GOE 264 AIRFOIL (goe264-il)
GOE 264 AIRFOIL - Gottingen 264 airfoil
| Details | Dat file | Parser | |
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(goe264-il) GOE 264 AIRFOIL Gottingen 264 airfoil Max thickness 6.4% at 20.2% chord. Max camber 5.7% at 28.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 264 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122100 0.0165200
0.0276500 0.0267600
0.0497600 0.0382200
0.0746800 0.0492800
0.0996300 0.0577400
0.1495400 0.0723600
0.2017300 0.0818400
0.2892600 0.0880200
0.3994500 0.0863600
0.4994900 0.0795000
0.5995600 0.0689400
0.6996400 0.0567800
0.7997400 0.0409200
0.8998500 0.0228600
0.9499199 0.0126800
1.0000000 0.0032000
0.0000000 0.0000000
0.0125600 -.0092200
0.0261500 -.0109600
0.0500500 -.0079800
0.0750300 -.0040200
0.1000000 0.0006400
0.1499400 0.0100600
0.1998900 0.0172800
0.2998300 0.0259200
0.3998300 0.0265600
0.4998500 0.0235000
0.5998700 0.0198400
0.6999100 0.0145800
0.7999400 0.0094200
0.8999700 0.0046600
0.9499900 0.0012800
1.0000000 -.0032000
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Polars for GOE 264 AIRFOIL (goe264-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe264-il | 50,000 | 9 | 32.2 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe264-il | 50,000 | 5 | 41.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe264-il | 100,000 | 9 | 59.9 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe264-il | 100,000 | 5 | 60.8 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe264-il | 200,000 | 9 | 79.2 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe264-il | 200,000 | 5 | 79.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe264-il | 500,000 | 9 | 106.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe264-il | 500,000 | 5 | 104.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe264-il | 1,000,000 | 9 | 126.9 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe264-il | 1,000,000 | 5 | 121.8 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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