GOE 6K AIRFOIL (goe06k-il)
GOE 6K AIRFOIL - Gottingen 6K airfoil
| Details | Dat file | Parser | |
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(goe06k-il) GOE 6K AIRFOIL Gottingen 6K airfoil Max thickness 7.5% at 50% chord. Max camber 3.1% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 6K AIRFOIL
16. 16.
0.0000000 0.0000000
0.0250000 0.0157100
0.0500000 0.0234300
0.0750000 0.0295400
0.1000000 0.0349600
0.1500000 0.0436900
0.2000000 0.0506200
0.3000000 0.0607800
0.4000000 0.0665400
0.5000000 0.0685000
0.6000000 0.0668600
0.7000000 0.0594200
0.8000000 0.0467800
0.9000000 0.0279400
0.9500000 0.0162700
1.0000000 0.0000000
0.0000000 0.0000000
0.0250000 -.0070900
0.0500000 -.0079700
0.0750000 -.0085500
0.1000000 -.0088400
0.1500000 -.0093100
0.2000000 -.0090800
0.3000000 -.0082200
0.4000000 -.0073600
0.5000000 -.0065000
0.6000000 -.0056400
0.7000000 -.0047800
0.8000000 -.0039200
0.9000000 -.0030600
0.9500000 -.0026300
1.0000000 0.0000000
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Polars for GOE 6K AIRFOIL (goe06k-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe06k-il | 50,000 | 9 | 26.4 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe06k-il | 50,000 | 5 | 28.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe06k-il | 100,000 | 9 | 45.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe06k-il | 100,000 | 5 | 44.6 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe06k-il | 200,000 | 9 | 74.4 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe06k-il | 200,000 | 5 | 77 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe06k-il | 500,000 | 9 | 117.9 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe06k-il | 500,000 | 5 | 116.5 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe06k-il | 1,000,000 | 9 | 147.6 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe06k-il | 1,000,000 | 5 | 132.8 at α=1.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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