GOE 711 AIRFOIL (goe711-il)
GOE 711 AIRFOIL - Gottingen 711 airfoil
| Details | Dat file | Parser | |
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(goe711-il) GOE 711 AIRFOIL Gottingen 711 airfoil Max thickness 14.9% at 30% chord. Max camber 6.3% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 711 AIRFOIL
16. 16.
0.0000000 0.0000000
0.0125000 0.0271600
0.0250000 0.0418200
0.0500000 0.0626500
0.0750000 0.0834700
0.1000000 0.0978000
0.1500000 0.1179500
0.2000000 0.1301000
0.3000000 0.1394000
0.4000000 0.1382000
0.5000000 0.1305000
0.7000000 0.1001000
0.8000000 0.0779000
0.9000000 0.0492000
0.9500000 0.0317500
1.0000000 0.0140000
0.0000000 0.0000000
0.0125000 -.0108400
0.0250000 -.0126800
0.0500000 -.0123500
0.0750000 -.0120200
0.1000000 -.0117000
0.1500000 -.0110500
0.2000000 -.0104000
0.3000000 -.0091000
0.4000000 -.0078000
0.5000000 -.0065000
0.7000000 -.0039000
0.8000000 -.0026000
0.9000000 -.0013000
0.9500000 -.0006500
1.0000000 0.0000000
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Polars for GOE 711 AIRFOIL (goe711-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe711-il | 50,000 | 9 | 20.3 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe711-il | 50,000 | 5 | 33.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe711-il | 100,000 | 9 | 48.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe711-il | 100,000 | 5 | 49.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe711-il | 200,000 | 9 | 64.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe711-il | 200,000 | 5 | 62.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe711-il | 500,000 | 9 | 86.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe711-il | 500,000 | 5 | 83.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe711-il | 1,000,000 | 9 | 107.2 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe711-il | 1,000,000 | 5 | 102.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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