GOE 406 AIRFOIL (goe406-il)
GOE 406 AIRFOIL - Gottingen 406 airfoil
| Details | Dat file | Parser | |
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(goe406-il) GOE 406 AIRFOIL Gottingen 406 airfoil Max thickness 11.7% at 29.9% chord. Max camber 5.5% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 406 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123600 0.0264700
0.0248000 0.0371300
0.0497100 0.0541700
0.0746300 0.0680000
0.0995700 0.0788400
0.1494800 0.0960100
0.1994300 0.1063800
0.2993900 0.1137200
0.3993900 0.1132600
0.4994300 0.1064000
0.5995000 0.0926400
0.6996000 0.0738800
0.7997100 0.0530200
0.8998300 0.0307600
0.9498900 0.0162100
1.0000000 0.0000000
0.0000000 0.0000000
0.0125800 -.0147300
0.0250900 -.0157600
0.0500800 -.0151300
0.0750700 -.0129900
0.1000600 -.0111600
0.1500500 -.0078700
0.2000300 -.0058200
0.3000200 -.0031800
0.4000100 -.0026400
0.5000100 -.0026000
0.6000200 -.0035400
0.7000300 -.0047200
0.8000300 -.0062800
0.9000500 -.0089400
0.9500600 -.0082700
1.0000000 0.0000000
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Polars for GOE 406 AIRFOIL (goe406-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe406-il | 50,000 | 9 | 17.8 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe406-il | 50,000 | 5 | 34.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe406-il | 100,000 | 9 | 54.1 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe406-il | 100,000 | 5 | 53.1 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe406-il | 200,000 | 9 | 75.6 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe406-il | 200,000 | 5 | 68.1 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe406-il | 500,000 | 9 | 94.8 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe406-il | 500,000 | 5 | 89.3 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe406-il | 1,000,000 | 9 | 114.2 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe406-il | 1,000,000 | 5 | 112 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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