GOE 549 AIRFOIL (goe549-il)
GOE 549 AIRFOIL - Gottingen 549 airfoil
| Details | Dat file | Parser | |
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(goe549-il) GOE 549 AIRFOIL Gottingen 549 airfoil Max thickness 13.9% at 30% chord. Max camber 4.7% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 549 AIRFOIL
21. 21.
0.0000000 0.0000000
0.0020000 0.0085700
0.0040000 0.0124400
0.0060000 0.0151100
0.0080000 0.0179800
0.0125000 0.0229300
0.0250000 0.0343600
0.0500000 0.0517300
0.0750000 0.0645900
0.1000000 0.0759500
0.1500000 0.0931800
0.2000000 0.1044000
0.3000000 0.1143500
0.4000000 0.1133000
0.5000000 0.1032500
0.6000000 0.0867000
0.7000000 0.0686500
0.8000000 0.0466000
0.9000000 0.0235500
0.9500000 0.0122700
1.0000000 0.0000000
0.0000000 0.0000000
0.0020000 -.0058300
0.0040000 -.0087600
0.0060000 -.0105900
0.0080000 -.0120200
0.0125000 -.0145200
0.0250000 -.0176400
0.0500000 -.0217800
0.0750000 -.0244100
0.1000000 -.0255500
0.1500000 -.0268200
0.2000000 -.0271000
0.3000000 -.0241500
0.4000000 -.0197000
0.5000000 -.0142500
0.6000000 -.0083000
0.7000000 -.0038500
0.8000000 -.0014000
0.9000000 -.0004500
0.9500000 -.0002300
1.0000000 0.0000000
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Polars for GOE 549 AIRFOIL (goe549-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe549-il | 50,000 | 9 | 7.6 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe549-il | 50,000 | 5 | 26.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe549-il | 100,000 | 9 | 43 at α=11.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe549-il | 100,000 | 5 | 52.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe549-il | 200,000 | 9 | 74.4 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe549-il | 200,000 | 5 | 75.7 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe549-il | 500,000 | 9 | 107.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe549-il | 500,000 | 5 | 100.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe549-il | 1,000,000 | 9 | 128.7 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe549-il | 1,000,000 | 5 | 115.8 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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