GOE 505 AIRFOIL (goe505-il)
GOE 505 AIRFOIL - Gottingen 505 airfoil
| Details | Dat file | Parser | |
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(goe505-il) GOE 505 AIRFOIL Gottingen 505 airfoil Max thickness 14% at 19.7% chord. Max camber 5.9% at 39.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 505 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0120000 0.0217800
0.0241700 0.0360600
0.0486500 0.0586200
0.0732700 0.0751900
0.0979600 0.0887500
0.1475500 0.1063900
0.1973000 0.1175400
0.2971100 0.1258300
0.3971100 0.1256300
0.4972400 0.1199400
0.5975000 0.1087400
0.6979100 0.0910500
0.7985000 0.0653700
0.8991800 0.0356800
0.9495900 0.0178400
1.0000000 0.0000000
0.0000000 0.0000000
0.0128700 -.0162000
0.0254700 -.0204100
0.0505800 -.0253400
0.0756300 -.0272600
0.1006400 -.0276900
0.1506000 -.0260400
0.2005000 -.0218900
0.3003100 -.0135900
0.4001800 -.0078000
0.5001800 -.0080000
0.6002600 -.0111900
0.7003000 -.0128900
0.8002700 -.0115900
0.9001600 -.0068000
0.9501000 -.0041500
1.0000000 0.0000000
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Polars for GOE 505 AIRFOIL (goe505-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe505-il | 50,000 | 9 | 12.3 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe505-il | 50,000 | 5 | 29.8 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe505-il | 100,000 | 9 | 49.1 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe505-il | 100,000 | 5 | 43.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe505-il | 200,000 | 9 | 68.7 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe505-il | 200,000 | 5 | 53.8 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe505-il | 500,000 | 9 | 73.5 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe505-il | 500,000 | 5 | 69.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe505-il | 1,000,000 | 9 | 91 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe505-il | 1,000,000 | 5 | 87.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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