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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(ls421mod-il) NASA/LANGLEY LS(1)-0421MOD AIRFOIL | NASA/Langley LS(1)-0421MOD general aviation airfoil Max thickness 21% at 32.5% chord Max camber 2.3% at 30% chord | Remove Airfoil details Airfoil plotter |
(e559-il) EPPLER 559 AIRFOIL | Eppler E559 general aviation airfoil Max thickness 16% at 27.2% chord Max camber 4.3% at 50.2% chord | Remove Airfoil details Airfoil plotter |
(df101-il) DF 101 AIRFOIL | David Fraser DF 101 low Reynolds number airfoil Max thickness 11% at 29.1% chord Max camber 2.3% at 43.5% chord | Remove Airfoil details Airfoil plotter |
(s2048-il) S2048 | Selig S2048 low Reynolds number airfoil Max thickness 8.6% at 35.4% chord Max camber 1.7% at 60.1% chord | Remove Airfoil details Airfoil plotter |
(s2060-il) S2060 8% | Selig S2060 low Reynolds number airfoil Max thickness 8% at 30.2% chord Max camber 1.6% at 49.7% 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 |
(curtisc72-il) Curtis C-72 | Curtis C-72 airfoil Max thickness 11.7% at 30% chord Max camber 3.8% at 50% chord | Remove Airfoil details Airfoil plotter |
(e180-il) E180 (8.59%) | Eppler E180 low Reynolds number airfoil Max thickness 8.6% at 33.5% chord Max camber 2% at 38.1% chord | Remove Airfoil details Airfoil plotter |
(b707d-il) BOEING 707 .54 SPAN AIRFOIL | Boeing Commercial Airplane Company model 707 airfoils Max thickness 9% at 40% chord Max camber 1.8% at 30% chord | Remove Airfoil details Airfoil plotter |
(goe403-il) GOE 403 AIRFOIL | Gottingen 403 airfoil Max thickness 6.7% at 29.9% chord Max camber 4.3% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(daytonwright6-il) Dayton-Wright 6 | Dayton-Wright 6 airfoil Max thickness 13.6% at 30% chord Max camber 4.9% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe574-il) GOE 574 AIRFOIL | Gottingen 574 airfoil Max thickness 10.3% at 30% chord Max camber 4.9% at 40% chord | Remove Airfoil details Airfoil plotter |
(sd6080-il) SD6080 (9.2%) | Selig/Donovan SD6080 low Reynolds number airfoil Max thickness 9.2% at 30.9% chord Max camber 3.2% at 44.7% chord | Remove Airfoil details Airfoil plotter |
(e387-il) E387 | Eppler E387 low Reynolds number airfoil Max thickness 9.1% at 31.1% chord Max camber 3.2% at 44.8% chord | Remove Airfoil details Airfoil plotter |
(goe491-il) GOE 491 AIRFOIL | Gottingen 491 airfoil Max thickness 4.9% at 20% chord Max camber 2.9% at 30% chord | Remove Airfoil details Airfoil plotter |
(s6061-il) S6061 9% | Selig S6061 low Reynolds number airfoil Max thickness 9% at 34% chord Max camber 1.5% at 43.6% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (ls421mod-il,e559-il,df101-il,s2048-il,s2060-il,goe433-il,curtisc72-il,e180-il,b707d-il,goe403-il,daytonwright6-il,goe574-il,sd6080-il,e387-il,goe491-il,s6061-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ls421mod-il | 50,000 | 9 | 7.2 at α=0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ls421mod-il | 50,000 | 5 | 18.6 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ls421mod-il | 100,000 | 9 | 37.2 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ls421mod-il | 100,000 | 5 | 38.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ls421mod-il | 200,000 | 9 | 51.9 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ls421mod-il | 200,000 | 5 | 56 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ls421mod-il | 500,000 | 9 | 80.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ls421mod-il | 500,000 | 5 | 77.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ls421mod-il | 1,000,000 | 9 | 100 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ls421mod-il | 1,000,000 | 5 | 90.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e559-il | 50,000 | 9 | 8.8 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e559-il | 50,000 | 5 | 30.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e559-il | 100,000 | 9 | 43.7 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e559-il | 100,000 | 5 | 52.9 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e559-il | 200,000 | 9 | 70.4 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e559-il | 200,000 | 5 | 73.2 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e559-il | 500,000 | 9 | 103.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e559-il | 500,000 | 5 | 101.9 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e559-il | 1,000,000 | 9 | 130.6 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e559-il | 1,000,000 | 5 | 123.6 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| df101-il | 50,000 | 9 | 31.5 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| df101-il | 50,000 | 5 | 34.8 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| df101-il | 100,000 | 9 | 50.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| df101-il | 100,000 | 5 | 49.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| df101-il | 200,000 | 9 | 68.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| df101-il | 200,000 | 5 | 63 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| df101-il | 500,000 | 9 | 90.9 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| df101-il | 500,000 | 5 | 80.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| df101-il | 1,000,000 | 9 | 104.4 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| df101-il | 1,000,000 | 5 | 96.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2048-il | 50,000 | 9 | 37.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2048-il | 50,000 | 5 | 37.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2048-il | 100,000 | 9 | 55.8 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2048-il | 100,000 | 5 | 52.7 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2048-il | 200,000 | 9 | 75.8 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2048-il | 200,000 | 5 | 67.5 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2048-il | 500,000 | 9 | 100.7 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2048-il | 500,000 | 5 | 78.1 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2048-il | 1,000,000 | 9 | 110.3 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2048-il | 1,000,000 | 5 | 88.5 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2060-il | 50,000 | 9 | 36.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2060-il | 50,000 | 5 | 36.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2060-il | 100,000 | 9 | 53.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2060-il | 100,000 | 5 | 50.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2060-il | 200,000 | 9 | 70.9 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2060-il | 200,000 | 5 | 62.9 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2060-il | 500,000 | 9 | 91 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2060-il | 500,000 | 5 | 75.1 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s2060-il | 1,000,000 | 9 | 101.5 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s2060-il | 1,000,000 | 5 | 79 at α=3.25° | 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 | |
| curtisc72-il | 50,000 | 9 | 29.9 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| curtisc72-il | 50,000 | 5 | 37.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| curtisc72-il | 100,000 | 9 | 54.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| curtisc72-il | 100,000 | 5 | 56.5 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| curtisc72-il | 200,000 | 9 | 76.3 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| curtisc72-il | 200,000 | 5 | 73.3 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| curtisc72-il | 500,000 | 9 | 103.4 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| curtisc72-il | 500,000 | 5 | 95.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| curtisc72-il | 1,000,000 | 9 | 121 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| curtisc72-il | 1,000,000 | 5 | 114.4 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e180-il | 50,000 | 9 | 35.5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e180-il | 50,000 | 5 | 36.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e180-il | 100,000 | 9 | 52.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e180-il | 100,000 | 5 | 51.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e180-il | 200,000 | 9 | 71 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e180-il | 200,000 | 5 | 66 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e180-il | 500,000 | 9 | 93.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e180-il | 500,000 | 5 | 82.3 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e180-il | 1,000,000 | 9 | 109.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e180-il | 1,000,000 | 5 | 91.7 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| b707d-il | 50,000 | 9 | 36.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| b707d-il | 50,000 | 5 | 35.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| b707d-il | 100,000 | 9 | 53.9 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| b707d-il | 100,000 | 5 | 47.8 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| b707d-il | 200,000 | 9 | 70.3 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| b707d-il | 200,000 | 5 | 52.3 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| b707d-il | 500,000 | 9 | 80.1 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| b707d-il | 500,000 | 5 | 62.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| b707d-il | 1,000,000 | 9 | 75.9 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| b707d-il | 1,000,000 | 5 | 76.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe403-il | 50,000 | 9 | 42.6 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe403-il | 50,000 | 5 | 41.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe403-il | 100,000 | 9 | 59.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe403-il | 100,000 | 5 | 57.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe403-il | 200,000 | 9 | 75.8 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe403-il | 200,000 | 5 | 73 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe403-il | 500,000 | 9 | 98.6 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe403-il | 500,000 | 5 | 92.9 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe403-il | 1,000,000 | 9 | 116.1 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe403-il | 1,000,000 | 5 | 107.9 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| daytonwright6-il | 50,000 | 9 | 11 at α=1° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| daytonwright6-il | 50,000 | 5 | 31.1 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| daytonwright6-il | 100,000 | 9 | 45.6 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| daytonwright6-il | 100,000 | 5 | 49.7 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| daytonwright6-il | 200,000 | 9 | 66.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| daytonwright6-il | 200,000 | 5 | 66.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| daytonwright6-il | 500,000 | 9 | 92.6 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| daytonwright6-il | 500,000 | 5 | 89.6 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| daytonwright6-il | 1,000,000 | 9 | 115.8 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| daytonwright6-il | 1,000,000 | 5 | 111.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe574-il | 50,000 | 9 | 34.4 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe574-il | 50,000 | 5 | 35.7 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe574-il | 100,000 | 9 | 56 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe574-il | 100,000 | 5 | 55.8 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe574-il | 200,000 | 9 | 74.5 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe574-il | 200,000 | 5 | 73.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe574-il | 500,000 | 9 | 100 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe574-il | 500,000 | 5 | 97.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe574-il | 1,000,000 | 9 | 121.8 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe574-il | 1,000,000 | 5 | 118.1 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd6080-il | 50,000 | 9 | 36.1 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd6080-il | 50,000 | 5 | 39.6 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd6080-il | 100,000 | 9 | 59.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd6080-il | 100,000 | 5 | 60.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd6080-il | 200,000 | 9 | 83.6 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd6080-il | 200,000 | 5 | 80.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd6080-il | 500,000 | 9 | 115.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd6080-il | 500,000 | 5 | 104.4 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd6080-il | 1,000,000 | 9 | 137.4 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd6080-il | 1,000,000 | 5 | 119.7 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e387-il | 50,000 | 9 | 38.1 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e387-il | 50,000 | 5 | 38.7 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e387-il | 100,000 | 9 | 60.7 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e387-il | 100,000 | 5 | 60.9 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e387-il | 200,000 | 9 | 84.4 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e387-il | 200,000 | 5 | 82.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e387-il | 500,000 | 9 | 116.3 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e387-il | 500,000 | 5 | 109.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e387-il | 1,000,000 | 9 | 140.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e387-il | 1,000,000 | 5 | 127.5 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe491-il | 50,000 | 9 | 34.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe491-il | 50,000 | 5 | 37.1 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe491-il | 100,000 | 9 | 48.9 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe491-il | 100,000 | 5 | 50.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe491-il | 200,000 | 9 | 62.8 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe491-il | 200,000 | 5 | 62 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe491-il | 500,000 | 9 | 92.3 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe491-il | 500,000 | 5 | 73.2 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe491-il | 1,000,000 | 9 | 88 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe491-il | 1,000,000 | 5 | 86.8 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s6061-il | 50,000 | 9 | 34.1 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s6061-il | 50,000 | 5 | 35.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s6061-il | 100,000 | 9 | 51.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s6061-il | 100,000 | 5 | 50.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s6061-il | 200,000 | 9 | 68.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s6061-il | 200,000 | 5 | 63.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s6061-il | 500,000 | 9 | 88.8 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s6061-il | 500,000 | 5 | 77.3 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s6061-il | 1,000,000 | 9 | 102 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s6061-il | 1,000,000 | 5 | 81.7 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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