GOE 8K AIRFOIL (goe08k-il)
GOE 8K AIRFOIL - Gottingen 8K airfoil
| Details | Dat file | Parser | |
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(goe08k-il) GOE 8K AIRFOIL Gottingen 8K airfoil Max thickness 14.9% at 50% chord. Max camber 6.1% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 8K AIRFOIL
16. 16.
0.0000000 0.0000000
0.0250000 0.0311200
0.0500000 0.0463500
0.0750000 0.0583700
0.1000000 0.0691900
0.1500000 0.0865300
0.2000000 0.1000800
0.3000000 0.1202700
0.4000000 0.1316600
0.5000000 0.1355500
0.6000000 0.1321400
0.7000000 0.1175300
0.8000000 0.0925200
0.9000000 0.0553100
0.9500000 0.0320500
1.0000000 0.0000000
0.0000000 0.0000000
0.0250000 -.0140800
0.0500000 -.0158600
0.0750000 -.0164300
0.1000000 -.0175100
0.1500000 -.0184700
0.2000000 -.0180200
0.3000000 -.0163300
0.4000000 -.0146400
0.5000000 -.0129500
0.6000000 -.0112600
0.7000000 -.0095700
0.8000000 -.0078800
0.9000000 -.0061900
0.9500000 -.0053500
1.0000000 0.0000000
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Polars for GOE 8K AIRFOIL (goe08k-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe08k-il | 50,000 | 9 | 18 at α=14° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe08k-il | 50,000 | 5 | 15.7 at α=12.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe08k-il | 100,000 | 9 | 26.9 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe08k-il | 100,000 | 5 | 24.1 at α=11.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe08k-il | 200,000 | 9 | 44.4 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe08k-il | 200,000 | 5 | 43.5 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe08k-il | 500,000 | 9 | 103.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe08k-il | 500,000 | 5 | 96.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe08k-il | 1,000,000 | 9 | 143.1 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe08k-il | 1,000,000 | 5 | 122 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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