GOE 679 AIRFOIL (goe679-il)
GOE 679 AIRFOIL - Gottingen 679 airfoil
| Details | Dat file | Parser | |
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(goe679-il) GOE 679 AIRFOIL Gottingen 679 airfoil Max thickness 18.3% at 29.1% chord. Max camber 4.5% at 39.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 679 AIRFOIL
17. 17.
0.0000100 0.0000000
0.0103800 0.0312100
0.0218100 0.0469800
0.0452400 0.0700800
0.0691800 0.0857000
0.0933200 0.0983400
0.1421400 0.1156600
0.1914400 0.1260200
0.2908400 0.1347800
0.3910200 0.1320900
0.4916400 0.1229300
0.5926000 0.1088000
0.6939400 0.0891900
0.7955101 0.0660900
0.8973500 0.0390200
0.9484000 0.0214900
1.0000000 0.0000000
0.0000100 0.0000000
0.0142800 -.0260300
0.0272900 -.0336400
0.0529200 -.0429000
0.0783100 -.0486700
0.1035400 -.0519600
0.1536800 -.0540500
0.2036200 -.0531500
0.3032300 -.0473800
0.4027600 -.0406100
0.5023000 -.0338400
0.6018400 -.0270700
0.7013800 -.0203100
0.8009200 -.0135400
0.9004600 -.0067700
0.9502300 -.0033800
1.0000000 0.0000000
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Polars for GOE 679 AIRFOIL (goe679-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe679-il | 50,000 | 9 | 5.4 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe679-il | 50,000 | 5 | 25.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe679-il | 100,000 | 9 | 42.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe679-il | 100,000 | 5 | 41.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe679-il | 200,000 | 9 | 58.1 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe679-il | 200,000 | 5 | 54.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe679-il | 500,000 | 9 | 76.3 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe679-il | 500,000 | 5 | 72.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe679-il | 1,000,000 | 9 | 95.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe679-il | 1,000,000 | 5 | 88.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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