GOE 462 AIRFOIL (goe462-il)
GOE 462 AIRFOIL - Gottingen 462 airfoil
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(goe462-il) GOE 462 AIRFOIL Gottingen 462 airfoil Max thickness 11% at 9.9% chord. Max camber 13.4% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 462 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123000 0.0265900
0.0246500 0.0466800
0.0494100 0.0788700
0.0742400 0.1010600
0.0991200 0.1177400
0.1489500 0.1396200
0.1988700 0.1509900
0.2988400 0.1552400
0.3989000 0.1469900
0.4990200 0.1307400
0.5991700 0.1104900
0.6993500 0.0867500
0.7995500 0.0595000
0.8997700 0.0312500
0.9498700 0.0171200
1.0000000 0.0000000
0.0000000 0.0000000
0.0125500 -.0064100
0.0250500 -.0073100
0.0500400 -.0056200
0.0750000 -.0004400
0.0999400 0.0082500
0.1497200 0.0371200
0.1994600 0.0720000
0.2991600 0.1122400
0.3991300 0.1159900
0.4992000 0.1062400
0.5993200 0.0904900
0.6994700 0.0707500
0.7996399 0.0485000
0.8998200 0.0242500
0.9499100 0.0126200
1.0000000 0.0000000
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Polars for GOE 462 AIRFOIL (goe462-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe462-il | 50,000 | 9 | 8.9 at α=-0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe462-il | 50,000 | 5 | 29.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe462-il | 100,000 | 9 | 52.3 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe462-il | 100,000 | 5 | 46.4 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe462-il | 200,000 | 9 | 61.2 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe462-il | 200,000 | 5 | 62.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe462-il | 500,000 | 9 | 175.7 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe462-il | 500,000 | 5 | 88.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe462-il | 1,000,000 | 9 | 107.3 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe462-il | 1,000,000 | 5 | 111.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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