GOE 601 AIRFOIL (goe601-il)
GOE 601 AIRFOIL - Gottingen 601 airfoil
| Details | Dat file | Parser | |
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(goe601-il) GOE 601 AIRFOIL Gottingen 601 airfoil Max thickness 16% at 39% chord. Max camber 2.5% at 49% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 601 AIRFOIL
17. 17.
0.0000200 0.0000000
0.0103200 0.0220300
0.0219100 0.0311900
0.0454200 0.0460400
0.0692300 0.0579200
0.0932400 0.0678200
0.1418000 0.0821800
0.1909100 0.0910900
0.2900700 0.0995000
0.3897700 0.1024700
0.4901100 0.0990100
0.5911000 0.0891100
0.6927300 0.0727700
0.7948600 0.0514800
0.8971800 0.0282200
0.9486200 0.0138600
1.0000000 0.0000000
0.0000200 0.0000000
0.0146300 -.0210400
0.0278500 -.0282200
0.0538400 -.0381200
0.0794800 -.0445500
0.1048700 -.0485100
0.1555700 -.0554400
0.2059600 -.0594000
0.3060600 -.0603900
0.4057100 -.0569300
0.5048600 -.0485100
0.6039700 -.0396000
0.7029800 -.0297000
0.8019900 -.0198000
0.9009900 -.0099000
0.9505000 -.0049500
1.0000000 0.0000000
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Polars for GOE 601 AIRFOIL (goe601-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe601-il | 50,000 | 9 | 25.2 at α=11.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe601-il | 50,000 | 5 | 28 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe601-il | 100,000 | 9 | 47.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe601-il | 100,000 | 5 | 44.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe601-il | 200,000 | 9 | 69.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe601-il | 200,000 | 5 | 57.4 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe601-il | 500,000 | 9 | 82.8 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe601-il | 500,000 | 5 | 69 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe601-il | 1,000,000 | 9 | 91.2 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe601-il | 1,000,000 | 5 | 82.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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