GOE 610 B AIRFOIL (goe610b-il)
GOE 610 B AIRFOIL - Gottingen 610 B airfoil
| Details | Dat file | Parser | |
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(goe610b-il) GOE 610 B AIRFOIL Gottingen 610 B airfoil Max thickness 7.8% at 39.9% chord. Max camber 5.3% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 610 B AIRFOIL
16. 16.
0.0000000 0.0000000
0.0148000 0.0201500
0.0495900 0.0405000
0.0744900 0.0507400
0.0994200 0.0579900
0.1492900 0.0714900
0.1991800 0.0800900
0.2991100 0.0887900
0.3990800 0.0919900
0.4991500 0.0854900
0.5992800 0.0744900
0.6994000 0.0599900
0.7995900 0.0410000
0.8997800 0.0220000
0.9498900 0.0115000
1.0000000 0.0000000
0.0000000 0.0000000
0.0151000 -.0098500
0.0500800 -.0085000
0.0750600 -.0062500
0.1000300 -.0028000
0.1499600 0.0031000
0.1999300 0.0070000
0.2998800 0.0122000
0.3998600 0.0140000
0.4998600 0.0140000
0.5998900 0.0120000
0.6999100 0.0090000
0.7999600 0.0045000
0.9000000 0.0000000
0.9500100 -.0005000
1.0000000 0.0000000
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Polars for GOE 610 B AIRFOIL (goe610b-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe610b-il | 50,000 | 9 | 37.4 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe610b-il | 50,000 | 5 | 38.8 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe610b-il | 100,000 | 9 | 61.2 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe610b-il | 100,000 | 5 | 62.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe610b-il | 200,000 | 9 | 86.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe610b-il | 200,000 | 5 | 84 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe610b-il | 500,000 | 9 | 118 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe610b-il | 500,000 | 5 | 95.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe610b-il | 1,000,000 | 9 | 132.2 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe610b-il | 1,000,000 | 5 | 99.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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