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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(goe279-il) GOE 279 (DAIMLER X) AIRFOIL | Gottingen 279 (DAIMLER X) airfoil Max thickness 7.4% at 30% chord Max camber 4.7% at 40% chord | Remove Airfoil details Airfoil plotter |
(goe303-il) GOE 303 (FRIEDRICHSHAFEN G03) AIRFOIL | Gottingen 303 (Friedrichshafen G03) airfoil Max thickness 9.8% at 29.9% chord Max camber 5.9% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(goe269-il) GOE 269 AIRFOIL | Gottingen 269 airfoil Max thickness 6.6% at 29.9% chord Max camber 5% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(goe288-il) GOE 288 AIRFOIL | Gottingen 288 airfoil Max thickness 17.4% at 29.3% chord Max camber 5.5% at 39.3% chord | Remove Airfoil details Airfoil plotter |
(goe115-il) GOE 115 (MVA MK.2) AIRFOIL | Gottingen 115 (MVA MK.2) airfoil Max thickness 9.7% at 29.7% chord Max camber 3.7% at 39.7% chord | Remove Airfoil details Airfoil plotter |
(goe116-il) GOE 116 (MVA MK.3) AIRFOIL | Gottingen 116 (MVA MK.3) airfoil Max thickness 9.3% at 39.8% chord Max camber 4.1% at 39.8% chord | Remove Airfoil details Airfoil plotter |
(goe282-il) GOE 282 (DAIMLER XIII) AIRFOIL | Gottingen 282 (DAIMLER XIII) airfoil Max thickness 9.1% at 19.9% chord Max camber 5% at 39.9% chord | Remove Airfoil details Airfoil plotter |
(goe114-il) GOE 114 (MVA MK.1) AIRFOIL | Gottingen 114 (MVA MK.1) airfoil Max thickness 9.6% at 29.7% chord Max camber 3.5% at 49.7% chord | Remove Airfoil details Airfoil plotter |
(goe304-il) GOE 304 (FRIEDRICHSHAFEN G02) AIRFOIL | Gottingen 304 (Friedrichshafen G02) airfoil Max thickness 9% at 29.8% chord Max camber 6.3% at 39.8% chord | Remove Airfoil details Airfoil plotter |
(goe277-il) GOE 277 (DAIMLER VIII) AIRFOIL | Gottingen 277 (DAIMLER VIII) airfoil Max thickness 8.3% at 29.9% chord Max camber 4.4% at 29.9% chord | Remove Airfoil details Airfoil plotter |
(goe113-il) GOE 113 AIRFOIL | Gottingen 113 airfoil Max thickness 6.7% at 30% chord Max camber 3% at 40% chord | Remove Airfoil details Airfoil plotter |
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Polars for (goe279-il,goe303-il,goe269-il,goe288-il,goe115-il,goe116-il,goe282-il,goe114-il,goe304-il,goe277-il,goe113-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe279-il | 50,000 | 9 | 37.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe279-il | 50,000 | 5 | 42.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe279-il | 100,000 | 9 | 58.3 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe279-il | 100,000 | 5 | 59 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe279-il | 200,000 | 9 | 77.4 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe279-il | 200,000 | 5 | 73.5 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe279-il | 500,000 | 9 | 96.9 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe279-il | 500,000 | 5 | 93 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe279-il | 1,000,000 | 9 | 113.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe279-il | 1,000,000 | 5 | 105 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe303-il | 50,000 | 9 | 26.2 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe303-il | 50,000 | 5 | 39.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe303-il | 100,000 | 9 | 58.3 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe303-il | 100,000 | 5 | 61.6 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe303-il | 200,000 | 9 | 83.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe303-il | 200,000 | 5 | 81.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe303-il | 500,000 | 9 | 114.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe303-il | 500,000 | 5 | 106.4 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe303-il | 1,000,000 | 9 | 137.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe303-il | 1,000,000 | 5 | 122.1 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe269-il | 50,000 | 9 | 36.1 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe269-il | 50,000 | 5 | 43.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe269-il | 100,000 | 9 | 59.1 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe269-il | 100,000 | 5 | 61.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe269-il | 200,000 | 9 | 80.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe269-il | 200,000 | 5 | 79.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe269-il | 500,000 | 9 | 107.7 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe269-il | 500,000 | 5 | 102.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe269-il | 1,000,000 | 9 | 127.9 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe269-il | 1,000,000 | 5 | 115.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe288-il | 50,000 | 9 | 7.6 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe288-il | 50,000 | 5 | 27.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe288-il | 100,000 | 9 | 43.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe288-il | 100,000 | 5 | 50.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe288-il | 200,000 | 9 | 70.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe288-il | 200,000 | 5 | 69.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe288-il | 500,000 | 9 | 96.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe288-il | 500,000 | 5 | 91.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe288-il | 1,000,000 | 9 | 117.1 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe288-il | 1,000,000 | 5 | 113.9 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe115-il | 50,000 | 9 | 32.2 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe115-il | 50,000 | 5 | 37.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe115-il | 100,000 | 9 | 57.1 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe115-il | 100,000 | 5 | 57.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe115-il | 200,000 | 9 | 77.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe115-il | 200,000 | 5 | 76.7 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe115-il | 500,000 | 9 | 108.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe115-il | 500,000 | 5 | 102.9 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe115-il | 1,000,000 | 9 | 132 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe115-il | 1,000,000 | 5 | 98.7 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe116-il | 50,000 | 9 | 29.6 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe116-il | 50,000 | 5 | 37.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe116-il | 100,000 | 9 | 58 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe116-il | 100,000 | 5 | 56.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe116-il | 200,000 | 9 | 78.4 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe116-il | 200,000 | 5 | 76.2 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe116-il | 500,000 | 9 | 106.8 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe116-il | 500,000 | 5 | 81.4 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe116-il | 1,000,000 | 9 | 100.3 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe116-il | 1,000,000 | 5 | 91.9 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe282-il | 50,000 | 9 | 34.8 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe282-il | 50,000 | 5 | 41 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe282-il | 100,000 | 9 | 57 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe282-il | 100,000 | 5 | 59 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe282-il | 200,000 | 9 | 77.4 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe282-il | 200,000 | 5 | 75.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe282-il | 500,000 | 9 | 102.5 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe282-il | 500,000 | 5 | 94.8 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe282-il | 1,000,000 | 9 | 118.3 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe282-il | 1,000,000 | 5 | 105.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe114-il | 50,000 | 9 | 35.4 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe114-il | 50,000 | 5 | 32.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe114-il | 100,000 | 9 | 49.7 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe114-il | 100,000 | 5 | 44.4 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe114-il | 200,000 | 9 | 60.9 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe114-il | 200,000 | 5 | 50.8 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe114-il | 500,000 | 9 | 93.4 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe114-il | 500,000 | 5 | 74.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe114-il | 1,000,000 | 9 | 70.6 at α=1° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe114-il | 1,000,000 | 5 | 67.6 at α=1° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe304-il | 50,000 | 9 | 33.1 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe304-il | 50,000 | 5 | 38.9 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe304-il | 100,000 | 9 | 62 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe304-il | 100,000 | 5 | 64.1 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe304-il | 200,000 | 9 | 88.8 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe304-il | 200,000 | 5 | 86.1 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe304-il | 500,000 | 9 | 122.8 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe304-il | 500,000 | 5 | 109.7 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe304-il | 1,000,000 | 9 | 145.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe304-il | 1,000,000 | 5 | 117.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe277-il | 50,000 | 9 | 34 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe277-il | 50,000 | 5 | 38.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe277-il | 100,000 | 9 | 54.3 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe277-il | 100,000 | 5 | 55.7 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe277-il | 200,000 | 9 | 73.5 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe277-il | 200,000 | 5 | 73.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe277-il | 500,000 | 9 | 100.9 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe277-il | 500,000 | 5 | 98.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe277-il | 1,000,000 | 9 | 122.6 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe277-il | 1,000,000 | 5 | 118.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe113-il | 50,000 | 9 | 37.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe113-il | 50,000 | 5 | 40 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe113-il | 100,000 | 9 | 54.7 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe113-il | 100,000 | 5 | 54.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe113-il | 200,000 | 9 | 70 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe113-il | 200,000 | 5 | 66.8 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe113-il | 500,000 | 9 | 86.8 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe113-il | 500,000 | 5 | 78 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe113-il | 1,000,000 | 9 | 97.1 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe113-il | 1,000,000 | 5 | 83.3 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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