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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(goe499-il) GOE 499 AIRFOIL | Gottingen 499 airfoil Max thickness 6.8% at 30% chord Max camber 5.9% at 50% chord | Remove Airfoil details Airfoil plotter |
(goe124-il) GOE 124 (MVA H.4) AIRFOIL | Gottingen 124 (MVA H.4) airfoil Max thickness 7.9% at 29.9% chord Max camber 5.6% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(goe795-il) GOE 795 AIRFOIL | Gottingen 795 airfoil Max thickness 8% at 30.9% chord Max camber 2.4% at 43.5% 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 |
(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 |
(goe508-il) GOE 508 AIRFOIL | Gottingen 508 airfoil Max thickness 16.5% at 30% chord Max camber 5.6% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe117-il) GOE 117 (MVA MK.4) AIRFOIL | Gottingen 117 (MVA MK.4) airfoil Max thickness 9% at 29.8% chord Max camber 4.6% at 39.8% chord | Remove Airfoil details Airfoil plotter |
(goe561-il) GOE 561 AIRFOIL | Gottingen 561 airfoil Max thickness 25% at 29.8% chord Max camber 10.2% at 29.8% chord | Remove Airfoil details Airfoil plotter |
(goe284-il) GOE 284 AIRFOIL | Gottingen 284 airfoil Max thickness 17.7% at 29.3% chord Max camber 5.1% at 39.3% chord | Remove Airfoil details Airfoil plotter |
(goe506-il) GOE 506 AIRFOIL | Gottingen 506 airfoil Max thickness 16.5% at 29.3% chord Max camber 4.7% at 39.3% chord | Remove Airfoil details Airfoil plotter |
(goe325-il) GOE 325 (PFALZ 54) AIRFOIL | Gottingen 325 (Pfalz 54) airfoil Max thickness 8.2% at 20% chord Max camber 4.6% at 30% chord | Remove Airfoil details Airfoil plotter |
(goe804-il) GOE 804 (EA 8) AIRFOIL | Gottingen 804 (EA 8) airfoil Max thickness 6% at 40% chord Max camber 6.3% at 50% chord | Remove Airfoil details Airfoil plotter |
(goe425-il) GOE 425 AIRFOIL | Gottingen 425 airfoil Max thickness 16% at 29.3% chord Max camber 4.5% at 39.3% chord | Remove Airfoil details Airfoil plotter |
(goe07k-il) GOE 7K AIRFOIL | Gottingen 7K airfoil Max thickness 11% at 50% chord Max camber 4.5% at 50% 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 |
(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 |
(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 |
(goe483-il) GOE 483 AIRFOIL | Gottingen 483 airfoil Max thickness 5.5% at 15% chord Max camber 5.8% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe796-il) GOE 796 AIRFOIL | Gottingen 796 airfoil Max thickness 12% at 30% chord Max camber 3.6% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe379-il) GOE 379 AIRFOIL | Gottingen 379 airfoil Max thickness 6.5% at 30% chord Max camber 5.2% at 40% 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 |
(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 |
(goe617-il) GOE 617 AIRFOIL | Gottingen 617 airfoil Max thickness 13.9% at 30% chord Max camber 2.2% at 30% chord | Remove Airfoil details Airfoil plotter |
(goe223-il) GOE 223 (MVA H.34) AIRFOIL | Gottingen 223 (MVA H.34) airfoil Max thickness 18.8% at 29.1% chord Max camber 5.7% at 49.1% chord | Remove Airfoil details Airfoil plotter |
(goe527-il) GOE 527 AIRFOIL | Gottingen 527 airfoil Max thickness 16.5% at 29.5% chord Max camber 5.8% at 39.5% chord | Remove Airfoil details Airfoil plotter |
(goe412-il) GOE 412 AIRFOIL | Gottingen 412 airfoil Max thickness 13.1% at 29.7% chord Max camber 5.1% at 39.7% chord | Remove Airfoil details Airfoil plotter |
(goe14k-il) GOE 14K AIRFOIL | Gottingen 14K airfoil Max thickness 12% at 50% chord Max camber 2.7% at 50% chord | Remove Airfoil details Airfoil plotter |
(goe133-il) GOE 133 (MVA H.11) AIRFOIL | Gottingen 133 (MVA H.11) airfoil Max thickness 7.9% at 30% chord Max camber 4.3% at 30% chord | Remove Airfoil details Airfoil plotter |
(goe198-il) GOE 198 (L.F.G. 5294) AIRFOIL | Gottingen 198 (L.F.G. 5294) airfoil Max thickness 7.8% at 19.9% chord Max camber 6.5% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(goe474-il) GOE 474 AIRFOIL | Gottingen 474 airfoil Max thickness 7% at 30% chord Max camber 2.9% at 40% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (goe499-il,goe124-il,goe795-il,goe147-il,goe490-il,goe508-il,goe117-il,goe561-il,goe284-il,goe506-il,goe325-il,goe804-il,goe425-il,goe07k-il,goe361-il,goe167-il,goe180-il,goe483-il,goe796-il,goe379-il,goe533-il,goe411-il,goe460-il,goe617-il,goe223-il,goe527-il,goe412-il,goe14k-il,goe133-il,goe198-il,goe474-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe499-il | 50,000 | 9 | 38.8 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe499-il | 50,000 | 5 | 44.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe499-il | 100,000 | 9 | 71.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe499-il | 100,000 | 5 | 69.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe499-il | 200,000 | 9 | 102.2 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe499-il | 200,000 | 5 | 99.1 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe499-il | 500,000 | 9 | 149.4 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe499-il | 500,000 | 5 | 118.3 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe499-il | 1,000,000 | 9 | 157.8 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe499-il | 1,000,000 | 5 | 111.9 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe124-il | 50,000 | 9 | 35.9 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe124-il | 50,000 | 5 | 41.2 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe124-il | 100,000 | 9 | 60.2 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe124-il | 100,000 | 5 | 63.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe124-il | 200,000 | 9 | 84.4 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe124-il | 200,000 | 5 | 83.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe124-il | 500,000 | 9 | 114.8 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe124-il | 500,000 | 5 | 107.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe124-il | 1,000,000 | 9 | 133.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe124-il | 1,000,000 | 5 | 126.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe795-il | 50,000 | 9 | 38 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe795-il | 50,000 | 5 | 37.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe795-il | 100,000 | 9 | 56.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe795-il | 100,000 | 5 | 53.6 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe795-il | 200,000 | 9 | 75.4 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe795-il | 200,000 | 5 | 67.5 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe795-il | 500,000 | 9 | 95.7 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe795-il | 500,000 | 5 | 80.2 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe795-il | 1,000,000 | 9 | 105 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe795-il | 1,000,000 | 5 | 84.9 at α=6.25° | 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 | |
| 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 | |
| goe508-il | 50,000 | 9 | 5.2 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe508-il | 50,000 | 5 | 13.5 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe508-il | 100,000 | 9 | 40.3 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe508-il | 100,000 | 5 | 43.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe508-il | 200,000 | 9 | 71.3 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe508-il | 200,000 | 5 | 69.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe508-il | 500,000 | 9 | 105.7 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe508-il | 500,000 | 5 | 97.8 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe508-il | 1,000,000 | 9 | 132.8 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe508-il | 1,000,000 | 5 | 115.9 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe117-il | 50,000 | 9 | 32.5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe117-il | 50,000 | 5 | 38.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe117-il | 100,000 | 9 | 58.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe117-il | 100,000 | 5 | 58.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe117-il | 200,000 | 9 | 78.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe117-il | 200,000 | 5 | 77.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe117-il | 500,000 | 9 | 107.8 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe117-il | 500,000 | 5 | 104.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe117-il | 1,000,000 | 9 | 131.1 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe117-il | 1,000,000 | 5 | 116.9 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe561-il | 50,000 | 9 | 3.3 at α=-13.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe561-il | 50,000 | 5 | 5.7 at α=-8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe561-il | 100,000 | 9 | 8.4 at α=-8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe561-il | 100,000 | 5 | 8.6 at α=-6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe561-il | 200,000 | 9 | 28.7 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe561-il | 200,000 | 5 | 20.9 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe561-il | 500,000 | 9 | 43.2 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe561-il | 500,000 | 5 | 33 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe561-il | 1,000,000 | 9 | 49.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe561-il | 1,000,000 | 5 | 42 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe284-il | 50,000 | 9 | 4.3 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe284-il | 50,000 | 5 | 18 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe284-il | 100,000 | 9 | 34.1 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe284-il | 100,000 | 5 | 45.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe284-il | 200,000 | 9 | 69 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe284-il | 200,000 | 5 | 69.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe284-il | 500,000 | 9 | 103.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe284-il | 500,000 | 5 | 95 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe284-il | 1,000,000 | 9 | 126.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe284-il | 1,000,000 | 5 | 107.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe506-il | 50,000 | 9 | 10.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe506-il | 50,000 | 5 | 28 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe506-il | 100,000 | 9 | 45.1 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe506-il | 100,000 | 5 | 40.7 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe506-il | 200,000 | 9 | 58 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe506-il | 200,000 | 5 | 48.4 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe506-il | 500,000 | 9 | 64.2 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe506-il | 500,000 | 5 | 61.9 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe506-il | 1,000,000 | 9 | 81.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe506-il | 1,000,000 | 5 | 75.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe325-il | 50,000 | 9 | 35.1 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe325-il | 50,000 | 5 | 37.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe325-il | 100,000 | 9 | 53.7 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe325-il | 100,000 | 5 | 55.3 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe325-il | 200,000 | 9 | 72.9 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe325-il | 200,000 | 5 | 73.4 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe325-il | 500,000 | 9 | 100 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe325-il | 500,000 | 5 | 98.3 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe325-il | 1,000,000 | 9 | 121.4 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe325-il | 1,000,000 | 5 | 117.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe804-il | 50,000 | 9 | 43.7 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe804-il | 50,000 | 5 | 41.1 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe804-il | 100,000 | 9 | 70.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe804-il | 100,000 | 5 | 67.6 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe804-il | 200,000 | 9 | 107.1 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe804-il | 200,000 | 5 | 107 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe804-il | 500,000 | 9 | 169.1 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe804-il | 500,000 | 5 | 157.3 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe804-il | 1,000,000 | 9 | 211.4 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe804-il | 1,000,000 | 5 | 147 at α=0° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe425-il | 50,000 | 9 | 5.2 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe425-il | 50,000 | 5 | 17.4 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe425-il | 100,000 | 9 | 22.7 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe425-il | 100,000 | 5 | 44.6 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe425-il | 200,000 | 9 | 69.8 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe425-il | 200,000 | 5 | 74 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe425-il | 500,000 | 9 | 111 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe425-il | 500,000 | 5 | 108.4 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe425-il | 1,000,000 | 9 | 142.1 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe425-il | 1,000,000 | 5 | 132.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe07k-il | 50,000 | 9 | 24.4 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe07k-il | 50,000 | 5 | 25.2 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe07k-il | 100,000 | 9 | 38.7 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe07k-il | 100,000 | 5 | 40.7 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe07k-il | 200,000 | 9 | 69.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe07k-il | 200,000 | 5 | 70.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe07k-il | 500,000 | 9 | 122.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe07k-il | 500,000 | 5 | 116.5 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe07k-il | 1,000,000 | 9 | 159.9 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe07k-il | 1,000,000 | 5 | 142.8 at α=2.75° | 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 | |
| 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 | |
| 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 | |
| goe483-il | 50,000 | 9 | 42.8 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe483-il | 50,000 | 5 | 44.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe483-il | 100,000 | 9 | 62.7 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe483-il | 100,000 | 5 | 65.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe483-il | 200,000 | 9 | 83.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe483-il | 200,000 | 5 | 85.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe483-il | 500,000 | 9 | 114.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe483-il | 500,000 | 5 | 112.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe483-il | 1,000,000 | 9 | 137.4 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe483-il | 1,000,000 | 5 | 121.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe796-il | 50,000 | 9 | 32.2 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe796-il | 50,000 | 5 | 35.5 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe796-il | 100,000 | 9 | 55.5 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe796-il | 100,000 | 5 | 55.6 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe796-il | 200,000 | 9 | 78 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe796-il | 200,000 | 5 | 73.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe796-il | 500,000 | 9 | 105.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe796-il | 500,000 | 5 | 90.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe796-il | 1,000,000 | 9 | 122.7 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe796-il | 1,000,000 | 5 | 105.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe379-il | 50,000 | 9 | 39.6 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe379-il | 50,000 | 5 | 41 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe379-il | 100,000 | 9 | 58.2 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe379-il | 100,000 | 5 | 60.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe379-il | 200,000 | 9 | 77.7 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe379-il | 200,000 | 5 | 79.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe379-il | 500,000 | 9 | 106 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe379-il | 500,000 | 5 | 103.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe379-il | 1,000,000 | 9 | 126.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe379-il | 1,000,000 | 5 | 121.5 at α=4° | 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 | |
| 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 | |
| goe617-il | 50,000 | 9 | 29.3 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe617-il | 50,000 | 5 | 31.4 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe617-il | 100,000 | 9 | 49.4 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe617-il | 100,000 | 5 | 48.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe617-il | 200,000 | 9 | 67.2 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe617-il | 200,000 | 5 | 63 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe617-il | 500,000 | 9 | 87.9 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe617-il | 500,000 | 5 | 72.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe617-il | 1,000,000 | 9 | 91 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe617-il | 1,000,000 | 5 | 82.3 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe223-il | 50,000 | 9 | 5 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe223-il | 50,000 | 5 | 15.8 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe223-il | 100,000 | 9 | 43.4 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe223-il | 100,000 | 5 | 48.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe223-il | 200,000 | 9 | 73 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe223-il | 200,000 | 5 | 67 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe223-il | 500,000 | 9 | 95.5 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe223-il | 500,000 | 5 | 80.6 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe223-il | 1,000,000 | 9 | 108.5 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe223-il | 1,000,000 | 5 | 80.4 at α=0.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe527-il | 50,000 | 9 | 4.3 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe527-il | 50,000 | 5 | 15.9 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe527-il | 100,000 | 9 | 36.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe527-il | 100,000 | 5 | 47 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe527-il | 200,000 | 9 | 69.5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe527-il | 200,000 | 5 | 69.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe527-il | 500,000 | 9 | 102.3 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe527-il | 500,000 | 5 | 96.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe527-il | 1,000,000 | 9 | 128.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe527-il | 1,000,000 | 5 | 116.9 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe412-il | 50,000 | 9 | 15.9 at α=15.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe412-il | 50,000 | 5 | 26.8 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe412-il | 100,000 | 9 | 54.7 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe412-il | 100,000 | 5 | 55.8 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe412-il | 200,000 | 9 | 82.9 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe412-il | 200,000 | 5 | 79.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe412-il | 500,000 | 9 | 116.5 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe412-il | 500,000 | 5 | 103.2 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe412-il | 1,000,000 | 9 | 137.7 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe412-il | 1,000,000 | 5 | 113.7 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe14k-il | 50,000 | 9 | 25.3 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe14k-il | 50,000 | 5 | 25.4 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe14k-il | 100,000 | 9 | 36 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe14k-il | 100,000 | 5 | 38.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe14k-il | 200,000 | 9 | 60.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe14k-il | 200,000 | 5 | 59.8 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe14k-il | 500,000 | 9 | 100.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe14k-il | 500,000 | 5 | 76.8 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe14k-il | 1,000,000 | 9 | 98.1 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe14k-il | 1,000,000 | 5 | 86.1 at α=1.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe133-il | 50,000 | 9 | 33.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe133-il | 50,000 | 5 | 40.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe133-il | 100,000 | 9 | 53.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe133-il | 100,000 | 5 | 58.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe133-il | 200,000 | 9 | 74.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe133-il | 200,000 | 5 | 74.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe133-il | 500,000 | 9 | 99.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe133-il | 500,000 | 5 | 93 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe133-il | 1,000,000 | 9 | 114.9 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe133-il | 1,000,000 | 5 | 108 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe198-il | 50,000 | 9 | 36.2 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe198-il | 50,000 | 5 | 43.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe198-il | 100,000 | 9 | 64.5 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe198-il | 100,000 | 5 | 64 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe198-il | 200,000 | 9 | 88.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe198-il | 200,000 | 5 | 80.4 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe198-il | 500,000 | 9 | 112.3 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe198-il | 500,000 | 5 | 92.9 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe198-il | 1,000,000 | 9 | 117 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe198-il | 1,000,000 | 5 | 92.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe474-il | 50,000 | 9 | 38.4 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe474-il | 50,000 | 5 | 38.3 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe474-il | 100,000 | 9 | 57 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe474-il | 100,000 | 5 | 54.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe474-il | 200,000 | 9 | 77.1 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe474-il | 200,000 | 5 | 70.1 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe474-il | 500,000 | 9 | 101.6 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe474-il | 500,000 | 5 | 85.1 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe474-il | 1,000,000 | 9 | 115.8 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe474-il | 1,000,000 | 5 | 91 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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