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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(sg6050-il) SG6050 | Selig / Giguere SG6050 wind turbine airfoil Max thickness 16% at 31.5% chord Max camber 3.1% at 48.9% chord | Remove Airfoil details Airfoil plotter |
(stf86361-il) EPPLER STF 863-615 AIRFOIL | Eppler STF 863-615 airfoil Max thickness 14.7% at 44.7% chord Max camber 4.2% at 72.3% chord | Remove Airfoil details Airfoil plotter |
(sa7035-il) SA7035 | Selig / Ashok Gopalarathnam SA7035 Max thickness 9.2% at 27.9% chord Max camber 2.4% at 41.9% chord | Remove Airfoil details Airfoil plotter |
(ste87391-il) EPPLER STE 87(-3)-914 AIRFOIL | Eppler STE 87(-3)-914 airfoil Max thickness 14.6% at 34.1% chord Max camber 4.2% at 58.3% chord | Remove Airfoil details Airfoil plotter |
(sg6040-il) SG6040 | Selig / Giguere SG6040 wind turbine airfoil Max thickness 16% at 35.3% chord Max camber 2.3% at 60.5% chord | Remove Airfoil details Airfoil plotter |
(s4180-il) S4180-098-84 | Selig S4180 low Reynolds number airfoil Max thickness 9.8% at 26.1% chord Max camber 4% at 39.4% chord | Remove Airfoil details Airfoil plotter |
(sd7090-il) SD7090 (10%) | Selig/Donovan SD7090 low Reynolds number airfoil Max thickness 10% at 29.3% chord Max camber 1.5% at 43.6% chord | Remove Airfoil details Airfoil plotter |
(sa7036-il) SA7036 | Selig / Ashok Gopalarathnam SA7036 Max thickness 9.2% at 28.1% chord Max camber 2.6% at 42.1% chord | Remove Airfoil details Airfoil plotter |
(sc20610-il) NASA SC(2)-0610 AIRFOIL | NASA SC(2)-0610 airfoil (NASA TP-2969) Max thickness 10% at 38% chord Max camber 1.8% at 82% chord | Remove Airfoil details Airfoil plotter |
(sd7062-il) SD7062 (14%) | Selig/Donovan SD7062 low Reynolds number airfoil Max thickness 14% at 25.5% chord Max camber 3.5% at 38.8% chord | Remove Airfoil details Airfoil plotter |
(sg6043-il) SG6043 | Selig / Giguere SG6043 wind turbine airfoil (high L/D) Max thickness 10% at 32.1% chord Max camber 5.1% at 53.3% chord | Remove Airfoil details Airfoil plotter |
(sg6041-il) SG6041 | Selig / Giguere SG6041 wind turbine airfoil (high L/D) Max thickness 10% at 34.9% chord Max camber 1.6% at 49.7% chord | Remove Airfoil details Airfoil plotter |
(sd7034-il) SD7034 | Selig/Donovan SD7034 low Reynolds number airfoil Max thickness 10.5% at 26% chord Max camber 3.6% at 39.4% chord | Remove Airfoil details Airfoil plotter |
(s4053-il) S4053 | Selig S4053 low Reynolds number airfoil Max thickness 8.9% at 30.9% chord Max camber 3% at 45% chord | Remove Airfoil details Airfoil plotter |
(s4095-il) S4095 (designed for the E-flite UMX ASK-21 scale RC sailplane) | Selig airfoil for micro RC soaring. Used on the E-flite UMX ASK-21 scale RC sailplane. Max thickness 9.7% at 29.1% chord Max camber 1.7% at 33.7% chord | Remove Airfoil details Airfoil plotter |
(s3016-il) S3016-095-87 | Selig S3016 low Reynolds number airfoil Max thickness 9.5% at 28.9% chord Max camber 1.8% at 43.1% chord | Remove Airfoil details Airfoil plotter |
(s806a-nr) NREL's S806A Airfoil (modified line 35) | NREL HAWT airfoil S806A tip Max thickness 11.5% at 45% chord Max camber 2.8% at 45% chord | Remove Airfoil details Airfoil plotter |
(s3010-il) S3010-103-84 | Selig S3010 low Reynolds number airfoil Max thickness 10.3% at 25% chord Max camber 2.3% at 43.3% chord | Remove Airfoil details Airfoil plotter |
(sc20412-il) NASA SC(2)-0412 AIRFOIL | NASA SC(2)-0412 airfoil (NASA TP-2969) Max thickness 12% at 37% chord Max camber 1.3% at 83% chord | Remove Airfoil details Airfoil plotter |
(sc20706-il) NASA SC(2)-0706 AIRFOIL | NASA SC(2)-0706 airfoil (NASA TP-2969) Max thickness 6% at 34% chord Max camber 1.6% at 82% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (sg6050-il,stf86361-il,sa7035-il,ste87391-il,sg6040-il,s4180-il,sd7090-il,sa7036-il,sc20610-il,sd7062-il,sg6043-il,sg6041-il,sd7034-il,s4053-il,s4095-il,s3016-il,s806a-nr,s3010-il,sc20412-il,sc20706-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| sg6050-il | 50,000 | 9 | 8.2 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6050-il | 50,000 | 5 | 25.6 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6050-il | 100,000 | 9 | 50 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6050-il | 100,000 | 5 | 52.4 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6050-il | 200,000 | 9 | 74.7 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6050-il | 200,000 | 5 | 73.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6050-il | 500,000 | 9 | 105.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6050-il | 500,000 | 5 | 97.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6050-il | 1,000,000 | 9 | 126.5 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6050-il | 1,000,000 | 5 | 113 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| stf86361-il | 50,000 | 9 | 22.2 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| stf86361-il | 50,000 | 5 | 23.7 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| stf86361-il | 100,000 | 9 | 32.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| stf86361-il | 100,000 | 5 | 34.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| stf86361-il | 200,000 | 9 | 54.3 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| stf86361-il | 200,000 | 5 | 56.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| stf86361-il | 500,000 | 9 | 92.2 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| stf86361-il | 500,000 | 5 | 98.7 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| stf86361-il | 1,000,000 | 9 | 145.1 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| stf86361-il | 1,000,000 | 5 | 142.7 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7035-il | 50,000 | 9 | 33.2 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7035-il | 50,000 | 5 | 37.8 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7035-il | 100,000 | 9 | 52.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7035-il | 100,000 | 5 | 53.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7035-il | 200,000 | 9 | 71.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7035-il | 200,000 | 5 | 68 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7035-il | 500,000 | 9 | 94.9 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7035-il | 500,000 | 5 | 87.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7035-il | 1,000,000 | 9 | 111.4 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7035-il | 1,000,000 | 5 | 101.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ste87391-il | 50,000 | 9 | 32.2 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ste87391-il | 50,000 | 5 | 30.9 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ste87391-il | 100,000 | 9 | 51.3 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ste87391-il | 100,000 | 5 | 45.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ste87391-il | 200,000 | 9 | 69.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ste87391-il | 200,000 | 5 | 61.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ste87391-il | 500,000 | 9 | 97.4 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ste87391-il | 500,000 | 5 | 92.5 at α=1.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ste87391-il | 1,000,000 | 9 | 146 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ste87391-il | 1,000,000 | 5 | 106.6 at α=-0.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6040-il | 50,000 | 9 | 26.1 at α=11.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6040-il | 50,000 | 5 | 26.4 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6040-il | 100,000 | 9 | 50.5 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6040-il | 100,000 | 5 | 50.9 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6040-il | 200,000 | 9 | 72.9 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6040-il | 200,000 | 5 | 68.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6040-il | 500,000 | 9 | 96.6 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6040-il | 500,000 | 5 | 88.5 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6040-il | 1,000,000 | 9 | 114.7 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6040-il | 1,000,000 | 5 | 102.3 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4180-il | 50,000 | 9 | 28.3 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4180-il | 50,000 | 5 | 37.7 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4180-il | 100,000 | 9 | 55.1 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4180-il | 100,000 | 5 | 58.8 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4180-il | 200,000 | 9 | 78.7 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4180-il | 200,000 | 5 | 78.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4180-il | 500,000 | 9 | 110.5 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4180-il | 500,000 | 5 | 104.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4180-il | 1,000,000 | 9 | 133.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4180-il | 1,000,000 | 5 | 122.6 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7090-il | 50,000 | 9 | 30.7 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7090-il | 50,000 | 5 | 34.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7090-il | 100,000 | 9 | 47.1 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7090-il | 100,000 | 5 | 47.6 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7090-il | 200,000 | 9 | 62.9 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7090-il | 200,000 | 5 | 60.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7090-il | 500,000 | 9 | 83.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7090-il | 500,000 | 5 | 78.3 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7090-il | 1,000,000 | 9 | 99 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7090-il | 1,000,000 | 5 | 92.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7036-il | 50,000 | 9 | 33.6 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7036-il | 50,000 | 5 | 38.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7036-il | 100,000 | 9 | 53.9 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7036-il | 100,000 | 5 | 54.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7036-il | 200,000 | 9 | 73 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7036-il | 200,000 | 5 | 69.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7036-il | 500,000 | 9 | 97.1 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7036-il | 500,000 | 5 | 88.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7036-il | 1,000,000 | 9 | 114 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7036-il | 1,000,000 | 5 | 103.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20610-il | 50,000 | 9 | 23.7 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20610-il | 50,000 | 5 | 24.6 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20610-il | 100,000 | 9 | 31.7 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20610-il | 100,000 | 5 | 31.8 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20610-il | 200,000 | 9 | 41.9 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20610-il | 200,000 | 5 | 43.1 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20610-il | 500,000 | 9 | 64.9 at α=0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20610-il | 500,000 | 5 | 62.7 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20610-il | 1,000,000 | 9 | 74.3 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20610-il | 1,000,000 | 5 | 77.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7062-il | 50,000 | 9 | 12.1 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7062-il | 50,000 | 5 | 32.1 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7062-il | 100,000 | 9 | 47.6 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7062-il | 100,000 | 5 | 52.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7062-il | 200,000 | 9 | 70 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7062-il | 200,000 | 5 | 70.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7062-il | 500,000 | 9 | 99.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7062-il | 500,000 | 5 | 94.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7062-il | 1,000,000 | 9 | 121.5 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7062-il | 1,000,000 | 5 | 113.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6043-il | 50,000 | 9 | 39.7 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6043-il | 50,000 | 5 | 37.9 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6043-il | 100,000 | 9 | 66.5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6043-il | 100,000 | 5 | 65.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6043-il | 200,000 | 9 | 98 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6043-il | 200,000 | 5 | 94.7 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6043-il | 500,000 | 9 | 143 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6043-il | 500,000 | 5 | 129.8 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6043-il | 1,000,000 | 9 | 175.2 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6043-il | 1,000,000 | 5 | 145.2 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6041-il | 50,000 | 9 | 35.4 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6041-il | 50,000 | 5 | 35.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6041-il | 100,000 | 9 | 53.5 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6041-il | 100,000 | 5 | 49.8 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6041-il | 200,000 | 9 | 72.8 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6041-il | 200,000 | 5 | 63.9 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6041-il | 500,000 | 9 | 91.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6041-il | 500,000 | 5 | 74.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sg6041-il | 1,000,000 | 9 | 96.5 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sg6041-il | 1,000,000 | 5 | 88 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7034-il | 50,000 | 9 | 27.8 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7034-il | 50,000 | 5 | 37.4 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7034-il | 100,000 | 9 | 54.3 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7034-il | 100,000 | 5 | 57.6 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7034-il | 200,000 | 9 | 77.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7034-il | 200,000 | 5 | 76.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7034-il | 500,000 | 9 | 107.4 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7034-il | 500,000 | 5 | 99.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7034-il | 1,000,000 | 9 | 128.4 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7034-il | 1,000,000 | 5 | 116.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4053-il | 50,000 | 9 | 38.2 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4053-il | 50,000 | 5 | 39.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4053-il | 100,000 | 9 | 58.9 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4053-il | 100,000 | 5 | 57.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4053-il | 200,000 | 9 | 80.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4053-il | 200,000 | 5 | 75.6 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4053-il | 500,000 | 9 | 109.1 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4053-il | 500,000 | 5 | 96.5 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4053-il | 1,000,000 | 9 | 129 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4053-il | 1,000,000 | 5 | 109.6 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4095-il | 50,000 | 9 | 27.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4095-il | 50,000 | 5 | 32.8 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4095-il | 100,000 | 9 | 41.1 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4095-il | 100,000 | 5 | 43.5 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4095-il | 200,000 | 9 | 53.4 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4095-il | 200,000 | 5 | 53.5 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4095-il | 500,000 | 9 | 67.2 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4095-il | 500,000 | 5 | 65.2 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4095-il | 1,000,000 | 9 | 75.6 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4095-il | 1,000,000 | 5 | 72.5 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s3016-il | 50,000 | 9 | 31.8 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s3016-il | 50,000 | 5 | 34.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s3016-il | 100,000 | 9 | 49.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s3016-il | 100,000 | 5 | 48.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s3016-il | 200,000 | 9 | 65.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s3016-il | 200,000 | 5 | 61 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s3016-il | 500,000 | 9 | 85.5 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s3016-il | 500,000 | 5 | 78.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s3016-il | 1,000,000 | 9 | 99.1 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s3016-il | 1,000,000 | 5 | 93.3 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s806a-nr | 50,000 | 9 | 34.4 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s806a-nr | 100,000 | 9 | 53.3 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s806a-nr | 200,000 | 9 | 76.1 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s806a-nr | 500,000 | 9 | 107.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s806a-nr | 1,000,000 | 9 | 119.2 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s3010-il | 50,000 | 9 | 28.5 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s3010-il | 50,000 | 5 | 36.2 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s3010-il | 100,000 | 9 | 50.2 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s3010-il | 100,000 | 5 | 52.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s3010-il | 200,000 | 9 | 70 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s3010-il | 200,000 | 5 | 68.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s3010-il | 500,000 | 9 | 95.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s3010-il | 500,000 | 5 | 89.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s3010-il | 1,000,000 | 9 | 113.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s3010-il | 1,000,000 | 5 | 104.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20412-il | 50,000 | 9 | 24.4 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20412-il | 50,000 | 5 | 21.8 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20412-il | 100,000 | 9 | 26.7 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20412-il | 100,000 | 5 | 30.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20412-il | 200,000 | 9 | 35.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20412-il | 200,000 | 5 | 43 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20412-il | 500,000 | 9 | 56.7 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20412-il | 500,000 | 5 | 63 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20412-il | 1,000,000 | 9 | 75.8 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20412-il | 1,000,000 | 5 | 78.2 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20706-il | 50,000 | 9 | 24 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20706-il | 50,000 | 5 | 25.3 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20706-il | 100,000 | 9 | 38.2 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20706-il | 100,000 | 5 | 33.3 at α=1.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20706-il | 200,000 | 9 | 40.6 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20706-il | 200,000 | 5 | 44.1 at α=0.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20706-il | 500,000 | 9 | 67 at α=0.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20706-il | 500,000 | 5 | 55.8 at α=-0.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20706-il | 1,000,000 | 9 | 96.6 at α=-0.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20706-il | 1,000,000 | 5 | 68 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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