GOE 474 AIRFOIL (goe474-il)
GOE 474 AIRFOIL - Gottingen 474 airfoil
| Details | Dat file | Parser | |
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(goe474-il) GOE 474 AIRFOIL Gottingen 474 airfoil Max thickness 7% at 30% chord. Max camber 2.9% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 474 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0157400
0.0250000 0.0229900
0.0500000 0.0329700
0.0750000 0.0394600
0.1000000 0.0444500
0.1500000 0.0514200
0.2000000 0.0564000
0.3000000 0.0618500
0.4000000 0.0633000
0.5000000 0.0617500
0.6000000 0.0552000
0.7000000 0.0451500
0.8000000 0.0321000
0.9000000 0.0170500
0.9500000 0.0090200
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0092600
0.0250000 -.0125100
0.0500000 -.0165300
0.0750000 -.0180400
0.1000000 -.0175500
0.1500000 -.0145700
0.2000000 -.0116000
0.3000000 -.0076500
0.4000000 -.0052000
0.5000000 -.0037500
0.6000000 -.0038000
0.7000000 -.0033500
0.8000000 -.0034000
0.9000000 -.0019500
0.9500000 -.0009700
1.0000000 0.0000000
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Polars for GOE 474 AIRFOIL (goe474-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe474-il | 50,000 | 9 | 38.4 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe474-il | 50,000 | 5 | 38.3 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe474-il | 100,000 | 9 | 57 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe474-il | 100,000 | 5 | 54.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe474-il | 200,000 | 9 | 77.1 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe474-il | 200,000 | 5 | 70.1 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe474-il | 500,000 | 9 | 101.6 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe474-il | 500,000 | 5 | 85.1 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe474-il | 1,000,000 | 9 | 115.8 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe474-il | 1,000,000 | 5 | 91 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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