GOE 766 AIRFOIL (goe766-il)
GOE 766 AIRFOIL - Gottingen 766 airfoil
| Details | Dat file | Parser | |
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(goe766-il) GOE 766 AIRFOIL Gottingen 766 airfoil Max thickness 12% at 25% chord. Max camber 1.5% at 20% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 766 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0264000
0.0250000 0.0360000
0.0500000 0.0481000
0.1000000 0.0628000
0.1500000 0.0709000
0.2000000 0.0740000
0.2500000 0.0743000
0.3000000 0.0728000
0.4000000 0.0654000
0.5000000 0.0557000
0.6000000 0.0453000
0.7000000 0.0346000
0.8000000 0.0237000
0.9000000 0.0119000
0.9500000 0.0061000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0170000
0.0250000 -.0233000
0.0500000 -.0303000
0.1000000 -.0383000
0.1500000 -.0419000
0.2000000 -.0443000
0.2500000 -.0458000
0.3000000 -.0465000
0.4000000 -.0452000
0.5000000 -.0421000
0.6000000 -.0364000
0.7000000 -.0289000
0.8000000 -.0205000
0.9000000 -.0110000
0.9500000 -.0059000
1.0000000 0.0000000
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Polars for GOE 766 AIRFOIL (goe766-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe766-il | 50,000 | 9 | 19.2 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe766-il | 50,000 | 5 | 27.4 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe766-il | 100,000 | 9 | 37.6 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe766-il | 100,000 | 5 | 42 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe766-il | 200,000 | 9 | 55.9 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe766-il | 200,000 | 5 | 57.2 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe766-il | 500,000 | 9 | 80.3 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe766-il | 500,000 | 5 | 77 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe766-il | 1,000,000 | 9 | 98 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe766-il | 1,000,000 | 5 | 87.2 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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