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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(sd8040-il) SD8040 (10%) | Selig/Donovan SD8040 low Reynolds number airfoil Max thickness 10% at 29.7% chord Max camber 2.1% at 44% chord | Remove Airfoil details Airfoil plotter |
(goe15k-il) GOE 15K AIRFOIL | Gottingen 15K airfoil Max thickness 15% at 50% chord Max camber 3.4% at 50% chord | Remove Airfoil details Airfoil plotter |
(s2062-il) S2062 8% | Selig S2062 low Reynolds number airfoil Max thickness 8% at 30.1% chord Max camber 1.5% at 49.6% chord | Remove Airfoil details Airfoil plotter |
(mh38-il) MH 38 9.68% | Martin Hepperle MH 38 for Endurance Model Max thickness 9.7% at 31.6% chord Max camber 3.9% at 45.3% chord | Remove Airfoil details Airfoil plotter |
(ah79k135-il) AH 79-K-135/20 B | Althaus AH 79-K-135/20 airfoil for use with flaps (K) Max thickness 13.5% at 40.2% chord Max camber 3.1% at 40.2% chord | Remove Airfoil details Airfoil plotter |
(goe632-il) GOE 632 AIRFOIL | Gottingen 632 airfoil Max thickness 14% at 30% chord Max camber 3.9% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe532-il) GOE 532 AIRFOIL | Gottingen 532 airfoil Max thickness 12.5% at 30% chord Max camber 4.8% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe404-il) GOE 404 AIRFOIL | Gottingen 404 airfoil Max thickness 13.2% at 29.6% chord Max camber 5% at 29.6% chord | Remove Airfoil details Airfoil plotter |
(e485-il) EPPLER 485 AIRFOIL | Eppler E485 tailplane airfoil Max thickness 12.5% at 31.8% chord Max camber 1.1% at 27.1% chord | Remove Airfoil details Airfoil plotter |
(e421-il) EPPLER 421 AIRFOIL | Eppler E421 high lift airfoil Max thickness 14.5% at 26% chord Max camber 8.6% at 37.4% chord | Remove Airfoil details Airfoil plotter |
(fx69pr281-il) FX 69-PR-281 | Wortmann FX 69-PR-281 airfoil Max thickness 28.1% at 22.2% chord Max camber 5.6% at 50% chord | Remove Airfoil details Airfoil plotter |
(goe624-il) GOE 624 AIRFOIL | Gottingen 624 airfoil Max thickness 16% at 30% chord Max camber 5.2% at 40% chord | Remove Airfoil details Airfoil plotter |
(amsoil1-il) RUTAN CANARD AIRFOIL | Rutan AMSOIL racer canard airfoil Max thickness 11.6% at 39% chord Max camber 2.1% at 42% chord | Remove Airfoil details Airfoil plotter |
(e656-il) EPPLER 656 AIRFOIL | Eppler E656 sailplane airfoil Max thickness 16.2% at 37% chord Max camber 4.8% at 42.2% chord | Remove Airfoil details Airfoil plotter |
(goe433-il) GOE 433 AIRFOIL | Gottingen 433 airfoil Max thickness 17.4% at 29.2% chord Max camber 4.8% at 49.2% chord | Remove Airfoil details Airfoil plotter |
(fx78k140a20-il) FX 78-K-140 A/20 | Wortmann FX 78-K-140 airfoil for use with flaps (K) A/20 Max thickness 14.1% at 43.5% chord Max camber 4.4% at 43.5% chord | Remove Airfoil details Airfoil plotter |
(e417-il) EPPLER 417 AIRFOIL | Eppler E417 general purpose airfoil Max thickness 14.2% at 38.3% chord Max camber 3.1% at 76.3% chord | Remove Airfoil details Airfoil plotter |
(s4022-il) S4022 | Selig S4022 low Reynolds number airfoil Max thickness 11.3% at 34.1% chord Max camber 4.3% at 57.8% chord | Remove Airfoil details Airfoil plotter |
(goe16k-il) GOE 16K AIRFOIL | Gottingen 16K airfoil Max thickness 18.2% at 50% chord Max camber 4.1% at 50% chord | Remove Airfoil details Airfoil plotter |
(usa35a-il) USA 35 A AIRFOIL | USA-35A airfoil Max thickness 18.2% at 29.4% chord Max camber 6.4% at 39.4% chord | Remove Airfoil details Airfoil plotter |
(e855-il) EPPLER 855 AIRFOIL | Eppler E855 propeller airfoil Max thickness 15.7% at 32.2% chord Max camber 3.7% at 50.6% chord | Remove Airfoil details Airfoil plotter |
(naca65210-il) NACA 65-210 | NACA 65-210 airfoil Max thickness 10% at 40% chord Max camber 1.1% at 50% chord | Remove Airfoil details Airfoil plotter |
(goe210-il) GOE 210 (DAIMLER) AIRFOIL | Gottingen 210 (DAIMLER) airfoil Max thickness 6.6% at 30% chord Max camber 4.3% at 40% chord | Remove Airfoil details Airfoil plotter |
(e431-il) EPPLER 431 AIRFOIL | Eppler E431 sailplane airfoil Max thickness 15.1% at 37.4% chord Max camber 4.2% at 42.6% 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 |
(e603-il) EPPLER 603 AIRFOIL | Eppler E603 general purpose airfoil Max thickness 19% at 40% chord Max camber 3.6% at 35.6% chord | Remove Airfoil details Airfoil plotter |
(s2091-il) S2091-101-83 | Selig S2091 low Reynolds number airfoil Max thickness 10.1% at 26% chord Max camber 3.7% at 39.5% chord | Remove Airfoil details Airfoil plotter |
(goe409-il) GOE 409 AIRFOIL | Gottingen 409 airfoil Max thickness 12.7% at 30% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (sd8040-il,goe15k-il,s2062-il,mh38-il,ah79k135-il,goe632-il,goe532-il,goe404-il,e485-il,e421-il,fx69pr281-il,goe624-il,amsoil1-il,e656-il,goe433-il,fx78k140a20-il,e417-il,s4022-il,goe16k-il,usa35a-il,e855-il,naca65210-il,goe210-il,e431-il,s806a-nr,e603-il,s2091-il,goe409-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| sd8040-il | 50,000 | 9 | 32.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd8040-il | 50,000 | 5 | 36.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd8040-il | 100,000 | 9 | 51.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd8040-il | 100,000 | 5 | 51.7 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd8040-il | 200,000 | 9 | 69.2 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd8040-il | 200,000 | 5 | 65.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd8040-il | 500,000 | 9 | 91.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd8040-il | 500,000 | 5 | 84.7 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd8040-il | 1,000,000 | 9 | 107.7 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd8040-il | 1,000,000 | 5 | 99 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe15k-il | 50,000 | 9 | 23.7 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe15k-il | 50,000 | 5 | 20.8 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe15k-il | 100,000 | 9 | 32.5 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe15k-il | 100,000 | 5 | 30.7 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe15k-il | 200,000 | 9 | 49.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe15k-il | 200,000 | 5 | 49.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe15k-il | 500,000 | 9 | 92.8 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe15k-il | 500,000 | 5 | 67.7 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe15k-il | 1,000,000 | 9 | 92.4 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe15k-il | 1,000,000 | 5 | 83.1 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2062-il | 50,000 | 9 | 36 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2062-il | 50,000 | 5 | 36.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2062-il | 100,000 | 9 | 52.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2062-il | 100,000 | 5 | 49.9 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2062-il | 200,000 | 9 | 69.7 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2062-il | 200,000 | 5 | 61.8 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2062-il | 500,000 | 9 | 89.3 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2062-il | 500,000 | 5 | 74.6 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2062-il | 1,000,000 | 9 | 99.7 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2062-il | 1,000,000 | 5 | 78.9 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh38-il | 50,000 | 9 | 37.7 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh38-il | 50,000 | 5 | 37.8 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh38-il | 100,000 | 9 | 61.4 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh38-il | 100,000 | 5 | 61.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh38-il | 200,000 | 9 | 86.8 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh38-il | 200,000 | 5 | 85.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh38-il | 500,000 | 9 | 122.7 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh38-il | 500,000 | 5 | 114.5 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| mh38-il | 1,000,000 | 9 | 149.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| mh38-il | 1,000,000 | 5 | 133.9 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah79k135-il | 50,000 | 9 | 24 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah79k135-il | 50,000 | 5 | 24.3 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah79k135-il | 100,000 | 9 | 48 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah79k135-il | 100,000 | 5 | 46.3 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah79k135-il | 200,000 | 9 | 78.9 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah79k135-il | 200,000 | 5 | 74.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah79k135-il | 500,000 | 9 | 104.3 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah79k135-il | 500,000 | 5 | 95 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah79k135-il | 1,000,000 | 9 | 122.7 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah79k135-il | 1,000,000 | 5 | 111.7 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe632-il | 50,000 | 9 | 7.4 at α=12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe632-il | 50,000 | 5 | 26 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe632-il | 100,000 | 9 | 48.5 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe632-il | 100,000 | 5 | 51.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe632-il | 200,000 | 9 | 72.3 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe632-il | 200,000 | 5 | 69.6 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe632-il | 500,000 | 9 | 98.8 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe632-il | 500,000 | 5 | 81.6 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe632-il | 1,000,000 | 9 | 104.1 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe632-il | 1,000,000 | 5 | 88.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe532-il | 50,000 | 9 | 17.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe532-il | 50,000 | 5 | 34.7 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe532-il | 100,000 | 9 | 53.3 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe532-il | 100,000 | 5 | 56 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe532-il | 200,000 | 9 | 76.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe532-il | 200,000 | 5 | 73.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe532-il | 500,000 | 9 | 101.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe532-il | 500,000 | 5 | 89.7 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe532-il | 1,000,000 | 9 | 115.7 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe532-il | 1,000,000 | 5 | 102.7 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe404-il | 50,000 | 9 | 15.2 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe404-il | 50,000 | 5 | 31.6 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe404-il | 100,000 | 9 | 45.2 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe404-il | 100,000 | 5 | 50.8 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe404-il | 200,000 | 9 | 68.8 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe404-il | 200,000 | 5 | 69.7 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe404-il | 500,000 | 9 | 98.8 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe404-il | 500,000 | 5 | 94.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe404-il | 1,000,000 | 9 | 121.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe404-il | 1,000,000 | 5 | 110.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e485-il | 50,000 | 9 | 27.4 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e485-il | 50,000 | 5 | 30.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e485-il | 100,000 | 9 | 44.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e485-il | 100,000 | 5 | 44.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e485-il | 200,000 | 9 | 59.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e485-il | 200,000 | 5 | 55.2 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e485-il | 500,000 | 9 | 73.8 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e485-il | 500,000 | 5 | 69 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e485-il | 1,000,000 | 9 | 86.2 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e485-il | 1,000,000 | 5 | 81.9 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e421-il | 50,000 | 9 | 5.3 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e421-il | 50,000 | 5 | 20 at α=0.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e421-il | 100,000 | 9 | 27.7 at α=1° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e421-il | 100,000 | 5 | 48 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e421-il | 200,000 | 9 | 63 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e421-il | 200,000 | 5 | 74.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e421-il | 500,000 | 9 | 107.4 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e421-il | 500,000 | 5 | 109.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e421-il | 1,000,000 | 9 | 141.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e421-il | 1,000,000 | 5 | 141.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx69pr281-il | 50,000 | 9 | 3.4 at α=-5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx69pr281-il | 50,000 | 5 | 6.4 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx69pr281-il | 100,000 | 9 | 21.5 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx69pr281-il | 100,000 | 5 | 26.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx69pr281-il | 200,000 | 9 | 41.1 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx69pr281-il | 200,000 | 5 | 35 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx69pr281-il | 500,000 | 9 | 49.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx69pr281-il | 500,000 | 5 | 47.1 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx69pr281-il | 1,000,000 | 9 | 64.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx69pr281-il | 1,000,000 | 5 | 61.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe624-il | 50,000 | 9 | 5.9 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe624-il | 50,000 | 5 | 22.8 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe624-il | 100,000 | 9 | 39.8 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe624-il | 100,000 | 5 | 50.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe624-il | 200,000 | 9 | 69.1 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe624-il | 200,000 | 5 | 69.9 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe624-il | 500,000 | 9 | 99.5 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe624-il | 500,000 | 5 | 97.6 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe624-il | 1,000,000 | 9 | 126.9 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe624-il | 1,000,000 | 5 | 120.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| amsoil1-il | 50,000 | 9 | 33 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| amsoil1-il | 50,000 | 5 | 31.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| amsoil1-il | 100,000 | 9 | 48.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| amsoil1-il | 100,000 | 5 | 46.8 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| amsoil1-il | 200,000 | 9 | 67.5 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| amsoil1-il | 200,000 | 5 | 59.9 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| amsoil1-il | 500,000 | 9 | 86.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| amsoil1-il | 500,000 | 5 | 68.1 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| amsoil1-il | 1,000,000 | 9 | 93 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| amsoil1-il | 1,000,000 | 5 | 81.1 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e656-il | 50,000 | 9 | 5.7 at α=12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e656-il | 50,000 | 5 | 14.6 at α=13.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e656-il | 100,000 | 9 | 34.7 at α=12.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e656-il | 100,000 | 5 | 29.8 at α=11.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e656-il | 200,000 | 9 | 69.1 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e656-il | 200,000 | 5 | 70.6 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e656-il | 500,000 | 9 | 125.4 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e656-il | 500,000 | 5 | 118.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e656-il | 1,000,000 | 9 | 161.3 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e656-il | 1,000,000 | 5 | 147.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe433-il | 50,000 | 9 | 5.7 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe433-il | 50,000 | 5 | 22.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe433-il | 100,000 | 9 | 48.2 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe433-il | 100,000 | 5 | 53.1 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe433-il | 200,000 | 9 | 75.9 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe433-il | 200,000 | 5 | 71.9 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe433-il | 500,000 | 9 | 102.7 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe433-il | 500,000 | 5 | 89 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe433-il | 1,000,000 | 9 | 115.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe433-il | 1,000,000 | 5 | 100.3 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx78k140a20-il | 50,000 | 9 | 16.8 at α=13° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx78k140a20-il | 50,000 | 5 | 15.8 at α=11.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx78k140a20-il | 100,000 | 9 | 25.4 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx78k140a20-il | 100,000 | 5 | 27.8 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx78k140a20-il | 200,000 | 9 | 54.6 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx78k140a20-il | 200,000 | 5 | 57.5 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx78k140a20-il | 500,000 | 9 | 118.9 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx78k140a20-il | 500,000 | 5 | 111.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx78k140a20-il | 1,000,000 | 9 | 147.4 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx78k140a20-il | 1,000,000 | 5 | 142.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e417-il | 50,000 | 9 | 33.2 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e417-il | 50,000 | 5 | 30.2 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e417-il | 100,000 | 9 | 46.8 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e417-il | 100,000 | 5 | 46 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e417-il | 200,000 | 9 | 65.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e417-il | 200,000 | 5 | 66.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e417-il | 500,000 | 9 | 103.1 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e417-il | 500,000 | 5 | 94.4 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e417-il | 1,000,000 | 9 | 135.9 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e417-il | 1,000,000 | 5 | 112.5 at α=1° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4022-il | 50,000 | 9 | 39.4 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4022-il | 50,000 | 5 | 39.1 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4022-il | 100,000 | 9 | 64.7 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4022-il | 100,000 | 5 | 65.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4022-il | 200,000 | 9 | 93.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4022-il | 200,000 | 5 | 90.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4022-il | 500,000 | 9 | 129.8 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4022-il | 500,000 | 5 | 113.5 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s4022-il | 1,000,000 | 9 | 148.3 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s4022-il | 1,000,000 | 5 | 128.1 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe16k-il | 50,000 | 9 | 21.5 at α=11.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe16k-il | 50,000 | 5 | 16.6 at α=11.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe16k-il | 100,000 | 9 | 26.4 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe16k-il | 100,000 | 5 | 23.7 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe16k-il | 200,000 | 9 | 35.9 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe16k-il | 500,000 | 9 | 69.2 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe16k-il | 500,000 | 5 | 50.6 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe16k-il | 1,000,000 | 9 | 80.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe16k-il | 1,000,000 | 5 | 70.9 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa35a-il | 50,000 | 9 | 4.3 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa35a-il | 50,000 | 5 | 20.4 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa35a-il | 100,000 | 9 | 35.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa35a-il | 100,000 | 5 | 46.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa35a-il | 200,000 | 9 | 66.5 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa35a-il | 200,000 | 5 | 67.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa35a-il | 500,000 | 9 | 97.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa35a-il | 500,000 | 5 | 92.3 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| usa35a-il | 1,000,000 | 9 | 122.3 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| usa35a-il | 1,000,000 | 5 | 109.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e855-il | 50,000 | 9 | 5.7 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e855-il | 50,000 | 5 | 23 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e855-il | 100,000 | 9 | 47 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e855-il | 100,000 | 5 | 52.9 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e855-il | 200,000 | 9 | 76.4 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e855-il | 200,000 | 5 | 77.4 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e855-il | 500,000 | 9 | 112 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e855-il | 500,000 | 5 | 106.9 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e855-il | 1,000,000 | 9 | 140.5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e855-il | 1,000,000 | 5 | 122.6 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca65210-il | 50,000 | 9 | 24.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca65210-il | 50,000 | 5 | 29.7 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca65210-il | 100,000 | 9 | 43.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca65210-il | 100,000 | 5 | 43 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca65210-il | 200,000 | 9 | 59 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca65210-il | 200,000 | 5 | 50.8 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca65210-il | 500,000 | 9 | 72.9 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca65210-il | 500,000 | 5 | 62.7 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| naca65210-il | 1,000,000 | 9 | 82.6 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| naca65210-il | 1,000,000 | 5 | 69.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe210-il | 50,000 | 9 | 40.7 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe210-il | 50,000 | 5 | 43.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe210-il | 100,000 | 9 | 62 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe210-il | 100,000 | 5 | 62 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe210-il | 200,000 | 9 | 82.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe210-il | 200,000 | 5 | 77.9 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe210-il | 500,000 | 9 | 105.1 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe210-il | 500,000 | 5 | 86.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe210-il | 1,000,000 | 9 | 116.7 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe210-il | 1,000,000 | 5 | 99.8 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e431-il | 50,000 | 9 | 22.1 at α=13.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e431-il | 50,000 | 5 | 19.8 at α=12° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e431-il | 100,000 | 9 | 48.3 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e431-il | 100,000 | 5 | 46.2 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e431-il | 200,000 | 9 | 79.8 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e431-il | 200,000 | 5 | 76.8 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e431-il | 500,000 | 9 | 116 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e431-il | 500,000 | 5 | 109.2 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e431-il | 1,000,000 | 9 | 144.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e431-il | 1,000,000 | 5 | 130.2 at α=4° | 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 | |
| e603-il | 50,000 | 9 | 4 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e603-il | 50,000 | 5 | 10.2 at α=15.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e603-il | 100,000 | 9 | 26.6 at α=14° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e603-il | 100,000 | 5 | 22.6 at α=12° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e603-il | 200,000 | 9 | 56.5 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e603-il | 200,000 | 5 | 63 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e603-il | 500,000 | 9 | 103.6 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e603-il | 500,000 | 5 | 103.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e603-il | 1,000,000 | 9 | 136.9 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e603-il | 1,000,000 | 5 | 127.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2091-il | 50,000 | 9 | 28.9 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2091-il | 50,000 | 5 | 38.2 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2091-il | 100,000 | 9 | 54.7 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2091-il | 100,000 | 5 | 57.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2091-il | 200,000 | 9 | 77.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2091-il | 200,000 | 5 | 76.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2091-il | 500,000 | 9 | 107.4 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2091-il | 500,000 | 5 | 99.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2091-il | 1,000,000 | 9 | 128.2 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2091-il | 1,000,000 | 5 | 116.2 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe409-il | 50,000 | 9 | 28.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe409-il | 50,000 | 5 | 26.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe409-il | 100,000 | 9 | 38.6 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe409-il | 100,000 | 5 | 32.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe409-il | 200,000 | 9 | 40.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe409-il | 200,000 | 5 | 37.7 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe409-il | 500,000 | 9 | 46.5 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe409-il | 500,000 | 5 | 50.7 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe409-il | 1,000,000 | 9 | 64.2 at α=13° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe409-il | 1,000,000 | 5 | 70.5 at α=11.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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