Airfoil Comparison
Select airfoils from the airfoil database or add your own airfoils and compare the airfoil shape and lift/drag polars.
| Open full size plan in new window | Open paginated plan in new window | |
| Download PDF file | SVG image as text file | |
| Clear all | ||
(goe481-il) GOE 481 AIRFOIL | Gottingen 481 airfoil Max thickness 13.4% at 9.6% chord Max camber 8.8% at 39.4% chord | Remove Airfoil details Airfoil plotter |
(goe177-il) GOE 177 AIRFOIL | Gottingen 177 airfoil Max thickness 7.7% at 20% chord Max camber 5% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe346-il) GOE 346 (FRIEDRICHSHAFEN-STAAKEN) AIRFOIL | Gottingen 346 (Friedrichshafen-Staaken) airfoil Max thickness 5.7% at 39.9% chord Max camber 3.8% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(goe15-il) GOE 15 AIRFOIL | Gottingen 15 airfoil Max thickness 9% at 29.8% chord Max camber 7.8% at 29.8% chord | Remove Airfoil details Airfoil plotter |
(goe458-il) GOE 458 AIRFOIL | Gottingen 458 airfoil Max thickness 7.2% at 29.9% chord Max camber 5.2% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(goe476-il) GOE 476 AIRFOIL | Gottingen 476 airfoil Max thickness 14.5% at 29.5% chord Max camber 5.2% at 39.5% chord | Remove Airfoil details Airfoil plotter |
(goe482-il) GOE 482 AIRFOIL | Gottingen 482 airfoil Max thickness 16.5% at 29.6% chord Max camber 8.8% at 39.6% chord | Remove Airfoil details Airfoil plotter |
(goe164-il) GOE 164 (MVA MK.10) AIRFOIL | Gottingen 164 (MVA MK.10) airfoil Max thickness 8.9% at 19.9% chord Max camber 6.6% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(goe370-il) GOE 370 AIRFOIL | Gottingen 370 airfoil Max thickness 4.7% at 20% chord Max camber 5.7% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe525-il) GOE 525 AIRFOIL | Gottingen 525 airfoil Max thickness 16.5% at 29.7% chord Max camber 9.7% at 49.7% chord | Remove Airfoil details Airfoil plotter |
(goe610b-il) GOE 610 B AIRFOIL | Gottingen 610 B airfoil Max thickness 7.8% at 39.9% chord Max camber 5.3% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(goe488-il) GOE 488 AIRFOIL | Gottingen 488 airfoil Max thickness 6.8% at 19.9% chord Max camber 3% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(goe397-il) GOE 397 AIRFOIL | Gottingen 397 airfoil Max thickness 5.1% at 30% chord Max camber 4% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe368-il) GOE 368 AIRFOIL | Gottingen 368 airfoil Max thickness 7.7% at 14.9% chord Max camber 3.8% at 29.9% chord | Remove Airfoil details Airfoil plotter |
(goe174-il) GOE 174 (ALBATROS 5020) AIRFOIL | Gottingen 174 (Albatros 5020) airfoil Max thickness 8.6% at 19.9% chord Max camber 5.6% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(goe377-il) GOE 377 AIRFOIL | Gottingen 377 airfoil Max thickness 6.5% at 30% chord Max camber 3.9% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe598-il) GOE 598 AIRFOIL | Gottingen 598 airfoil Max thickness 6.5% at 39.8% chord Max camber 1% at 49.8% chord | Remove Airfoil details Airfoil plotter |
(goe421-il) GOE 421 AIRFOIL | Gottingen 421 airfoil Max thickness 19% at 29.3% chord Max camber 8.1% at 49.3% chord | Remove Airfoil details Airfoil plotter |
(goe184-il) GOE 184 (MVA H.29) AIRFOIL | Gottingen 184 (MVA H.29) airfoil Max thickness 8.3% at 19.9% chord Max camber 5.3% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(goe654-il) GOE 654 AIRFOIL | Gottingen 654 airfoil Max thickness 14.5% at 30% chord Max camber 5.2% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe408-il) GOE 408 AIRFOIL | Gottingen 408 airfoil Max thickness 7.8% at 30% chord Max camber 4.1% at 30% chord | Remove Airfoil details Airfoil plotter |
(goe335-il) GOE 335 (D.F.W.) AIRFOIL | Gottingen 335 (D.F.W.) airfoil Max thickness 6.9% at 20% chord Max camber 4.8% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe505-il) GOE 505 AIRFOIL | Gottingen 505 airfoil Max thickness 14% at 19.7% chord Max camber 5.9% at 39.7% chord | Remove Airfoil details Airfoil plotter |
(goe176-il) GOE 176 (ALBATROS 7020) AIRFOIL | Gottingen 176 (Albatros 7020) airfoil Max thickness 10.3% at 19.8% chord Max camber 5.6% at 39.8% chord | Remove Airfoil details Airfoil plotter |
(goe564-il) GOE 564 AIRFOIL | Gottingen 564 airfoil Max thickness 8.2% at 30% chord Max camber 2.7% at 40% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (goe481-il,goe177-il,goe346-il,goe15-il,goe458-il,goe476-il,goe482-il,goe164-il,goe370-il,goe525-il,goe610b-il,goe488-il,goe397-il,goe368-il,goe174-il,goe377-il,goe598-il,goe421-il,goe184-il,goe654-il,goe408-il,goe335-il,goe505-il,goe176-il,goe564-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe481-il | 50,000 | 9 | 7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe481-il | 50,000 | 5 | 28.9 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe481-il | 100,000 | 9 | 43 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe481-il | 100,000 | 5 | 41.1 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe481-il | 200,000 | 9 | 53.4 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe481-il | 200,000 | 5 | 48.9 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe481-il | 500,000 | 9 | 63.4 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe481-il | 500,000 | 5 | 58.3 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe481-il | 1,000,000 | 9 | 70.3 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe481-il | 1,000,000 | 5 | 63.8 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe177-il | 50,000 | 9 | 39.1 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe177-il | 50,000 | 5 | 41.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe177-il | 100,000 | 9 | 58.3 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe177-il | 100,000 | 5 | 57.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe177-il | 200,000 | 9 | 74.7 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe177-il | 200,000 | 5 | 71.5 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe177-il | 500,000 | 9 | 91.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe177-il | 500,000 | 5 | 79.8 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe177-il | 1,000,000 | 9 | 99.9 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe177-il | 1,000,000 | 5 | 89.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe346-il | 50,000 | 9 | 40.3 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe346-il | 50,000 | 5 | 42.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe346-il | 100,000 | 9 | 61.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe346-il | 100,000 | 5 | 59.5 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe346-il | 200,000 | 9 | 81.2 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe346-il | 200,000 | 5 | 72.8 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe346-il | 500,000 | 9 | 95.5 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe346-il | 500,000 | 5 | 83 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe346-il | 1,000,000 | 9 | 100.8 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe346-il | 1,000,000 | 5 | 91.1 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe15-il | 50,000 | 9 | 8.7 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe15-il | 50,000 | 5 | 31.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe15-il | 100,000 | 9 | 46.6 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe15-il | 100,000 | 5 | 53.4 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe15-il | 200,000 | 9 | 70.7 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe15-il | 200,000 | 5 | 72.4 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe15-il | 500,000 | 9 | 126.4 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe15-il | 500,000 | 5 | 94.3 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe15-il | 1,000,000 | 9 | 128.7 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe15-il | 1,000,000 | 5 | 115.3 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe458-il | 50,000 | 9 | 42.8 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe458-il | 50,000 | 5 | 42.7 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe458-il | 100,000 | 9 | 65.1 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe458-il | 100,000 | 5 | 64.6 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe458-il | 200,000 | 9 | 87.5 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe458-il | 200,000 | 5 | 86.9 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe458-il | 500,000 | 9 | 117.8 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe458-il | 500,000 | 5 | 115.3 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe458-il | 1,000,000 | 9 | 140.9 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe458-il | 1,000,000 | 5 | 136.3 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe476-il | 50,000 | 9 | 6.4 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe476-il | 50,000 | 5 | 18.1 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe476-il | 100,000 | 9 | 44.8 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe476-il | 100,000 | 5 | 49.9 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe476-il | 200,000 | 9 | 75.2 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe476-il | 200,000 | 5 | 74.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe476-il | 500,000 | 9 | 108.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe476-il | 500,000 | 5 | 101.7 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe476-il | 1,000,000 | 9 | 132.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe476-il | 1,000,000 | 5 | 116.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe482-il | 50,000 | 9 | 4.9 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe482-il | 50,000 | 5 | 17.3 at α=1.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe482-il | 100,000 | 9 | 35.8 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe482-il | 100,000 | 5 | 51 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe482-il | 200,000 | 9 | 71.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe482-il | 200,000 | 5 | 73.9 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe482-il | 500,000 | 9 | 107.3 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe482-il | 500,000 | 5 | 100.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe482-il | 1,000,000 | 9 | 137.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe482-il | 1,000,000 | 5 | 121.4 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe164-il | 50,000 | 9 | 34.3 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe164-il | 50,000 | 5 | 43.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe164-il | 100,000 | 9 | 60.8 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe164-il | 100,000 | 5 | 62.6 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe164-il | 200,000 | 9 | 81.4 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe164-il | 200,000 | 5 | 77.4 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe164-il | 500,000 | 9 | 104.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe164-il | 500,000 | 5 | 92 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe164-il | 1,000,000 | 9 | 112.5 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe164-il | 1,000,000 | 5 | 102.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe370-il | 50,000 | 9 | 45.2 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe370-il | 50,000 | 5 | 44.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe370-il | 100,000 | 9 | 67.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe370-il | 100,000 | 5 | 67.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe370-il | 200,000 | 9 | 92 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe370-il | 200,000 | 5 | 92.3 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe370-il | 500,000 | 9 | 128.1 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe370-il | 500,000 | 5 | 121.6 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe370-il | 1,000,000 | 9 | 154.2 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe370-il | 1,000,000 | 5 | 119.5 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe525-il | 50,000 | 9 | 5.3 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe525-il | 50,000 | 5 | 20.5 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe525-il | 100,000 | 9 | 48.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe525-il | 100,000 | 5 | 50.9 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe525-il | 200,000 | 9 | 74.3 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe525-il | 200,000 | 5 | 71.5 at α=1.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe525-il | 500,000 | 9 | 102.1 at α=0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe525-il | 500,000 | 5 | 90.6 at α=0.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe525-il | 1,000,000 | 9 | 120.6 at α=0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe525-il | 1,000,000 | 5 | 104.4 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe610b-il | 50,000 | 9 | 37.4 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe610b-il | 50,000 | 5 | 38.8 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe610b-il | 100,000 | 9 | 61.2 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe610b-il | 100,000 | 5 | 62.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe610b-il | 200,000 | 9 | 86.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe610b-il | 200,000 | 5 | 84 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe610b-il | 500,000 | 9 | 118 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe610b-il | 500,000 | 5 | 95.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe610b-il | 1,000,000 | 9 | 132.2 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe610b-il | 1,000,000 | 5 | 99.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe488-il | 50,000 | 9 | 37.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe488-il | 50,000 | 5 | 37.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe488-il | 100,000 | 9 | 55.2 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe488-il | 100,000 | 5 | 51.3 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe488-il | 200,000 | 9 | 74.6 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe488-il | 200,000 | 5 | 64.8 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe488-il | 500,000 | 9 | 96.4 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe488-il | 500,000 | 5 | 79.7 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe488-il | 1,000,000 | 9 | 101.4 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe488-il | 1,000,000 | 5 | 89.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe397-il | 50,000 | 9 | 42.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe397-il | 50,000 | 5 | 43 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe397-il | 100,000 | 9 | 61.4 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe397-il | 100,000 | 5 | 61 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe397-il | 200,000 | 9 | 81.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe397-il | 200,000 | 5 | 79.1 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe397-il | 500,000 | 9 | 110 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe397-il | 500,000 | 5 | 102.1 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe397-il | 1,000,000 | 9 | 129.9 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe397-il | 1,000,000 | 5 | 97.6 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe368-il | 50,000 | 9 | 29.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe368-il | 50,000 | 5 | 36 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe368-il | 100,000 | 9 | 49.8 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe368-il | 100,000 | 5 | 50.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe368-il | 200,000 | 9 | 64.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe368-il | 200,000 | 5 | 63.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe368-il | 500,000 | 9 | 83.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe368-il | 500,000 | 5 | 83.6 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe368-il | 1,000,000 | 9 | 98.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe368-il | 1,000,000 | 5 | 98.1 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe174-il | 50,000 | 9 | 29.1 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe174-il | 50,000 | 5 | 40 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe174-il | 100,000 | 9 | 53.2 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe174-il | 100,000 | 5 | 59 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe174-il | 200,000 | 9 | 75.3 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe174-il | 200,000 | 5 | 76.6 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe174-il | 500,000 | 9 | 104.4 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe174-il | 500,000 | 5 | 101.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe174-il | 1,000,000 | 9 | 125.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe174-il | 1,000,000 | 5 | 117.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe377-il | 50,000 | 9 | 37.9 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe377-il | 50,000 | 5 | 41 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe377-il | 100,000 | 9 | 57.3 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe377-il | 100,000 | 5 | 58.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe377-il | 200,000 | 9 | 77.9 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe377-il | 200,000 | 5 | 73.9 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe377-il | 500,000 | 9 | 101.5 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe377-il | 500,000 | 5 | 91.7 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe377-il | 1,000,000 | 9 | 115.8 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe377-il | 1,000,000 | 5 | 105.2 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe598-il | 50,000 | 9 | 31.7 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe598-il | 50,000 | 5 | 30.5 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe598-il | 100,000 | 9 | 43.1 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe598-il | 100,000 | 5 | 40.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe598-il | 200,000 | 9 | 54.8 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe598-il | 200,000 | 5 | 48.6 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe598-il | 500,000 | 9 | 66.9 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe598-il | 500,000 | 5 | 54.6 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe598-il | 1,000,000 | 9 | 72.5 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe598-il | 1,000,000 | 5 | 60.8 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe421-il | 50,000 | 9 | 4.4 at α=13° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe421-il | 50,000 | 5 | 11.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe421-il | 100,000 | 9 | 31.4 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe421-il | 100,000 | 5 | 34.3 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe421-il | 200,000 | 9 | 68.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe421-il | 200,000 | 5 | 60.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe421-il | 500,000 | 9 | 96.5 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe421-il | 500,000 | 5 | 76.6 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe421-il | 1,000,000 | 9 | 103.9 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe421-il | 1,000,000 | 5 | 86.2 at α=1.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe184-il | 50,000 | 9 | 34 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe184-il | 50,000 | 5 | 39.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe184-il | 100,000 | 9 | 57.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe184-il | 100,000 | 5 | 60.4 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe184-il | 200,000 | 9 | 79.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe184-il | 200,000 | 5 | 79.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe184-il | 500,000 | 9 | 107.5 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe184-il | 500,000 | 5 | 102.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe184-il | 1,000,000 | 9 | 127.7 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe184-il | 1,000,000 | 5 | 111.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe654-il | 50,000 | 9 | 10 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe654-il | 50,000 | 5 | 28.4 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe654-il | 100,000 | 9 | 41 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe654-il | 100,000 | 5 | 50 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe654-il | 200,000 | 9 | 67.3 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe654-il | 200,000 | 5 | 67.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe654-il | 500,000 | 9 | 94.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe654-il | 500,000 | 5 | 92.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe654-il | 1,000,000 | 9 | 118.6 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe654-il | 1,000,000 | 5 | 115.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe408-il | 50,000 | 9 | 35.8 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe408-il | 50,000 | 5 | 40.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe408-il | 100,000 | 9 | 58.3 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe408-il | 100,000 | 5 | 59.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe408-il | 200,000 | 9 | 78.4 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe408-il | 200,000 | 5 | 75.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe408-il | 500,000 | 9 | 101.8 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe408-il | 500,000 | 5 | 94.7 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe408-il | 1,000,000 | 9 | 119.8 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe408-il | 1,000,000 | 5 | 102.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe335-il | 50,000 | 9 | 38.6 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe335-il | 50,000 | 5 | 41.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe335-il | 100,000 | 9 | 56.6 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe335-il | 100,000 | 5 | 57.9 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe335-il | 200,000 | 9 | 75.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe335-il | 200,000 | 5 | 75.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe335-il | 500,000 | 9 | 102.1 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe335-il | 500,000 | 5 | 100.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe335-il | 1,000,000 | 9 | 123.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe335-il | 1,000,000 | 5 | 119.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe505-il | 50,000 | 9 | 12.3 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe505-il | 50,000 | 5 | 29.8 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe505-il | 100,000 | 9 | 49.1 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe505-il | 100,000 | 5 | 43.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe505-il | 200,000 | 9 | 68.7 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe505-il | 200,000 | 5 | 53.8 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe505-il | 500,000 | 9 | 73.5 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe505-il | 500,000 | 5 | 69.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe505-il | 1,000,000 | 9 | 91 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe505-il | 1,000,000 | 5 | 87.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe176-il | 50,000 | 9 | 30.3 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe176-il | 50,000 | 5 | 40.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe176-il | 100,000 | 9 | 56 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe176-il | 100,000 | 5 | 57.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe176-il | 200,000 | 9 | 73.7 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe176-il | 200,000 | 5 | 73.6 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe176-il | 500,000 | 9 | 99.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe176-il | 500,000 | 5 | 87 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe176-il | 1,000,000 | 9 | 113.1 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe176-il | 1,000,000 | 5 | 93.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe564-il | 50,000 | 9 | 37.1 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe564-il | 50,000 | 5 | 37.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe564-il | 100,000 | 9 | 56 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe564-il | 100,000 | 5 | 52.6 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe564-il | 200,000 | 9 | 75.4 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe564-il | 200,000 | 5 | 65.6 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe564-il | 500,000 | 9 | 95.7 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe564-il | 500,000 | 5 | 77.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe564-il | 1,000,000 | 9 | 103.8 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe564-il | 1,000,000 | 5 | 89.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| Reynolds number calculator | |||||||