GOE 478 AIRFOIL (goe478-il)
GOE 478 AIRFOIL - Gottingen 478 airfoil
| Details | Dat file | Parser | |
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(goe478-il) GOE 478 AIRFOIL Gottingen 478 airfoil Max thickness 13.4% at 29.6% chord. Max camber 4.3% at 39.6% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 478 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0114600 0.0269400
0.0235000 0.0389000
0.0479100 0.0543400
0.0724700 0.0657900
0.0971200 0.0747400
0.1466100 0.0881400
0.1962400 0.0975600
0.2958500 0.1078900
0.3958500 0.1077400
0.4961100 0.1011000
0.5965200 0.0904700
0.6972300 0.0718400
0.7980500 0.0507200
0.8989601 0.0271100
0.9494400 0.0145500
1.0000000 0.0000000
0.0000000 0.0000000
0.0133700 -.0224900
0.0260600 -.0275000
0.0512100 -.0315300
0.0762900 -.0335600
0.1012900 -.0336000
0.1512600 -.0326800
0.2011500 -.0297600
0.3009800 -.0254100
0.4008300 -.0215700
0.5006800 -.0177200
0.6005300 -.0138800
0.7003900 -.0100400
0.8002600 -.0066900
0.9001300 -.0033500
0.9500500 -.0014200
1.0000000 0.0000000
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Polars for GOE 478 AIRFOIL (goe478-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe478-il | 50,000 | 9 | 19.7 at α=12.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe478-il | 50,000 | 5 | 31.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe478-il | 100,000 | 9 | 51.6 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe478-il | 100,000 | 5 | 53 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe478-il | 200,000 | 9 | 73.5 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe478-il | 200,000 | 5 | 71 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe478-il | 500,000 | 9 | 101.3 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe478-il | 500,000 | 5 | 95.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe478-il | 1,000,000 | 9 | 125.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe478-il | 1,000,000 | 5 | 114.8 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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