GOE 394 AIRFOIL (goe394-il)
GOE 394 AIRFOIL - Gottingen 394 airfoil
| Details | Dat file | Parser | |
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(goe394-il) GOE 394 AIRFOIL Gottingen 394 airfoil Max thickness 6.1% at 19.9% chord. Max camber 5.9% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 394 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123000 0.0181400
0.0247000 0.0267800
0.0495500 0.0395600
0.0744500 0.0488400
0.0993700 0.0561200
0.1492300 0.0681800
0.1991400 0.0767400
0.2990500 0.0848600
0.3990500 0.0846900
0.4991000 0.0801100
0.5992000 0.0709400
0.6993901 0.0538700
0.7995900 0.0368000
0.8997900 0.0186200
0.9499000 0.0091900
1.0000000 0.0007500
0.0000000 0.0000000
0.0126100 -.0098600
0.0251300 -.0112200
0.0501200 -.0106400
0.0750800 -.0069600
0.1000100 -.0008700
0.1499100 0.0081900
0.1998200 0.0157500
0.2997000 0.0268700
0.3996300 0.0330000
0.4996000 0.0356200
0.5996100 0.0345500
0.6997200 0.0245700
0.7998300 0.0154000
0.8999299 0.0066200
0.9499800 0.0021900
1.0000000 -.0007500
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Polars for GOE 394 AIRFOIL (goe394-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe394-il | 50,000 | 9 | 40.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe394-il | 50,000 | 5 | 44.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe394-il | 100,000 | 9 | 64.4 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe394-il | 100,000 | 5 | 66.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe394-il | 200,000 | 9 | 90.5 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe394-il | 200,000 | 5 | 85.9 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe394-il | 500,000 | 9 | 116.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe394-il | 500,000 | 5 | 108 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe394-il | 1,000,000 | 9 | 139.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe394-il | 1,000,000 | 5 | 112.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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