GOE 624 AIRFOIL (goe624-il)
GOE 624 AIRFOIL - Gottingen 624 airfoil
| Details | Dat file | Parser | |
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(goe624-il) GOE 624 AIRFOIL Gottingen 624 airfoil Max thickness 16% at 30% chord. Max camber 5.2% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 624 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0320000
0.0250000 0.0460000
0.0500000 0.0660000
0.0750000 0.0805000
0.1000000 0.0925000
0.1500000 0.1095000
0.2000000 0.1210000
0.3000000 0.1320000
0.4000000 0.1300000
0.5000000 0.1205000
0.6000000 0.1040000
0.7000000 0.0830000
0.8000000 0.0580000
0.9000000 0.0315000
0.9500000 0.0180000
1.0000000 0.0050000
0.0000000 0.0000000
0.0125000 -.0170000
0.0250000 -.0225000
0.0500000 -.0285000
0.0750000 -.0310000
0.1000000 -.0320000
0.1500000 -.0325000
0.2000000 -.0315000
0.3000000 -.0280000
0.4000000 -.0240000
0.5000000 -.0200000
0.6000000 -.0160000
0.7000000 -.0120000
0.8000000 -.0080000
0.9000000 -.0040000
0.9500000 -.0020000
1.0000000 0.0000000
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Polars for GOE 624 AIRFOIL (goe624-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe624-il | 50,000 | 9 | 5.9 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe624-il | 50,000 | 5 | 22.8 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe624-il | 100,000 | 9 | 39.8 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe624-il | 100,000 | 5 | 50.2 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe624-il | 200,000 | 9 | 69.1 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe624-il | 200,000 | 5 | 69.9 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe624-il | 500,000 | 9 | 99.5 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe624-il | 500,000 | 5 | 97.6 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe624-il | 1,000,000 | 9 | 126.9 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe624-il | 1,000,000 | 5 | 120.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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