GOE 399 AIRFOIL (goe399-il)
GOE 399 AIRFOIL - Gottingen 399 airfoil
| Details | Dat file | Parser | |
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(goe399-il) GOE 399 AIRFOIL Gottingen 399 airfoil Max thickness 6.9% at 29.9% chord. Max camber 4.2% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 399 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123800 0.0156000
0.0248000 0.0232000
0.0497300 0.0334000
0.0746600 0.0421000
0.0996100 0.0493000
0.1495100 0.0612000
0.1994500 0.0686000
0.2993900 0.0759000
0.3994000 0.0752000
0.4994400 0.0705000
0.5995100 0.0613000
0.6996100 0.0486000
0.7997200 0.0344000
0.8998500 0.0182000
0.9499300 0.0091000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125600 -.0079000
0.0250700 -.0093000
0.0500700 -.0086000
0.0750500 -.0064000
0.1000500 -.0043700
0.1500100 -.0008000
0.1999800 0.0026000
0.2999400 0.0069000
0.3999300 0.0092000
0.4999200 0.0100000
0.5999200 0.0098000
0.6999400 0.0071000
0.7999600 0.0049000
0.8999900 0.0017000
0.9500000 0.0001000
1.0000000 0.0000000
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Polars for GOE 399 AIRFOIL (goe399-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe399-il | 50,000 | 9 | 40.8 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe399-il | 50,000 | 5 | 41.9 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe399-il | 100,000 | 9 | 59.4 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe399-il | 100,000 | 5 | 60.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe399-il | 200,000 | 9 | 79.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe399-il | 200,000 | 5 | 76.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe399-il | 500,000 | 9 | 104.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe399-il | 500,000 | 5 | 98.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe399-il | 1,000,000 | 9 | 124.1 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe399-il | 1,000,000 | 5 | 112.4 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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