GOE 15 AIRFOIL (goe15-il)
GOE 15 AIRFOIL - Gottingen 15 airfoil
| Details | Dat file | Parser | |
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(goe15-il) GOE 15 AIRFOIL Gottingen 15 airfoil Max thickness 9% at 29.8% chord. Max camber 7.8% at 29.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 15 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0120800 0.0273800
0.0243600 0.0417700
0.0490500 0.0621500
0.0738200 0.0768300
0.0986500 0.0882100
0.1484100 0.1039700
0.1982500 0.1144300
0.2981200 0.1225600
0.3982000 0.1182900
0.4983300 0.1090200
0.5985600 0.0938600
0.6988800 0.0733900
0.7992100 0.0519300
0.8995900 0.0269600
0.9497800 0.0142300
1.0000000 0.0000000
0.0000000 0.0000000
0.0127100 -.0136100
0.0252300 -.0149100
0.0500800 -.0050300
0.0749300 0.0048500
0.0998100 0.0127300
0.1496500 0.0229900
0.1995800 0.0277500
0.2995000 0.0325800
0.3995300 0.0308100
0.4995800 0.0273400
0.5996900 0.0205800
0.6998100 0.0121100
0.7999000 0.0062400
0.8999800 0.0014700
0.9499900 0.0005300
1.0000000 0.0000000
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Polars for GOE 15 AIRFOIL (goe15-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe15-il | 50,000 | 9 | 8.7 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe15-il | 50,000 | 5 | 31.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe15-il | 100,000 | 9 | 46.6 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe15-il | 100,000 | 5 | 53.4 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe15-il | 200,000 | 9 | 70.7 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe15-il | 200,000 | 5 | 72.4 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe15-il | 500,000 | 9 | 126.4 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe15-il | 500,000 | 5 | 94.3 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe15-il | 1,000,000 | 9 | 128.7 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe15-il | 1,000,000 | 5 | 115.3 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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