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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(ag16-il) AG16 | Drela AG16 airfoil Max thickness 7.1% at 23.4% chord Max camber 1.9% at 46.9% 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 |
(goe600-il) GOE 600 AIRFOIL | Gottingen 600 airfoil Max thickness 13.1% at 29.4% chord Max camber 1.9% at 49.4% chord | Remove Airfoil details Airfoil plotter |
(goe416a-il) GOE 416A AIRFOIL | Gottingen 416A airfoil Max thickness 11.7% at 29.5% chord Max camber 1.3% at 59.6% chord | Remove Airfoil details Airfoil plotter |
(goe346-il) GOE 346 (FRIEDRICHSHAFEN-STAAKEN) AIRFOIL | Gottingen 346 (Friedrichshafen-Staaken) airfoil Max thickness 5.7% at 39.9% chord Max camber 3.8% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(goe534-il) GOE 534 AIRFOIL | Gottingen 534 airfoil Max thickness 14.1% at 19.6% chord Max camber 5.2% at 39.6% chord | Remove Airfoil details Airfoil plotter |
(s8038-il) S8038 (13%) | Selig S8038 (13%) low Reynolds number airfoil Max thickness 13% at 32.9% chord Max camber 0.6% at 40.1% chord | Remove Airfoil details Airfoil plotter |
(goe443-il) GOE 443 AIRFOIL | Gottingen 443 airfoil Max thickness 5% at 30% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(goe444-il) GOE 444 AIRFOIL | Gottingen 444 airfoil Max thickness 5.6% at 30% chord Max camber 0% at 0% chord | Remove Airfoil details Airfoil plotter |
(goe650-il) GOE 650 AIRFOIL | Gottingen 650 airfoil Max thickness 13.4% at 19.5% chord Max camber 4.4% at 49.5% chord | Remove Airfoil details Airfoil plotter |
(arad20-il) ARA-D 20% AIRFOIL | Aeronautical Research Association/Bocci-Dowty Rotol ARA-D 20% thick propeller airfoil Max thickness 20% at 25% chord Max camber 3.8% at 25% chord | Remove Airfoil details Airfoil plotter |
(oa206-il) ONERA OA206 AIRFOIL | ONERA/Aerospatiale OA206 rotorcraft airfoil (Constructed from patent and smoothed) Max thickness 6% at 31.8% chord Max camber 0.8% at 19.6% chord | Remove Airfoil details Airfoil plotter |
(fx05191-il) WORTMANN FX 05-191 AIRFOIL | Wortmann FX 05-191 airfoil Max thickness 19.1% at 37.1% chord Max camber 2.6% at 50% chord | Remove Airfoil details Airfoil plotter |
(goe514-il) GOE 514 AIRFOIL | Gottingen 514 airfoil Max thickness 16.6% at 19.7% chord Max camber 6.4% at 39.7% chord | Remove Airfoil details Airfoil plotter |
(fg1-il) Fage & Collins 1 | Fage & Collins 1 airfoil Max thickness 8.2% at 30% chord Max camber 3.1% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe233-il) GOE 233 (MVA CA4) AIRFOIL | Gottingen 233 (MVA CA4) airfoil Max thickness 11.6% at 19.8% chord Max camber 8.2% at 49.8% chord | Remove Airfoil details Airfoil plotter |
(goe615-il) GOE 615 AIRFOIL | Gottingen 615 airfoil Max thickness 13.7% at 29.7% chord Max camber 5.6% at 39.7% chord | Remove Airfoil details Airfoil plotter |
(e1212-il) EPPLER E1212 AIRFOIL | Eppler E1212 general aviation airfoil Max thickness 17.7% at 23.4% chord Max camber 3.2% at 36.4% chord | Remove Airfoil details Airfoil plotter |
(goe767-il) GOE 767 AIRFOIL | Gottingen 767 airfoil Max thickness 12% at 20% chord Max camber 1.5% at 20% chord | Remove Airfoil details Airfoil plotter |
(ag36-il) AG36 | Drela AG36 airfoil Max thickness 8.2% at 27.9% chord Max camber 2.3% at 37% chord | Remove Airfoil details Airfoil plotter |
(goe526-il) GOE 526 AIRFOIL | Gottingen 526 airfoil Max thickness 12.3% at 29.7% chord Max camber 4.1% at 39.7% chord | Remove Airfoil details Airfoil plotter |
(goe509-il) GOE 509 AIRFOIL | Gottingen 509 airfoil Max thickness 11.1% at 29.9% chord Max camber 5.2% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(goe363-il) GOE 363 AIRFOIL | Gottingen 363 airfoil Max thickness 11.1% at 19.8% chord Max camber 5.7% at 39.8% chord | Remove Airfoil details Airfoil plotter |
(goe548-il) GOE 548 AIRFOIL | Gottingen 548 airfoil Max thickness 11.9% at 40% chord Max camber 2.3% at 50% chord | Remove Airfoil details Airfoil plotter |
(goe54-il) GOE 54 AIRFOIL | Gottingen 54 airfoil Max thickness 6.5% at 14.9% chord Max camber 3.5% at 19.9% chord | Remove Airfoil details Airfoil plotter |
(goe654-il) GOE 654 AIRFOIL | Gottingen 654 airfoil Max thickness 14.5% at 30% chord Max camber 5.2% at 40% chord | Remove Airfoil details Airfoil plotter |
Drawing Options
Polars for (ag16-il,sc20410-il,goe600-il,goe416a-il,goe346-il,goe534-il,s8038-il,goe443-il,goe444-il,goe650-il,arad20-il,oa206-il,fx05191-il,goe514-il,fg1-il,goe233-il,goe615-il,e1212-il,goe767-il,ag36-il,goe526-il,goe509-il,goe363-il,goe548-il,goe54-il,goe654-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ag16-il | 50,000 | 9 | 33.5 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag16-il | 50,000 | 5 | 36 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag16-il | 100,000 | 9 | 48.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag16-il | 100,000 | 5 | 48.4 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag16-il | 200,000 | 9 | 63.6 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag16-il | 200,000 | 5 | 60.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag16-il | 500,000 | 9 | 82.4 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag16-il | 500,000 | 5 | 76.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag16-il | 1,000,000 | 9 | 95.3 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag16-il | 1,000,000 | 5 | 88.4 at α=4.75° | 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 | |
| goe600-il | 50,000 | 9 | 32.5 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe600-il | 50,000 | 5 | 33.9 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe600-il | 100,000 | 9 | 51.1 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe600-il | 100,000 | 5 | 49.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe600-il | 200,000 | 9 | 69.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe600-il | 200,000 | 5 | 62.9 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe600-il | 500,000 | 9 | 91.2 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe600-il | 500,000 | 5 | 76.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe600-il | 1,000,000 | 9 | 99.6 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe600-il | 1,000,000 | 5 | 86 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe416a-il | 50,000 | 9 | 31.1 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe416a-il | 50,000 | 5 | 34 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe416a-il | 100,000 | 9 | 46.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe416a-il | 100,000 | 5 | 47.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe416a-il | 200,000 | 9 | 61.4 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe416a-il | 200,000 | 5 | 57.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe416a-il | 500,000 | 9 | 71 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe416a-il | 500,000 | 5 | 67.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe416a-il | 1,000,000 | 9 | 80.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe416a-il | 1,000,000 | 5 | 75.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe346-il | 50,000 | 9 | 40.3 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe346-il | 50,000 | 5 | 42.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe346-il | 100,000 | 9 | 61.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe346-il | 100,000 | 5 | 59.5 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe346-il | 200,000 | 9 | 81.2 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe346-il | 200,000 | 5 | 72.8 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe346-il | 500,000 | 9 | 95.5 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe346-il | 500,000 | 5 | 83 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe346-il | 1,000,000 | 9 | 100.8 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe346-il | 1,000,000 | 5 | 91.1 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe534-il | 50,000 | 9 | 20 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe534-il | 50,000 | 5 | 32.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe534-il | 100,000 | 9 | 44 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe534-il | 100,000 | 5 | 50.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe534-il | 200,000 | 9 | 65.4 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe534-il | 200,000 | 5 | 67.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe534-il | 500,000 | 9 | 93.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe534-il | 500,000 | 5 | 91 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe534-il | 1,000,000 | 9 | 114.9 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe534-il | 1,000,000 | 5 | 110.2 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s8038-il | 50,000 | 9 | 29.2 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s8038-il | 50,000 | 5 | 30.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s8038-il | 100,000 | 9 | 45.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s8038-il | 100,000 | 5 | 43.2 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s8038-il | 200,000 | 9 | 59.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s8038-il | 200,000 | 5 | 52.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s8038-il | 500,000 | 9 | 71.6 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s8038-il | 500,000 | 5 | 69 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| s8038-il | 1,000,000 | 9 | 85.8 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| s8038-il | 1,000,000 | 5 | 83.6 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe443-il | 50,000 | 9 | 16.1 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe443-il | 50,000 | 5 | 16 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe443-il | 100,000 | 9 | 20.3 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe443-il | 100,000 | 5 | 26.2 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe443-il | 200,000 | 9 | 34 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe443-il | 200,000 | 5 | 32.2 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe443-il | 500,000 | 9 | 44.5 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe443-il | 500,000 | 5 | 32 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe443-il | 1,000,000 | 9 | 43.3 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe443-il | 1,000,000 | 5 | 60.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe444-il | 50,000 | 9 | 17.1 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe444-il | 50,000 | 5 | 16.5 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe444-il | 100,000 | 9 | 21.5 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe444-il | 100,000 | 5 | 24.8 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe444-il | 200,000 | 9 | 38.2 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe444-il | 200,000 | 5 | 35.2 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe444-il | 500,000 | 9 | 45.9 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe444-il | 500,000 | 5 | 31.8 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe444-il | 1,000,000 | 9 | 42.3 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe444-il | 1,000,000 | 5 | 34.1 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe650-il | 50,000 | 9 | 31.8 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe650-il | 50,000 | 5 | 34.8 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe650-il | 100,000 | 9 | 56 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe650-il | 100,000 | 5 | 53.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe650-il | 200,000 | 9 | 79 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe650-il | 200,000 | 5 | 70.5 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe650-il | 500,000 | 9 | 101.6 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe650-il | 500,000 | 5 | 83.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe650-il | 1,000,000 | 9 | 109.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe650-il | 1,000,000 | 5 | 96.4 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| arad20-il | 50,000 | 9 | 9.7 at α=-0.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| arad20-il | 50,000 | 5 | 18.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| arad20-il | 100,000 | 9 | 24.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| arad20-il | 100,000 | 5 | 38.6 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| arad20-il | 200,000 | 9 | 52 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| arad20-il | 200,000 | 5 | 56.7 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| arad20-il | 500,000 | 9 | 79.9 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| arad20-il | 500,000 | 5 | 80.1 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| arad20-il | 1,000,000 | 9 | 101.1 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| arad20-il | 1,000,000 | 5 | 98.5 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| oa206-il | 50,000 | 9 | 27.3 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| oa206-il | 50,000 | 5 | 27.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| oa206-il | 100,000 | 9 | 36.4 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| oa206-il | 100,000 | 5 | 35.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| oa206-il | 200,000 | 9 | 46.1 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| oa206-il | 200,000 | 5 | 44.1 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| oa206-il | 500,000 | 9 | 58.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| oa206-il | 500,000 | 5 | 56.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| oa206-il | 1,000,000 | 9 | 67.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| oa206-il | 1,000,000 | 5 | 69.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx05191-il | 50,000 | 9 | 18.1 at α=13.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx05191-il | 50,000 | 5 | 14 at α=13° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx05191-il | 100,000 | 9 | 27.6 at α=11.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx05191-il | 100,000 | 5 | 29.2 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx05191-il | 200,000 | 9 | 55.6 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx05191-il | 200,000 | 5 | 57.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx05191-il | 500,000 | 9 | 89.4 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx05191-il | 500,000 | 5 | 89.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx05191-il | 1,000,000 | 9 | 118.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx05191-il | 1,000,000 | 5 | 112.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe514-il | 50,000 | 9 | 7.2 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe514-il | 50,000 | 5 | 26.1 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe514-il | 100,000 | 9 | 45.3 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe514-il | 100,000 | 5 | 41.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe514-il | 200,000 | 9 | 57.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe514-il | 200,000 | 5 | 51.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe514-il | 500,000 | 9 | 69.2 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe514-il | 500,000 | 5 | 64.7 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe514-il | 1,000,000 | 9 | 84.1 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe514-il | 1,000,000 | 5 | 78.1 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fg1-il | 50,000 | 9 | 37.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fg1-il | 50,000 | 5 | 37.5 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fg1-il | 100,000 | 9 | 57.2 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fg1-il | 100,000 | 5 | 52.7 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fg1-il | 200,000 | 9 | 78.1 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fg1-il | 200,000 | 5 | 66 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fg1-il | 500,000 | 9 | 93.6 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fg1-il | 500,000 | 5 | 82.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fg1-il | 1,000,000 | 9 | 104.9 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fg1-il | 1,000,000 | 5 | 99.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe233-il | 50,000 | 9 | 26.4 at α=11.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe233-il | 50,000 | 5 | 33.4 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe233-il | 100,000 | 9 | 60.9 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe233-il | 100,000 | 5 | 63.1 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe233-il | 200,000 | 9 | 86.7 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe233-il | 200,000 | 5 | 87.1 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe233-il | 500,000 | 9 | 120.7 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe233-il | 500,000 | 5 | 115.8 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe233-il | 1,000,000 | 9 | 146.8 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe233-il | 1,000,000 | 5 | 134.9 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe615-il | 50,000 | 9 | 10.3 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe615-il | 50,000 | 5 | 30.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe615-il | 100,000 | 9 | 51 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe615-il | 100,000 | 5 | 53 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe615-il | 200,000 | 9 | 74.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe615-il | 200,000 | 5 | 72.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe615-il | 500,000 | 9 | 104.1 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe615-il | 500,000 | 5 | 93.5 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe615-il | 1,000,000 | 9 | 125.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe615-il | 1,000,000 | 5 | 102.7 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e1212-il | 50,000 | 9 | 7.1 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e1212-il | 50,000 | 5 | 23.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e1212-il | 100,000 | 9 | 32.1 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e1212-il | 100,000 | 5 | 41.9 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e1212-il | 200,000 | 9 | 55.2 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e1212-il | 200,000 | 5 | 59.6 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e1212-il | 500,000 | 9 | 84.7 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e1212-il | 500,000 | 5 | 85.5 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e1212-il | 1,000,000 | 9 | 109.8 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e1212-il | 1,000,000 | 5 | 107.5 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe767-il | 50,000 | 9 | 15.5 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe767-il | 50,000 | 5 | 23.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe767-il | 100,000 | 9 | 30.3 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe767-il | 100,000 | 5 | 38.6 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe767-il | 200,000 | 9 | 49.7 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe767-il | 200,000 | 5 | 54.9 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe767-il | 500,000 | 9 | 76 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe767-il | 500,000 | 5 | 74.7 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe767-il | 1,000,000 | 9 | 93.1 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe767-il | 1,000,000 | 5 | 91.5 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag36-il | 50,000 | 9 | 32.7 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag36-il | 50,000 | 5 | 36.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag36-il | 100,000 | 9 | 50.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag36-il | 100,000 | 5 | 51 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag36-il | 200,000 | 9 | 67.5 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag36-il | 200,000 | 5 | 64.3 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag36-il | 500,000 | 9 | 88.9 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag36-il | 500,000 | 5 | 81 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag36-il | 1,000,000 | 9 | 103 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag36-il | 1,000,000 | 5 | 93 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe526-il | 50,000 | 9 | 24.8 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe526-il | 50,000 | 5 | 33.3 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe526-il | 100,000 | 9 | 52.2 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe526-il | 100,000 | 5 | 52.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe526-il | 200,000 | 9 | 73.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe526-il | 200,000 | 5 | 69.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe526-il | 500,000 | 9 | 98.4 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe526-il | 500,000 | 5 | 91.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe526-il | 1,000,000 | 9 | 119.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe526-il | 1,000,000 | 5 | 107.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe509-il | 50,000 | 9 | 19.8 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe509-il | 50,000 | 5 | 35.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe509-il | 100,000 | 9 | 51.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe509-il | 100,000 | 5 | 52.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe509-il | 200,000 | 9 | 69.3 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe509-il | 200,000 | 5 | 68.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe509-il | 500,000 | 9 | 96.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe509-il | 500,000 | 5 | 91.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe509-il | 1,000,000 | 9 | 117.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe509-il | 1,000,000 | 5 | 97.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe363-il | 50,000 | 9 | 32.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe363-il | 50,000 | 5 | 37 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe363-il | 100,000 | 9 | 53.3 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe363-il | 100,000 | 5 | 52.3 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe363-il | 200,000 | 9 | 70.1 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe363-il | 200,000 | 5 | 65.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe363-il | 500,000 | 9 | 89.5 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe363-il | 500,000 | 5 | 88.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe363-il | 1,000,000 | 9 | 110.5 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe363-il | 1,000,000 | 5 | 104.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe548-il | 50,000 | 9 | 34.1 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe548-il | 50,000 | 5 | 32.8 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe548-il | 100,000 | 9 | 53.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe548-il | 100,000 | 5 | 51.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe548-il | 200,000 | 9 | 74.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe548-il | 200,000 | 5 | 68.7 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe548-il | 500,000 | 9 | 95 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe548-il | 500,000 | 5 | 76.6 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe548-il | 1,000,000 | 9 | 100.7 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe548-il | 1,000,000 | 5 | 76.3 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe54-il | 50,000 | 9 | 19.8 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe54-il | 50,000 | 5 | 29.3 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe54-il | 100,000 | 9 | 34.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe54-il | 100,000 | 5 | 44.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe54-il | 200,000 | 9 | 58.7 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe54-il | 200,000 | 5 | 64.2 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe54-il | 500,000 | 9 | 87.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe54-il | 500,000 | 5 | 88.1 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe54-il | 1,000,000 | 9 | 106.7 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe54-il | 1,000,000 | 5 | 105.7 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe654-il | 50,000 | 9 | 10 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe654-il | 50,000 | 5 | 28.4 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe654-il | 100,000 | 9 | 41 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe654-il | 100,000 | 5 | 50 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe654-il | 200,000 | 9 | 67.3 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe654-il | 200,000 | 5 | 67.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe654-il | 500,000 | 9 | 94.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe654-il | 500,000 | 5 | 92.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe654-il | 1,000,000 | 9 | 118.6 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe654-il | 1,000,000 | 5 | 115.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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