GOE 587 AIRFOIL (goe587-il)
GOE 587 AIRFOIL - Gottingen 587 airfoil
| Details | Dat file | Parser | |
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(goe587-il) GOE 587 AIRFOIL Gottingen 587 airfoil Max thickness 5.8% at 40% chord. Max camber 3% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 587 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125500 0.0104400
0.0250700 0.0148900
0.0501000 0.0227700
0.0751300 0.0296600
0.1001600 0.0350500
0.1502000 0.0448200
0.2002300 0.0516000
0.3002600 0.0581500
0.4002600 0.0582000
0.5002400 0.0527500
0.6002000 0.0453000
0.7001899 0.0354100
0.8001100 0.0249000
0.9000599 0.0134500
0.9500300 0.0077200
1.0000000 0.0000000
0.0000000 0.0000000
0.0124800 -.0050600
0.0249700 -.0061100
0.0499700 -.0057200
0.0749800 -.0048400
0.0999800 -.0034500
0.1500100 -.0013200
0.2000000 0.0001000
0.3000100 0.0011500
0.4000000 0.0002000
0.4999800 -.0037500
0.5999700 -.0067000
0.6999600 -.0091500
0.7999600 -.0091000
0.8999800 -.0045500
0.9499900 -.0017700
1.0000000 0.0000000
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Polars for GOE 587 AIRFOIL (goe587-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe587-il | 50,000 | 9 | 36.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe587-il | 50,000 | 5 | 37 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe587-il | 100,000 | 9 | 50.1 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe587-il | 100,000 | 5 | 50.7 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe587-il | 200,000 | 9 | 63.5 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe587-il | 200,000 | 5 | 62.9 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe587-il | 500,000 | 9 | 77.8 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe587-il | 500,000 | 5 | 70.7 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe587-il | 1,000,000 | 9 | 77.9 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe587-il | 1,000,000 | 5 | 77.1 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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