GOE 645 AIRFOIL (goe645-il)
GOE 645 AIRFOIL - Gottingen 645 airfoil
| Details | Dat file | Parser | |
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(goe645-il) GOE 645 AIRFOIL Gottingen 645 airfoil Max thickness 15.4% at 19.4% chord. Max camber 4.8% at 39.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 645 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0111200 0.0285400
0.0229300 0.0426100
0.0469300 0.0632800
0.0711700 0.0789500
0.0956800 0.0891400
0.1448600 0.1060300
0.1944000 0.1154300
0.2940700 0.1222600
0.3943000 0.1176200
0.4948600 0.1060000
0.5956400 0.0898900
0.6966200 0.0697900
0.7976600 0.0481900
0.8987600 0.0255900
0.9493400 0.0135400
1.0000000 0.0000000
0.0000000 0.0000000
0.0132900 -.0163600
0.0261000 -.0227300
0.0514800 -.0305000
0.0767400 -.0357800
0.1018500 -.0380600
0.1519500 -.0401300
0.2018800 -.0387100
0.3014500 -.0298800
0.4010000 -.0205500
0.5006400 -.0132200
0.6003600 -.0073800
0.7007000 -.0044300
0.8001100 -.0021900
0.9000400 -.0008500
0.9500200 -.0004200
1.0000000 0.0000000
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Polars for GOE 645 AIRFOIL (goe645-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe645-il | 50,000 | 9 | 9.5 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe645-il | 50,000 | 5 | 28.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe645-il | 100,000 | 9 | 43.7 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe645-il | 100,000 | 5 | 48.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe645-il | 200,000 | 9 | 66.3 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe645-il | 200,000 | 5 | 65.8 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe645-il | 500,000 | 9 | 93.5 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe645-il | 500,000 | 5 | 84.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe645-il | 1,000,000 | 9 | 110.5 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe645-il | 1,000,000 | 5 | 88.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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