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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(goe374-il) GOE 374 AIRFOIL | Gottingen 374 airfoil Max thickness 6.5% at 30% chord Max camber 4.5% at 30% chord | Remove Airfoil details Airfoil plotter |
(sc20410-il) NASA SC(2)-0410 AIRFOIL | NASA SC(2)-0410 airfoil (NASA TP-2969) Max thickness 10% at 38% chord Max camber 1.1% at 85% chord | Remove Airfoil details Airfoil plotter |
(s9033-il) S9033 (7.5%) | Selig S9033 (7.5%) symmetrical vertical stab airfoil used on the Blackhawk R/C sailplane Max thickness 7.5% at 22.8% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(s805a-nr) NREL's S805A Airfoil | NREL HAWT airfoil S805A primary Max thickness 13.5% at 40% chord Max camber 2.1% at 35% chord | Remove Airfoil details Airfoil plotter |
(e837-il) EPPLER E837 HYDROFOIL AIRFOIL | Eppler E837 hydrofoil Max thickness 16.1% at 36.9% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(sc20403-il) NASA SC(2)-0403 AIRFOIL | NASA SC(2)-0403 airfoil (NASA TP-2969) Max thickness 3% at 36% chord Max camber 0.6% at 85% chord | Remove Airfoil details Airfoil plotter |
(rg12-il) RG-12 | Rolf Girsberger RG 12 airfoil Max thickness 9.3% at 34.4% chord Max camber 1.4% at 34.4% chord | Remove Airfoil details Airfoil plotter |
(s9037-il) S9037 (9%) | Selig S9037 (9%) low Reynolds number airfoil used on the Opus R/C sailplane Max thickness 9% at 28.5% chord Max camber 3.3% at 42.4% chord | Remove Airfoil details Airfoil plotter |
(hq308-il) HQ 3.0/8 AIRFOIL | Quabeck HQ 3.0/8 R/C sailplane airfoil Max thickness 8% at 35% chord Max camber 3% at 50% chord | Remove Airfoil details Airfoil plotter |
(sc20518-il) NASA SC(2)-0518 AIRFOIL | NASA SC(2)-0518 airfoil (NASA TP-2969) Max thickness 18% at 35% chord Max camber 1.9% at 82% chord | Remove Airfoil details Airfoil plotter |
(goe566-il) GOE 566 AIRFOIL | Gottingen 566 airfoil Max thickness 8.7% at 30% chord Max camber 2.6% at 40% chord | Remove Airfoil details Airfoil plotter |
(sd7037-il) SD7037-092-88 | Selig/Donovan SD7037 low Reynolds number airfoil Max thickness 9.2% at 26.1% chord Max camber 2.5% at 44.7% chord | Remove Airfoil details Airfoil plotter |
(fx711520-il) FX 71-L-150/20 AIRFOIL | Wortmann FX 71-L-150/20 airfoil Max thickness 15% at 33.9% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(fx84w097-il) FX 84-W-097 | Wortmann FX 84-W-097 airfoil for use on wind turbines (W) Max thickness 9.7% at 33.9% chord Max camber 2.8% at 37.1% chord | Remove Airfoil details Airfoil plotter |
(e334-il) EPPLER 334 AIRFOIL | Eppler E334 flying wing airfoil Max thickness 11.9% at 30.3% chord Max camber 4% at 25.4% chord | Remove Airfoil details Airfoil plotter |
(fx66a175-il) WORTMANN FX 66-17A-175 AIRFOIL | Wortmann FX 66-17A-175 airfoil Max thickness 17.5% at 33.9% chord Max camber 4.2% at 40.2% chord | Remove Airfoil details Airfoil plotter |
(ag45ct02r-il) AG45ct -02f | Drela AG45ct -02f airfoil Max thickness 6.9% at 23.3% chord Max camber 1.8% at 33.1% chord | Remove Airfoil details Airfoil plotter |
(e332-il) EPPLER 332 AIRFOIL | Eppler E332 flying wing airfoil Max thickness 11.5% at 32.3% chord Max camber 3.1% at 22.6% chord | Remove Airfoil details Airfoil plotter |
(sa7026-il) SA7026 | Selig / Ashok Gopalarathnam SA7026 low Reynolds number airfoil Max thickness 9% at 32.9% chord Max camber 3.8% at 47.1% chord | Remove Airfoil details Airfoil plotter |
(sc20606-il) NASA SC(2)-0606 AIRFOIL | NASA SC(2)-0606 airfoil (NASA TP-2969) Max thickness 6% at 34% chord Max camber 1.3% at 81% chord | Remove Airfoil details Airfoil plotter |
(hq209-il) HQ 2.0/9 AIRFOIL | Quabeck HQ 2.0/9 R/C sailplane airfoil Max thickness 9% at 35% chord Max camber 2% at 50% chord | Remove Airfoil details Airfoil plotter |
(raf32-il) RAF 32 AIRFOIL | RAF-32 airfoil Max thickness 12.7% at 30% chord Max camber 5% at 50% chord | Remove Airfoil details Airfoil plotter |
(e541-il) EPPLER 541 AIRFOIL | Eppler E541 general aviation airfoil Max thickness 16.6% at 46.2% chord Max camber 1.7% at 36.3% chord | Remove Airfoil details Airfoil plotter |
(hs1620-il) HAM-STD HS1-620 AIRFOIL | HS1 family of prop airfoils from US Patent No. 4 Max thickness 20% at 34% chord Max camber 4.1% at 44% chord | Remove Airfoil details Airfoil plotter |
(e543-il) EPPLER 543 AIRFOIL | Eppler E543 general aviation airfoil Max thickness 17.2% at 40.7% chord Max camber 1.9% at 31% chord | Remove Airfoil details Airfoil plotter |
(ah82150f-il) AH 82-150 F | Althaus AH 82-150 F airfoil Max thickness 15% at 43.5% chord Max camber 3.6% at 46.7% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (goe374-il,sc20410-il,s9033-il,s805a-nr,e837-il,sc20403-il,rg12-il,s9037-il,hq308-il,sc20518-il,goe566-il,sd7037-il,fx711520-il,fx84w097-il,e334-il,fx66a175-il,ag45ct02r-il,e332-il,sa7026-il,sc20606-il,hq209-il,raf32-il,e541-il,hs1620-il,e543-il,ah82150f-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe374-il | 50,000 | 9 | 32.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe374-il | 50,000 | 5 | 40.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe374-il | 100,000 | 9 | 51.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe374-il | 100,000 | 5 | 57.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe374-il | 200,000 | 9 | 72.4 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe374-il | 200,000 | 5 | 74.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe374-il | 500,000 | 9 | 98.7 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe374-il | 500,000 | 5 | 97.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe374-il | 1,000,000 | 9 | 117.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe374-il | 1,000,000 | 5 | 110.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20410-il | 50,000 | 9 | 22.4 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20410-il | 50,000 | 5 | 22.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20410-il | 100,000 | 9 | 30.6 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20410-il | 100,000 | 5 | 29.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20410-il | 200,000 | 9 | 35.3 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20410-il | 200,000 | 5 | 41.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20410-il | 500,000 | 9 | 54 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20410-il | 500,000 | 5 | 60.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20410-il | 1,000,000 | 9 | 71.9 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20410-il | 1,000,000 | 5 | 74.7 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s9033-il | 50,000 | 9 | 21.7 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s9033-il | 50,000 | 5 | 23.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s9033-il | 100,000 | 9 | 29.5 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s9033-il | 100,000 | 5 | 32.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s9033-il | 200,000 | 9 | 39.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s9033-il | 200,000 | 5 | 42.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s9033-il | 500,000 | 9 | 56.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s9033-il | 500,000 | 5 | 58.9 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s9033-il | 1,000,000 | 9 | 70.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s9033-il | 1,000,000 | 5 | 72 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s805a-nr | 50,000 | 9 | 30.1 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s805a-nr | 50,000 | 5 | 27.1 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s805a-nr | 100,000 | 9 | 50.9 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s805a-nr | 100,000 | 5 | 50.6 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s805a-nr | 200,000 | 9 | 75.6 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s805a-nr | 200,000 | 5 | 67 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s805a-nr | 500,000 | 9 | 96.9 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s805a-nr | 500,000 | 5 | 89.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s805a-nr | 1,000,000 | 9 | 117.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s805a-nr | 1,000,000 | 5 | 103.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e837-il | 50,000 | 9 | 26.6 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e837-il | 50,000 | 5 | 25.5 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e837-il | 100,000 | 9 | 43.2 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e837-il | 100,000 | 5 | 37.7 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e837-il | 200,000 | 9 | 53 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e837-il | 200,000 | 5 | 50.3 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e837-il | 500,000 | 9 | 70.6 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e837-il | 500,000 | 5 | 61.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e837-il | 1,000,000 | 9 | 80.1 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e837-il | 1,000,000 | 5 | 65.7 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20403-il | 50,000 | 9 | 18 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20403-il | 50,000 | 5 | 18 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20403-il | 100,000 | 9 | 24.4 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20403-il | 100,000 | 5 | 21.8 at α=1.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20403-il | 200,000 | 9 | 32.5 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20403-il | 200,000 | 5 | 28.9 at α=1° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20403-il | 500,000 | 9 | 42.4 at α=0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20403-il | 500,000 | 5 | 33.2 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20403-il | 1,000,000 | 9 | 46.5 at α=0.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20403-il | 1,000,000 | 5 | 39.9 at α=1.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rg12-il | 50,000 | 9 | 32.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rg12-il | 50,000 | 5 | 34.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rg12-il | 100,000 | 9 | 48.9 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rg12-il | 100,000 | 5 | 47.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rg12-il | 200,000 | 9 | 64.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rg12-il | 200,000 | 5 | 58.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rg12-il | 500,000 | 9 | 82.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rg12-il | 500,000 | 5 | 72.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| rg12-il | 1,000,000 | 9 | 91.4 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| rg12-il | 1,000,000 | 5 | 81.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s9037-il | 50,000 | 9 | 34.7 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s9037-il | 50,000 | 5 | 39.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s9037-il | 100,000 | 9 | 56.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s9037-il | 100,000 | 5 | 57.7 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s9037-il | 200,000 | 9 | 78.1 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s9037-il | 200,000 | 5 | 74.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s9037-il | 500,000 | 9 | 104.8 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s9037-il | 500,000 | 5 | 95.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s9037-il | 1,000,000 | 9 | 123.2 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s9037-il | 1,000,000 | 5 | 110.1 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq308-il | 50,000 | 9 | 40.6 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq308-il | 50,000 | 5 | 42.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq308-il | 100,000 | 9 | 62.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq308-il | 100,000 | 5 | 60.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq308-il | 200,000 | 9 | 86.1 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq308-il | 200,000 | 5 | 79.6 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq308-il | 500,000 | 9 | 116.5 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq308-il | 500,000 | 5 | 99.5 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq308-il | 1,000,000 | 9 | 135.4 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq308-il | 1,000,000 | 5 | 99.9 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20518-il | 50,000 | 9 | 26 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20518-il | 50,000 | 5 | 20.9 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20518-il | 100,000 | 9 | 25.9 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20518-il | 100,000 | 5 | 30.2 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20518-il | 200,000 | 9 | 36.5 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20518-il | 200,000 | 5 | 43.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20518-il | 500,000 | 9 | 59.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20518-il | 500,000 | 5 | 62.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20518-il | 1,000,000 | 9 | 77.3 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20518-il | 1,000,000 | 5 | 78.1 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe566-il | 50,000 | 9 | 34.4 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe566-il | 50,000 | 5 | 36.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe566-il | 100,000 | 9 | 52.4 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe566-il | 100,000 | 5 | 50.3 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe566-il | 200,000 | 9 | 70 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe566-il | 200,000 | 5 | 61.7 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe566-il | 500,000 | 9 | 88.5 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe566-il | 500,000 | 5 | 79.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe566-il | 1,000,000 | 9 | 97.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe566-il | 1,000,000 | 5 | 90 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7037-il | 50,000 | 9 | 34.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7037-il | 50,000 | 5 | 39.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7037-il | 100,000 | 9 | 55.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7037-il | 100,000 | 5 | 55.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7037-il | 200,000 | 9 | 74.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7037-il | 200,000 | 5 | 70.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7037-il | 500,000 | 9 | 99.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7037-il | 500,000 | 5 | 90.1 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sd7037-il | 1,000,000 | 9 | 116 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sd7037-il | 1,000,000 | 5 | 104.6 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx711520-il | 50,000 | 9 | 27.2 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx711520-il | 50,000 | 5 | 25.6 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx711520-il | 100,000 | 9 | 36.7 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx711520-il | 100,000 | 5 | 33.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx711520-il | 200,000 | 9 | 44.3 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx711520-il | 200,000 | 5 | 38.6 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx711520-il | 500,000 | 9 | 49.1 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx711520-il | 500,000 | 5 | 48 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx711520-il | 1,000,000 | 9 | 57.9 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx711520-il | 1,000,000 | 5 | 56.8 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w097-il | 50,000 | 9 | 36.1 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w097-il | 50,000 | 5 | 36.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w097-il | 100,000 | 9 | 56.5 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w097-il | 100,000 | 5 | 55.6 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w097-il | 200,000 | 9 | 76.9 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w097-il | 200,000 | 5 | 73.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w097-il | 500,000 | 9 | 104.3 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w097-il | 500,000 | 5 | 96.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx84w097-il | 1,000,000 | 9 | 123.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx84w097-il | 1,000,000 | 5 | 112.1 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e334-il | 50,000 | 9 | 16.6 at α=0.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e334-il | 50,000 | 5 | 27.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e334-il | 100,000 | 9 | 39.9 at α=12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e334-il | 100,000 | 5 | 48.6 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e334-il | 200,000 | 9 | 66.1 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e334-il | 200,000 | 5 | 70 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e334-il | 500,000 | 9 | 100.8 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e334-il | 500,000 | 5 | 98.4 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e334-il | 1,000,000 | 9 | 125.6 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e334-il | 1,000,000 | 5 | 116.5 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx66a175-il | 50,000 | 9 | 4.9 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx66a175-il | 50,000 | 5 | 12.3 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx66a175-il | 100,000 | 9 | 12.6 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx66a175-il | 100,000 | 5 | 34.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx66a175-il | 200,000 | 9 | 70.1 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx66a175-il | 200,000 | 5 | 71.5 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx66a175-il | 500,000 | 9 | 103.3 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx66a175-il | 500,000 | 5 | 100.6 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx66a175-il | 1,000,000 | 9 | 128.4 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx66a175-il | 1,000,000 | 5 | 124.1 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag45ct02r-il | 50,000 | 9 | 30.3 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag45ct02r-il | 50,000 | 5 | 34.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag45ct02r-il | 100,000 | 9 | 45.3 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag45ct02r-il | 100,000 | 5 | 46.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag45ct02r-il | 200,000 | 9 | 60.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag45ct02r-il | 200,000 | 5 | 59.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag45ct02r-il | 500,000 | 9 | 80.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag45ct02r-il | 500,000 | 5 | 76.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag45ct02r-il | 1,000,000 | 9 | 94.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag45ct02r-il | 1,000,000 | 5 | 89.1 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e332-il | 50,000 | 9 | 17.4 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e332-il | 50,000 | 5 | 27.7 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e332-il | 100,000 | 9 | 40.7 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e332-il | 100,000 | 5 | 47.1 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e332-il | 200,000 | 9 | 64.3 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e332-il | 200,000 | 5 | 67.2 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e332-il | 500,000 | 9 | 95.6 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e332-il | 500,000 | 5 | 86 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e332-il | 1,000,000 | 9 | 107.9 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e332-il | 1,000,000 | 5 | 101.8 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7026-il | 50,000 | 9 | 38.4 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7026-il | 50,000 | 5 | 40.6 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7026-il | 100,000 | 9 | 61.8 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7026-il | 100,000 | 5 | 61.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7026-il | 200,000 | 9 | 87.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7026-il | 200,000 | 5 | 82.8 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7026-il | 500,000 | 9 | 121.1 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7026-il | 500,000 | 5 | 106.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sa7026-il | 1,000,000 | 9 | 143.1 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sa7026-il | 1,000,000 | 5 | 120.7 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20606-il | 50,000 | 9 | 23.3 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20606-il | 50,000 | 5 | 25.3 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20606-il | 100,000 | 9 | 31.7 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20606-il | 100,000 | 5 | 35 at α=1.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20606-il | 200,000 | 9 | 51.8 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20606-il | 200,000 | 5 | 46.2 at α=0.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20606-il | 500,000 | 9 | 72.4 at α=0.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20606-il | 500,000 | 5 | 53.6 at α=-0.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| sc20606-il | 1,000,000 | 9 | 82.1 at α=-0.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sc20606-il | 1,000,000 | 5 | 65.6 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq209-il | 50,000 | 9 | 36.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq209-il | 50,000 | 5 | 37.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq209-il | 100,000 | 9 | 55.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq209-il | 100,000 | 5 | 53.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq209-il | 200,000 | 9 | 74.2 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq209-il | 200,000 | 5 | 68.1 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq209-il | 500,000 | 9 | 97.9 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq209-il | 500,000 | 5 | 79.6 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hq209-il | 1,000,000 | 9 | 105.7 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hq209-il | 1,000,000 | 5 | 85.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf32-il | 50,000 | 9 | 29.2 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf32-il | 50,000 | 5 | 25.6 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf32-il | 100,000 | 9 | 56.2 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf32-il | 100,000 | 5 | 56.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf32-il | 200,000 | 9 | 85.7 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf32-il | 200,000 | 5 | 84.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf32-il | 500,000 | 9 | 123.7 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf32-il | 500,000 | 5 | 116.6 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| raf32-il | 1,000,000 | 9 | 152.3 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| raf32-il | 1,000,000 | 5 | 134.8 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e541-il | 50,000 | 9 | 25.2 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e541-il | 50,000 | 5 | 21 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e541-il | 100,000 | 9 | 40.5 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e541-il | 100,000 | 5 | 29.3 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e541-il | 200,000 | 9 | 46.8 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e541-il | 200,000 | 5 | 50.7 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e541-il | 500,000 | 9 | 78.3 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e541-il | 500,000 | 5 | 79.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e541-il | 1,000,000 | 9 | 106.4 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e541-il | 1,000,000 | 5 | 96.7 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hs1620-il | 50,000 | 9 | 16 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hs1620-il | 50,000 | 5 | 25.2 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hs1620-il | 100,000 | 9 | 43.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hs1620-il | 100,000 | 5 | 38.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hs1620-il | 200,000 | 9 | 59.4 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hs1620-il | 200,000 | 5 | 51.2 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hs1620-il | 500,000 | 9 | 72.2 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hs1620-il | 500,000 | 5 | 57.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| hs1620-il | 1,000,000 | 9 | 76.3 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| hs1620-il | 1,000,000 | 5 | 70.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e543-il | 50,000 | 9 | 21.3 at α=12.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e543-il | 50,000 | 5 | 17.9 at α=11.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e543-il | 100,000 | 9 | 42.3 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e543-il | 100,000 | 5 | 35.3 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e543-il | 200,000 | 9 | 56.6 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e543-il | 200,000 | 5 | 58.6 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e543-il | 500,000 | 9 | 86.2 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e543-il | 500,000 | 5 | 82.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e543-il | 1,000,000 | 9 | 108.4 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e543-il | 1,000,000 | 5 | 98.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah82150f-il | 50,000 | 9 | 17.6 at α=12.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah82150f-il | 50,000 | 5 | 19.4 at α=10.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah82150f-il | 100,000 | 9 | 34.6 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah82150f-il | 100,000 | 5 | 33.5 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah82150f-il | 200,000 | 9 | 58.2 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah82150f-il | 200,000 | 5 | 53.1 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah82150f-il | 500,000 | 9 | 95.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah82150f-il | 500,000 | 5 | 99.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah82150f-il | 1,000,000 | 9 | 135.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah82150f-il | 1,000,000 | 5 | 133.8 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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