Max thickness 8.7% at 30% chord Max camber 4.4% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe234-il) GOE 234 (MVA CA5) AIRFOIL | Gottingen 234 (MVA CA5) airfoil Max thickness 14.2% at 19.7% chord Max camber 9.2% at 49.7% chord | Remove Airfoil details Airfoil plotter |
(goe167-il) GOE 167 (V.KARMAN PROP.2) AIRFOIL | Gottingen 167 (V.Karman PROP.2) airfoil Max thickness 10.1% at 29.9% chord Max camber 4.5% at 29.9% chord | Remove Airfoil details Airfoil plotter |
(goe361-il) GOE 361 AIRFOIL | Gottingen 361 airfoil Max thickness 6.8% at 20% chord Max camber 5.5% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe274-il) GOE 274 (DAIMLER V) AIRFOIL | Gottingen 274 (DAIMLER V) airfoil Max thickness 8.7% at 29.9% chord Max camber 4.8% at 29.9% chord | Remove Airfoil details Airfoil plotter |
(goe775-il) GOE 775 AIRFOIL | Gottingen 775 airfoil Max thickness 21% at 30% chord Max camber 0% at 1.3% chord | Remove Airfoil details Airfoil plotter |
(goe235-il) GOE 235 (SCHTTE-LANZ) AIRFOIL | Gottingen 235 (SCHATTE-LANZ) airfoil Max thickness 6.5% at 19.9% chord Max camber 3.5% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(goe490-il) GOE 490 AIRFOIL | Gottingen 490 airfoil Max thickness 8.8% at 19.9% chord Max camber 3.8% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(goe147-il) GOE 147 (MVA H.6) AIRFOIL | Gottingen 147 (MVA H.6) airfoil Max thickness 7.5% at 14.9% chord Max camber 3.8% at 29.9% chord | Remove Airfoil details Airfoil plotter |
(goe766-il) GOE 766 AIRFOIL | Gottingen 766 airfoil Max thickness 12% at 25% chord Max camber 1.5% at 20% chord | Remove Airfoil details Airfoil plotter |
(goe601-il) GOE 601 AIRFOIL | Gottingen 601 airfoil Max thickness 16% at 39% chord Max camber 2.5% at 49% chord | Remove Airfoil details Airfoil plotter |
(goe360-il) GOE 360 AIRFOIL | Gottingen 360 airfoil Max thickness 9.7% at 29.9% chord Max camber 5.9% at 29.9% chord | Remove Airfoil details Airfoil plotter |
(goe336-il) GOE 336 (MVA H.44) AIRFOIL | Gottingen 336 (MVA H.44) airfoil Max thickness 9% at 29.9% chord Max camber 5.4% at 29.9% chord | Remove Airfoil details Airfoil plotter |
(goe723-il) GOE 723 AIRFOIL | Gottingen 723 airfoil Max thickness 11.6% at 29.7% chord Max camber 4.5% at 49.7% chord | Remove Airfoil details Airfoil plotter |
(goe765-il) Gottingen 765 airfoil (recovered). Thick: .144 LE radius: 0.02062 LE slope: 0.17300 | Used on the Me163 Komet Max thickness 14.4% at 30% chord Max camber 1.9% at 25.9% chord | Remove Airfoil details Airfoil plotter |
(goe477-il) GOE 477 AIRFOIL | Gottingen 477 airfoil Max thickness 10.1% at 30% chord Max camber 4.9% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe144-il) GOE 144 (MVA H.21) AIRFOIL | Gottingen 144 (MVA H.21) airfoil Max thickness 7.3% at 19.9% chord Max camber 4.7% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(goe599-il) GOE 599 AIRFOIL | Gottingen 599 airfoil Max thickness 10% at 29.6% chord Max camber 1.5% at 59.7% chord | Remove Airfoil details Airfoil plotter |
(goe402-il) GOE 402 AIRFOIL | Gottingen 402 airfoil Max thickness 6.8% at 20% chord Max camber 5.7% at 30% chord | Remove Airfoil details Airfoil plotter |
(goe226-il) GOE 226 (MVA H.36) AIRFOIL | Gottingen 226 (MVA H.36) airfoil Max thickness 13.9% at 19.7% chord Max camber 8.1% at 49.7% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (goe275-il,goe269-il,goe243-il,goe411-il,goe460-il,goe533-il,goe769-il,goe758-il,goe180-il,goe234-il,goe167-il,goe361-il,goe274-il,goe775-il,goe235-il,goe490-il,goe147-il,goe766-il,goe601-il,goe360-il,goe336-il,goe723-il,goe765-il,goe477-il,goe144-il,goe599-il,goe402-il,goe226-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe275-il | 50,000 | 9 | 34.4 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe275-il | 50,000 | 5 | 40.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe275-il | 100,000 | 9 | 53.1 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe275-il | 100,000 | 5 | 55.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe275-il | 200,000 | 9 | 72 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe275-il | 200,000 | 5 | 73.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe275-il | 500,000 | 9 | 99.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe275-il | 500,000 | 5 | 94.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe275-il | 1,000,000 | 9 | 118.1 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe275-il | 1,000,000 | 5 | 106.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe269-il | 50,000 | 9 | 36.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe269-il | 50,000 | 5 | 43.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe269-il | 100,000 | 9 | 59.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe269-il | 100,000 | 5 | 61.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe269-il | 200,000 | 9 | 80.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe269-il | 200,000 | 5 | 79.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe269-il | 500,000 | 9 | 107.7 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe269-il | 500,000 | 5 | 102.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe269-il | 1,000,000 | 9 | 127.9 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe269-il | 1,000,000 | 5 | 115.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe243-il | 50,000 | 9 | 5.7 at α=-0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe243-il | 50,000 | 5 | 17.9 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe243-il | 100,000 | 9 | 44.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe243-il | 100,000 | 5 | 49.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe243-il | 200,000 | 9 | 70.4 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe243-il | 200,000 | 5 | 69.4 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe243-il | 500,000 | 9 | 99.1 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe243-il | 500,000 | 5 | 90.3 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe243-il | 1,000,000 | 9 | 119.1 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe243-il | 1,000,000 | 5 | 107.9 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe411-il | 50,000 | 9 | 30.1 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe411-il | 50,000 | 5 | 28 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe411-il | 100,000 | 9 | 40.7 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe411-il | 100,000 | 5 | 34.1 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe411-il | 200,000 | 9 | 43.7 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe411-il | 200,000 | 5 | 35.6 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe411-il | 500,000 | 9 | 45.8 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe411-il | 500,000 | 5 | 42.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe411-il | 1,000,000 | 9 | 48.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe411-il | 1,000,000 | 5 | 53.4 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe460-il | 50,000 | 9 | 20.8 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe460-il | 50,000 | 5 | 25.8 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe460-il | 100,000 | 9 | 39.8 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe460-il | 100,000 | 5 | 34.1 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe460-il | 200,000 | 9 | 46.4 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe460-il | 200,000 | 5 | 39.4 at α=10.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe460-il | 500,000 | 9 | 54.4 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe460-il | 500,000 | 5 | 50.6 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe460-il | 1,000,000 | 9 | 66.6 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe460-il | 1,000,000 | 5 | 57.5 at α=10.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe533-il | 50,000 | 9 | 10.5 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe533-il | 50,000 | 5 | 29.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe533-il | 100,000 | 9 | 46.5 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe533-il | 100,000 | 5 | 54.8 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe533-il | 200,000 | 9 | 73.8 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe533-il | 200,000 | 5 | 75.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe533-il | 500,000 | 9 | 106.3 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe533-il | 500,000 | 5 | 102.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe533-il | 1,000,000 | 9 | 131.1 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe533-il | 1,000,000 | 5 | 121.7 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe769-il | 50,000 | 9 | 16.6 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe769-il | 50,000 | 5 | 28.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe769-il | 100,000 | 9 | 39.1 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe769-il | 100,000 | 5 | 45.3 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe769-il | 200,000 | 9 | 59.1 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe769-il | 200,000 | 5 | 61.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe769-il | 500,000 | 9 | 85.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe769-il | 500,000 | 5 | 85.2 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe769-il | 1,000,000 | 9 | 107.9 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe769-il | 1,000,000 | 5 | 106 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe758-il | 50,000 | 9 | 7.6 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe758-il | 50,000 | 5 | 25.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe758-il | 100,000 | 9 | 45.4 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe758-il | 100,000 | 5 | 52.7 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe758-il | 200,000 | 9 | 73.7 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe758-il | 200,000 | 5 | 75.6 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe758-il | 500,000 | 9 | 108.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe758-il | 500,000 | 5 | 102.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe758-il | 1,000,000 | 9 | 133.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe758-il | 1,000,000 | 5 | 123.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe180-il | 50,000 | 9 | 33.2 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe180-il | 50,000 | 5 | 40.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe180-il | 100,000 | 9 | 55.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe180-il | 100,000 | 5 | 59.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe180-il | 200,000 | 9 | 78.2 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe180-il | 200,000 | 5 | 77.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe180-il | 500,000 | 9 | 107.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe180-il | 500,000 | 5 | 99.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe180-il | 1,000,000 | 9 | 126.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe180-il | 1,000,000 | 5 | 112 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe234-il | 50,000 | 9 | 10.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe234-il | 50,000 | 5 | 27.7 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe234-il | 100,000 | 9 | 54.7 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe234-il | 100,000 | 5 | 56.6 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe234-il | 200,000 | 9 | 77 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe234-il | 200,000 | 5 | 79.4 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe234-il | 500,000 | 9 | 110.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe234-il | 500,000 | 5 | 108.4 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe234-il | 1,000,000 | 9 | 137.7 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe234-il | 1,000,000 | 5 | 127.1 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe167-il | 50,000 | 9 | 26.6 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe167-il | 50,000 | 5 | 34 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe167-il | 100,000 | 9 | 58 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe167-il | 100,000 | 5 | 58.8 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe167-il | 200,000 | 9 | 80.8 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe167-il | 200,000 | 5 | 78.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe167-il | 500,000 | 9 | 106.9 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe167-il | 500,000 | 5 | 97.9 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe167-il | 1,000,000 | 9 | 124.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe167-il | 1,000,000 | 5 | 108.6 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe361-il | 50,000 | 9 | 39.3 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe361-il | 50,000 | 5 | 42.4 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe361-il | 100,000 | 9 | 57.8 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe361-il | 100,000 | 5 | 59.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe361-il | 200,000 | 9 | 76.6 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe361-il | 200,000 | 5 | 77.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe361-il | 500,000 | 9 | 103.8 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe361-il | 500,000 | 5 | 101.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe361-il | 1,000,000 | 9 | 123.4 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe361-il | 1,000,000 | 5 | 119.5 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe274-il | 50,000 | 9 | 37.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe274-il | 50,000 | 5 | 40.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe274-il | 100,000 | 9 | 55.8 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe274-il | 100,000 | 5 | 57 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe274-il | 200,000 | 9 | 73.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe274-il | 200,000 | 5 | 73.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe274-il | 500,000 | 9 | 99 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe274-il | 500,000 | 5 | 92.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe274-il | 1,000,000 | 9 | 115.1 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe274-il | 1,000,000 | 5 | 105.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe775-il | 50,000 | 9 | 18.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe775-il | 50,000 | 5 | 25.1 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe775-il | 100,000 | 9 | 36.9 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe775-il | 100,000 | 5 | 35.8 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe775-il | 200,000 | 9 | 48.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe775-il | 200,000 | 5 | 43.4 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe775-il | 500,000 | 9 | 60.3 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe775-il | 500,000 | 5 | 56.6 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe775-il | 1,000,000 | 9 | 74.6 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe775-il | 1,000,000 | 5 | 69.8 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe235-il | 50,000 | 9 | 36.9 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe235-il | 50,000 | 5 | 37.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe235-il | 100,000 | 9 | 52.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe235-il | 100,000 | 5 | 48 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe235-il | 200,000 | 9 | 60.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe235-il | 200,000 | 5 | 57.6 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe235-il | 500,000 | 9 | 73.9 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe235-il | 500,000 | 5 | 68.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe235-il | 1,000,000 | 9 | 80.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe235-il | 1,000,000 | 5 | 81.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe490-il | 50,000 | 9 | 33.2 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe490-il | 50,000 | 5 | 38.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe490-il | 100,000 | 9 | 54.3 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe490-il | 100,000 | 5 | 54.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe490-il | 200,000 | 9 | 72.5 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe490-il | 200,000 | 5 | 70.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe490-il | 500,000 | 9 | 96.2 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe490-il | 500,000 | 5 | 89.6 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe490-il | 1,000,000 | 9 | 114.1 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe490-il | 1,000,000 | 5 | 98.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe147-il | 50,000 | 9 | 29.2 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe147-il | 50,000 | 5 | 36.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe147-il | 100,000 | 9 | 48.6 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe147-il | 100,000 | 5 | 49.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe147-il | 200,000 | 9 | 64.3 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe147-il | 200,000 | 5 | 66.1 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe147-il | 500,000 | 9 | 86.8 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe147-il | 500,000 | 5 | 86.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe147-il | 1,000,000 | 9 | 102.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe147-il | 1,000,000 | 5 | 101.4 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe766-il | 50,000 | 9 | 19.2 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe766-il | 50,000 | 5 | 27.4 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe766-il | 100,000 | 9 | 37.6 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe766-il | 100,000 | 5 | 42 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe766-il | 200,000 | 9 | 55.9 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe766-il | 200,000 | 5 | 57.2 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe766-il | 500,000 | 9 | 80.3 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe766-il | 500,000 | 5 | 77 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe766-il | 1,000,000 | 9 | 98 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe766-il | 1,000,000 | 5 | 87.2 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe601-il | 50,000 | 9 | 25.2 at α=11.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe601-il | 50,000 | 5 | 28 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe601-il | 100,000 | 9 | 47.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe601-il | 100,000 | 5 | 44.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe601-il | 200,000 | 9 | 69.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe601-il | 200,000 | 5 | 57.4 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe601-il | 500,000 | 9 | 82.8 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe601-il | 500,000 | 5 | 69 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe601-il | 1,000,000 | 9 | 91.2 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe601-il | 1,000,000 | 5 | 82.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe360-il | 50,000 | 9 | 20.7 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe360-il | 50,000 | 5 | 36.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe360-il | 100,000 | 9 | 51.4 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe360-il | 100,000 | 5 | 56.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe360-il | 200,000 | 9 | 73.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe360-il | 200,000 | 5 | 76.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe360-il | 500,000 | 9 | 105.3 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe360-il | 500,000 | 5 | 104.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe360-il | 1,000,000 | 9 | 131.2 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe360-il | 1,000,000 | 5 | 127.3 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe336-il | 50,000 | 9 | 30.6 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe336-il | 50,000 | 5 | 34.2 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe336-il | 100,000 | 9 | 56.7 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe336-il | 100,000 | 5 | 57.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe336-il | 200,000 | 9 | 79.5 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe336-il | 200,000 | 5 | 77.3 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe336-il | 500,000 | 9 | 107.1 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe336-il | 500,000 | 5 | 97.9 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe336-il | 1,000,000 | 9 | 125.8 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe336-il | 1,000,000 | 5 | 94.9 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe723-il | 50,000 | 9 | 32 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe723-il | 50,000 | 5 | 33.4 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe723-il | 100,000 | 9 | 58.4 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe723-il | 100,000 | 5 | 58.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe723-il | 200,000 | 9 | 82.2 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe723-il | 200,000 | 5 | 79.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe723-il | 500,000 | 9 | 114 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe723-il | 500,000 | 5 | 103.5 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe723-il | 1,000,000 | 9 | 136.6 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe723-il | 1,000,000 | 5 | 112 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe765-il | 50,000 | 9 | 15.1 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe765-il | 50,000 | 5 | 28.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe765-il | 100,000 | 9 | 41.5 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe765-il | 100,000 | 5 | 44.6 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe765-il | 200,000 | 9 | 59.4 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe765-il | 200,000 | 5 | 58.6 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe765-il | 500,000 | 9 | 80.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe765-il | 500,000 | 5 | 68.5 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe765-il | 1,000,000 | 9 | 85.9 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe765-il | 1,000,000 | 5 | 79.6 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe477-il | 50,000 | 9 | 34.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe477-il | 50,000 | 5 | 36.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe477-il | 100,000 | 9 | 56.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe477-il | 100,000 | 5 | 54.7 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe477-il | 200,000 | 9 | 80.5 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe477-il | 200,000 | 5 | 75 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe477-il | 500,000 | 9 | 111.3 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe477-il | 500,000 | 5 | 87.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe477-il | 1,000,000 | 9 | 121.7 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe477-il | 1,000,000 | 5 | 104.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe144-il | 50,000 | 9 | 38.6 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe144-il | 50,000 | 5 | 41.6 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe144-il | 100,000 | 9 | 59 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe144-il | 100,000 | 5 | 60.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe144-il | 200,000 | 9 | 79.3 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe144-il | 200,000 | 5 | 78 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe144-il | 500,000 | 9 | 106.1 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe144-il | 500,000 | 5 | 98.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe144-il | 1,000,000 | 9 | 125.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe144-il | 1,000,000 | 5 | 95.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe599-il | 50,000 | 9 | 34.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe599-il | 50,000 | 5 | 33.1 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe599-il | 100,000 | 9 | 48.5 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe599-il | 100,000 | 5 | 44.1 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe599-il | 200,000 | 9 | 61.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe599-il | 200,000 | 5 | 51.2 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe599-il | 500,000 | 9 | 72.8 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe599-il | 500,000 | 5 | 65.5 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe599-il | 1,000,000 | 9 | 79.8 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe599-il | 1,000,000 | 5 | 80.2 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe402-il | 50,000 | 9 | 31.5 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe402-il | 50,000 | 5 | 40.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe402-il | 100,000 | 9 | 55.1 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe402-il | 100,000 | 5 | 59.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe402-il | 200,000 | 9 | 75.7 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe402-il | 200,000 | 5 | 77.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe402-il | 500,000 | 9 | 105.7 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe402-il | 500,000 | 5 | 105.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe402-il | 1,000,000 | 9 | 129.2 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe402-il | 1,000,000 | 5 | 126.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe226-il | 50,000 | 9 | 8.6 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe226-il | 50,000 | 5 | 28.6 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe226-il | 100,000 | 9 | 52.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe226-il | 100,000 | 5 | 59.7 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe226-il | 200,000 | 9 | 85.5 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe226-il | 200,000 | 5 | 78.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe226-il | 500,000 | 9 | 109.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe226-il | 500,000 | 5 | 102.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe226-il | 1,000,000 | 9 | 135.5 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe226-il | 1,000,000 | 5 | 125.9 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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