GOE 629 AIRFOIL (goe629-il)
GOE 629 AIRFOIL - Gottingen 629 airfoil
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(goe629-il) GOE 629 AIRFOIL Gottingen 629 airfoil Max thickness 13.6% at 29.4% chord. Max camber 2.8% at 39.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 629 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0111100 0.0231700
0.0230600 0.0323800
0.0472200 0.0463300
0.0716300 0.0563000
0.0961500 0.0642700
0.1454300 0.0762300
0.1949200 0.0846900
0.2944400 0.0926700
0.3943800 0.0936600
0.4947400 0.0876800
0.5953400 0.0777200
0.6961700 0.0637700
0.7972500 0.0458300
0.8985400 0.0244100
0.9492500 0.0124600
1.0000000 0.0000000
0.0000000 0.0000000
0.0136800 -.0196800
0.0267100 -.0284000
0.0523000 -.0383600
0.0776000 -.0433400
0.1027800 -.0463300
0.1528700 -.0478300
0.2028400 -.0473300
0.3026000 -.0433400
0.4022700 -.0378600
0.5019100 -.0318900
0.6015600 -.0259100
0.7012000 -.0199300
0.8008100 -.0134500
0.9004200 -.0069700
0.9502100 -.0034900
1.0000000 0.0000000
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Polars for GOE 629 AIRFOIL (goe629-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe629-il | 50,000 | 9 | 29.4 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe629-il | 50,000 | 5 | 32.2 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe629-il | 100,000 | 9 | 50.3 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe629-il | 100,000 | 5 | 50.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe629-il | 200,000 | 9 | 70 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe629-il | 200,000 | 5 | 66.2 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe629-il | 500,000 | 9 | 94.7 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe629-il | 500,000 | 5 | 81.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe629-il | 1,000,000 | 9 | 107.2 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe629-il | 1,000,000 | 5 | 92.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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