GOE 585 AIRFOIL (goe585-il)
GOE 585 AIRFOIL - Gottingen 585 airfoil
| Details | Dat file | Parser | |
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(goe585-il) GOE 585 AIRFOIL Gottingen 585 airfoil Max thickness 8.2% at 20% chord. Max camber 3.4% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 585 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0187300
0.0250000 0.0274600
0.0500000 0.0394300
0.0750000 0.0483900
0.1000000 0.0553500
0.1500000 0.0642700
0.2000000 0.0692000
0.3000000 0.0725500
0.4000000 0.0714000
0.5000000 0.0672500
0.6000000 0.0591000
0.7000000 0.0479500
0.8000000 0.0348000
0.9000000 0.0186500
0.9500000 0.0100800
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0112700
0.0250000 -.0140400
0.0500000 -.0165800
0.0750000 -.0171100
0.1000000 -.0166500
0.1500000 -.0147200
0.2000000 -.0128000
0.3000000 -.0079500
0.4000000 -.0041000
0.5000000 -.0022500
0.6000000 -.0014000
0.7000000 -.0010500
0.8000000 -.0017000
0.9000000 -.0008500
0.9500000 -.0004300
1.0000000 0.0000000
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Polars for GOE 585 AIRFOIL (goe585-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe585-il | 50,000 | 9 | 34.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe585-il | 50,000 | 5 | 37.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe585-il | 100,000 | 9 | 52.7 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe585-il | 100,000 | 5 | 51 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe585-il | 200,000 | 9 | 70.3 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe585-il | 200,000 | 5 | 66.1 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe585-il | 500,000 | 9 | 90.4 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe585-il | 500,000 | 5 | 87.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe585-il | 1,000,000 | 9 | 108.2 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe585-il | 1,000,000 | 5 | 104.5 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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