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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(ah80129-il) AH 80-129 | Althaus AH 80-129 airfoil Max thickness 12.9% at 40.2% chord Max camber 4.1% at 43.5% chord | Remove Airfoil details Airfoil plotter |
(goe137-il) GOE 137 (MVA H.15) AIRFOIL | Gottingen 137 (MVA H.15) airfoil Max thickness 8.6% at 29.9% chord Max camber 4.4% at 39.9% 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 |
(goe54-il) GOE 54 AIRFOIL | Gottingen 54 airfoil Max thickness 6.5% at 14.9% chord Max camber 3.5% at 19.9% chord | Remove Airfoil details Airfoil plotter |
(cr001sm-il) cr001sm | Cody Robertson CR 001 R/C hand-launch low Reynolds number airfoil (smoothed) Max thickness 7.3% at 27.1% chord Max camber 4.1% at 45.4% chord | Remove Airfoil details Airfoil plotter |
(goe309-il) GOE 309 (MVA H.41) AIRFOIL | Gottingen 309 (MVA H.41) airfoil Max thickness 8.4% at 30% chord Max camber 4.7% at 30% chord | Remove Airfoil details Airfoil plotter |
(fx67k150-il) FX 67-K-150/17 AIRFOIL | Wortmann FX 67-K-150/17 airfoil Max thickness 15% at 40.2% chord Max camber 4.8% at 43.5% chord | Remove Airfoil details Airfoil plotter |
(goe572-il) GOE 572 AIRFOIL | Gottingen 572 airfoil Max thickness 18.6% at 29.9% chord Max camber 8.3% at 29.9% chord | Remove Airfoil details Airfoil plotter |
(ah80140-il) AH 80-140 | Althaus AH 80-140 airfoil Max thickness 14% at 30.9% chord Max camber 4.4% at 33.9% chord | Remove Airfoil details Airfoil plotter |
(naca634421-il) NACA 63(4)-421 | NACA 63(4)-421 airfoil Max thickness 21% at 34.8% chord Max camber 2.2% at 50% chord | Remove Airfoil details Airfoil plotter |
(n64212-il) NACA 64(1)-212 | NACA 64(1)-212 airfoil Max thickness 12% at 40% chord Max camber 1.1% at 50% chord | Remove Airfoil details Airfoil plotter |
(goe398-il) GOE 398 AIRFOIL | Gottingen 398 airfoil Max thickness 13.9% at 30% chord Max camber 4.9% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe308-il) GOE 308 (MVA H.40) AIRFOIL | Gottingen 308 (MVA H.40) airfoil Max thickness 8.1% at 29.9% chord Max camber 5% at 29.9% chord | Remove Airfoil details Airfoil plotter |
(n64108-il) NACA 64-108 AIRFOIL | NACA 64-108 airfoil Max thickness 8% at 40% chord Max camber 0.6% at 50% chord | Remove Airfoil details Airfoil plotter |
(goe801-il) GOE 801 (MVA 301) AIRFOIL | Gottingen 801 (MVA 301) airfoil Max thickness 9.8% at 30% chord Max camber 6.1% at 40% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (ah80129-il,goe137-il,goe411-il,goe54-il,cr001sm-il,goe309-il,fx67k150-il,goe572-il,ah80140-il,naca634421-il,n64212-il,goe398-il,goe308-il,n64108-il,goe801-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ah80129-il | 50,000 | 9 | 18.2 at α=11.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah80129-il | 50,000 | 5 | 19 at α=10.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah80129-il | 100,000 | 9 | 37.9 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah80129-il | 100,000 | 5 | 39.4 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah80129-il | 200,000 | 9 | 79 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah80129-il | 200,000 | 5 | 78.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah80129-il | 500,000 | 9 | 124.7 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah80129-il | 500,000 | 5 | 121.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah80129-il | 1,000,000 | 9 | 152.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah80129-il | 1,000,000 | 5 | 143.7 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe137-il | 50,000 | 9 | 35.2 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe137-il | 50,000 | 5 | 39.8 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe137-il | 100,000 | 9 | 56.9 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe137-il | 100,000 | 5 | 59.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe137-il | 200,000 | 9 | 78.4 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe137-il | 200,000 | 5 | 77.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe137-il | 500,000 | 9 | 104.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe137-il | 500,000 | 5 | 97.3 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe137-il | 1,000,000 | 9 | 120.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe137-il | 1,000,000 | 5 | 109.2 at α=3.75° | 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 | |
| goe54-il | 50,000 | 9 | 19.8 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe54-il | 50,000 | 5 | 29.3 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe54-il | 100,000 | 9 | 34.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe54-il | 100,000 | 5 | 44.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe54-il | 200,000 | 9 | 58.7 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe54-il | 200,000 | 5 | 64.2 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe54-il | 500,000 | 9 | 87.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe54-il | 500,000 | 5 | 88.1 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe54-il | 1,000,000 | 9 | 106.7 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe54-il | 1,000,000 | 5 | 105.7 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cr001sm-il | 50,000 | 9 | 41.2 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cr001sm-il | 50,000 | 5 | 44.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cr001sm-il | 100,000 | 9 | 64.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cr001sm-il | 100,000 | 5 | 64.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cr001sm-il | 200,000 | 9 | 89.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cr001sm-il | 200,000 | 5 | 83.3 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cr001sm-il | 500,000 | 9 | 120.2 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cr001sm-il | 500,000 | 5 | 105.2 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| cr001sm-il | 1,000,000 | 9 | 139.9 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| cr001sm-il | 1,000,000 | 5 | 119.7 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe309-il | 50,000 | 9 | 34.3 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe309-il | 50,000 | 5 | 37.7 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe309-il | 100,000 | 9 | 54.7 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe309-il | 100,000 | 5 | 55.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe309-il | 200,000 | 9 | 73.4 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe309-il | 200,000 | 5 | 71.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe309-il | 500,000 | 9 | 97 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe309-il | 500,000 | 5 | 90.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe309-il | 1,000,000 | 9 | 113.8 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe309-il | 1,000,000 | 5 | 101.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx67k150-il | 50,000 | 9 | 5.8 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx67k150-il | 50,000 | 5 | 14.3 at α=12° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx67k150-il | 100,000 | 9 | 25 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx67k150-il | 100,000 | 5 | 27.1 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx67k150-il | 200,000 | 9 | 61.6 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx67k150-il | 200,000 | 5 | 68.5 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx67k150-il | 500,000 | 9 | 126.3 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx67k150-il | 500,000 | 5 | 118.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx67k150-il | 1,000,000 | 9 | 157.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx67k150-il | 1,000,000 | 5 | 147.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe572-il | 50,000 | 9 | 3.1 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe572-il | 50,000 | 5 | 14.6 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe572-il | 100,000 | 9 | 29.9 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe572-il | 100,000 | 5 | 38.4 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe572-il | 200,000 | 9 | 55.7 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe572-il | 200,000 | 5 | 54.8 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe572-il | 500,000 | 9 | 79.9 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe572-il | 500,000 | 5 | 77.5 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe572-il | 1,000,000 | 9 | 103.8 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe572-il | 1,000,000 | 5 | 98.6 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah80140-il | 50,000 | 9 | 5.3 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah80140-il | 50,000 | 5 | 14.3 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah80140-il | 100,000 | 9 | 22.5 at α=14° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah80140-il | 100,000 | 5 | 35.7 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah80140-il | 200,000 | 9 | 70.9 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah80140-il | 200,000 | 5 | 74.2 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah80140-il | 500,000 | 9 | 116.4 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah80140-il | 500,000 | 5 | 113.2 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah80140-il | 1,000,000 | 9 | 149.2 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah80140-il | 1,000,000 | 5 | 139 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca634421-il | 50,000 | 9 | 3.8 at α=12.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca634421-il | 50,000 | 5 | 9.4 at α=14.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca634421-il | 100,000 | 9 | 24.4 at α=13.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca634421-il | 100,000 | 5 | 35 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca634421-il | 200,000 | 9 | 61.4 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca634421-il | 200,000 | 5 | 63 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca634421-il | 500,000 | 9 | 95.3 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca634421-il | 500,000 | 5 | 90.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca634421-il | 1,000,000 | 9 | 119.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca634421-il | 1,000,000 | 5 | 109.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64212-il | 50,000 | 9 | 31.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64212-il | 50,000 | 5 | 31.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64212-il | 100,000 | 9 | 48.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64212-il | 100,000 | 5 | 45.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64212-il | 200,000 | 9 | 65.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64212-il | 200,000 | 5 | 55.9 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64212-il | 500,000 | 9 | 80.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64212-il | 500,000 | 5 | 67.8 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64212-il | 1,000,000 | 9 | 91.2 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64212-il | 1,000,000 | 5 | 73.3 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe398-il | 50,000 | 9 | 10.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe398-il | 50,000 | 5 | 31 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe398-il | 100,000 | 9 | 50.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe398-il | 100,000 | 5 | 51.5 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe398-il | 200,000 | 9 | 71.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe398-il | 200,000 | 5 | 68.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe398-il | 500,000 | 9 | 96.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe398-il | 500,000 | 5 | 92.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe398-il | 1,000,000 | 9 | 120.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe398-il | 1,000,000 | 5 | 112.5 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe308-il | 50,000 | 9 | 32.2 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe308-il | 50,000 | 5 | 37.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe308-il | 100,000 | 9 | 54.3 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe308-il | 100,000 | 5 | 55.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe308-il | 200,000 | 9 | 74.2 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe308-il | 200,000 | 5 | 74.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe308-il | 500,000 | 9 | 103 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe308-il | 500,000 | 5 | 100.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe308-il | 1,000,000 | 9 | 126.3 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe308-il | 1,000,000 | 5 | 115.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64108-il | 50,000 | 9 | 26.4 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64108-il | 50,000 | 5 | 27.6 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64108-il | 100,000 | 9 | 39 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64108-il | 100,000 | 5 | 36.2 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64108-il | 200,000 | 9 | 49.4 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64108-il | 200,000 | 5 | 43.5 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64108-il | 500,000 | 9 | 60 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64108-il | 500,000 | 5 | 50.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| n64108-il | 1,000,000 | 9 | 63.1 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| n64108-il | 1,000,000 | 5 | 65.3 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe801-il | 50,000 | 9 | 17.9 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe801-il | 50,000 | 5 | 38.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe801-il | 100,000 | 9 | 55.9 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe801-il | 100,000 | 5 | 60.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe801-il | 200,000 | 9 | 79.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe801-il | 200,000 | 5 | 79.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe801-il | 500,000 | 9 | 110.4 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe801-il | 500,000 | 5 | 104.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe801-il | 1,000,000 | 9 | 132 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe801-il | 1,000,000 | 5 | 123 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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