GOE 622 AIRFOIL (goe622-il)
GOE 622 AIRFOIL - Gottingen 622 airfoil
| Details | Dat file | Parser | |
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(goe622-il) GOE 622 AIRFOIL Gottingen 622 airfoil Max thickness 8% at 30% chord. Max camber 2.4% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 622 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0138000
0.0250000 0.0216000
0.0500000 0.0317000
0.0750000 0.0393000
0.1000000 0.0444000
0.1500000 0.0526000
0.2000000 0.0578000
0.3000000 0.0632000
0.4000000 0.0636000
0.5000000 0.0590000
0.6000000 0.0519000
0.7000000 0.0428000
0.8000000 0.0307000
0.9000000 0.0171000
0.9500000 0.0103000
1.0000000 0.0020000
0.0000000 0.0000000
0.0125000 -.0092000
0.0250000 -.0129000
0.0500000 -.0168000
0.0750000 -.0187000
0.1000000 -.0191000
0.1500000 -.0192000
0.2000000 -.0187000
0.3000000 -.0168000
0.4000000 -.0144000
0.5000000 -.0120000
0.6000000 -.0096000
0.7000000 -.0072000
0.8000000 -.0048000
0.9000000 -.0024000
0.9500000 -.0012000
1.0000000 0.0000000
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Polars for GOE 622 AIRFOIL (goe622-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe622-il | 50,000 | 9 | 35.5 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe622-il | 50,000 | 5 | 38.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe622-il | 100,000 | 9 | 53.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe622-il | 100,000 | 5 | 52.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe622-il | 200,000 | 9 | 69.8 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe622-il | 200,000 | 5 | 64.9 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe622-il | 500,000 | 9 | 88.5 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe622-il | 500,000 | 5 | 75.5 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe622-il | 1,000,000 | 9 | 98.6 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe622-il | 1,000,000 | 5 | 82 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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