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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(goe711-il) GOE 711 AIRFOIL | Gottingen 711 airfoil Max thickness 14.9% at 30% chord Max camber 6.3% at 30% chord | Remove Airfoil details Airfoil plotter |
(goe481a-il) GOE 481A AIRFOIL | Gottingen 481A airfoil Max thickness 15.3% at 29.4% chord Max camber 5.5% at 39.4% chord | Remove Airfoil details Airfoil plotter |
(goe422-il) GOE 422 AIRFOIL | Gottingen 422 airfoil Max thickness 17.1% at 29.5% chord Max camber 6.5% at 39.5% chord | Remove Airfoil details Airfoil plotter |
(goe423-il) GOE 423 AIRFOIL | Gottingen 423 airfoil Max thickness 16.9% at 39.7% chord Max camber 5.1% at 39.7% chord | Remove Airfoil details Airfoil plotter |
(goe134-il) GOE 134 (MVA H.12) AIRFOIL | Gottingen 134 (MVA H.12) airfoil Max thickness 9.5% at 30% chord Max camber 4% at 30% chord | Remove Airfoil details Airfoil plotter |
(goe373-il) GOE 373 AIRFOIL | Gottingen 373 airfoil Max thickness 6.5% at 29.9% chord Max camber 5.1% at 39.9% 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 |
(goe322-il) GOE 322 (HANSA-BRANDENBURG IV.1) AIRFOIL | Gottingen 322 (Hansa-Brandenburg IV.1) airfoil Max thickness 13.1% at 29.8% chord Max camber 6% at 29.8% 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 |
(goe600-il) GOE 600 AIRFOIL | Gottingen 600 airfoil Max thickness 13.1% at 29.4% chord Max camber 1.9% at 49.4% chord | Remove Airfoil details Airfoil plotter |
(goe187-il) GOE 187 (SCHTTE-LANZ 2U10) AIRFOIL | Gottingen 187 (Schatte-Lanz 2U10) airfoil Max thickness 8.3% at 30% chord Max camber 4.8% at 30% chord | Remove Airfoil details Airfoil plotter |
(goe381-il) GOE 381 AIRFOIL | Gottingen 381 airfoil Max thickness 6.4% at 30% chord Max camber 5.8% at 30% chord | Remove Airfoil details Airfoil plotter |
(goe142-il) GOE 142 (MVA H.19) AIRFOIL | Gottingen 142 (MVA H.19) airfoil Max thickness 6.2% at 24.9% chord Max camber 3.8% at 34.9% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (goe711-il,goe481a-il,goe422-il,goe423-il,goe134-il,goe373-il,goe477-il,goe144-il,goe322-il,goe402-il,goe226-il,goe600-il,goe187-il,goe381-il,goe142-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe711-il | 50,000 | 9 | 20.3 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe711-il | 50,000 | 5 | 33.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe711-il | 100,000 | 9 | 48.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe711-il | 100,000 | 5 | 49.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe711-il | 200,000 | 9 | 64.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe711-il | 200,000 | 5 | 62.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe711-il | 500,000 | 9 | 86.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe711-il | 500,000 | 5 | 83.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe711-il | 1,000,000 | 9 | 107.2 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe711-il | 1,000,000 | 5 | 102.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe481a-il | 50,000 | 9 | 6.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe481a-il | 50,000 | 5 | 27.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe481a-il | 100,000 | 9 | 47.3 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe481a-il | 100,000 | 5 | 46.3 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe481a-il | 200,000 | 9 | 63.8 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe481a-il | 200,000 | 5 | 59 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe481a-il | 500,000 | 9 | 80.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe481a-il | 500,000 | 5 | 74.1 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe481a-il | 1,000,000 | 9 | 95.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe481a-il | 1,000,000 | 5 | 81.3 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe422-il | 50,000 | 9 | 5.8 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe422-il | 50,000 | 5 | 19.4 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe422-il | 100,000 | 9 | 44.9 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe422-il | 100,000 | 5 | 47.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe422-il | 200,000 | 9 | 71 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe422-il | 200,000 | 5 | 66.5 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe422-il | 500,000 | 9 | 97.4 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe422-il | 500,000 | 5 | 85.3 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe422-il | 1,000,000 | 9 | 117.3 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe422-il | 1,000,000 | 5 | 98.8 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe423-il | 50,000 | 9 | 4.7 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe423-il | 50,000 | 5 | 14.4 at α=0.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe423-il | 100,000 | 9 | 22.8 at α=0.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe423-il | 100,000 | 5 | 40.2 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe423-il | 200,000 | 9 | 69.3 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe423-il | 200,000 | 5 | 70.5 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe423-il | 500,000 | 9 | 105.9 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe423-il | 500,000 | 5 | 101.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe423-il | 1,000,000 | 9 | 133.4 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe423-il | 1,000,000 | 5 | 124.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe134-il | 50,000 | 9 | 29.4 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe134-il | 50,000 | 5 | 38.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe134-il | 100,000 | 9 | 50.7 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe134-il | 100,000 | 5 | 55.2 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe134-il | 200,000 | 9 | 70.4 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe134-il | 200,000 | 5 | 71.7 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe134-il | 500,000 | 9 | 96.1 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe134-il | 500,000 | 5 | 93.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe134-il | 1,000,000 | 9 | 114.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe134-il | 1,000,000 | 5 | 109.7 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe373-il | 50,000 | 9 | 35.5 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe373-il | 50,000 | 5 | 41.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe373-il | 100,000 | 9 | 59 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe373-il | 100,000 | 5 | 61.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe373-il | 200,000 | 9 | 80.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe373-il | 200,000 | 5 | 79 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe373-il | 500,000 | 9 | 105.9 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe373-il | 500,000 | 5 | 94.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe373-il | 1,000,000 | 9 | 105 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe373-il | 1,000,000 | 5 | 93.7 at α=4° | 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 | |
| goe322-il | 50,000 | 9 | 9.2 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe322-il | 50,000 | 5 | 28.9 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe322-il | 100,000 | 9 | 49.9 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe322-il | 100,000 | 5 | 53.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe322-il | 200,000 | 9 | 75.2 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe322-il | 200,000 | 5 | 73.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe322-il | 500,000 | 9 | 104.8 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe322-il | 500,000 | 5 | 95.7 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe322-il | 1,000,000 | 9 | 123.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe322-il | 1,000,000 | 5 | 114.2 at α=5.75° | 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 | |
| goe600-il | 50,000 | 9 | 32.5 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe600-il | 50,000 | 5 | 33.9 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe600-il | 100,000 | 9 | 51.1 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe600-il | 100,000 | 5 | 49.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe600-il | 200,000 | 9 | 69.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe600-il | 200,000 | 5 | 62.9 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe600-il | 500,000 | 9 | 91.2 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe600-il | 500,000 | 5 | 76.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe600-il | 1,000,000 | 9 | 99.6 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe600-il | 1,000,000 | 5 | 86 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe187-il | 50,000 | 9 | 31.8 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe187-il | 50,000 | 5 | 40.3 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe187-il | 100,000 | 9 | 53.7 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe187-il | 100,000 | 5 | 58.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe187-il | 200,000 | 9 | 74.4 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe187-il | 200,000 | 5 | 76.1 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe187-il | 500,000 | 9 | 100.9 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe187-il | 500,000 | 5 | 98.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe187-il | 1,000,000 | 9 | 118.9 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe187-il | 1,000,000 | 5 | 112.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe381-il | 50,000 | 9 | 37.6 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe381-il | 50,000 | 5 | 43 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe381-il | 100,000 | 9 | 58.9 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe381-il | 100,000 | 5 | 61.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe381-il | 200,000 | 9 | 80 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe381-il | 200,000 | 5 | 76.4 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe381-il | 500,000 | 9 | 100.7 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe381-il | 500,000 | 5 | 92 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe381-il | 1,000,000 | 9 | 111.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe381-il | 1,000,000 | 5 | 93.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe142-il | 50,000 | 9 | 36.1 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe142-il | 50,000 | 5 | 41 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe142-il | 100,000 | 9 | 55.7 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe142-il | 100,000 | 5 | 56.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe142-il | 200,000 | 9 | 74.2 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe142-il | 200,000 | 5 | 72.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe142-il | 500,000 | 9 | 99 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe142-il | 500,000 | 5 | 94.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe142-il | 1,000,000 | 9 | 118.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe142-il | 1,000,000 | 5 | 111.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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