GOE 776 AIRFOIL (goe776-il)
GOE 776 AIRFOIL - Gottingen 776 airfoil
| Details | Dat file | Parser | |
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(goe776-il) GOE 776 AIRFOIL Gottingen 776 airfoil Max thickness 25% at 30% chord. Max camber 0% at 60% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 776 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0395300
0.0250000 0.0545700
0.0500000 0.0741300
0.0750000 0.0876900
0.1000000 0.0977600
0.1500000 0.1116900
0.2000000 0.1200200
0.3000000 0.1257800
0.4000000 0.1218400
0.5000000 0.1116000
0.6000000 0.0965600
0.7000000 0.0781200
0.8000000 0.0567800
0.9000000 0.0325400
0.9500000 0.0192700
1.0000000 0.0052000
0.0000000 0.0000000
0.0125000 -.0394700
0.0250000 -.0544400
0.0500000 -.0738700
0.0750000 -.0873100
0.1000000 -.0972400
0.1500000 -.1109100
0.2000000 -.1189800
0.3000000 -.1242200
0.4000000 -.1197600
0.5000000 -.1090000
0.6000000 -.0934400
0.7000000 -.0744800
0.8000000 -.0526200
0.9000000 -.0278600
0.9500000 -.0143300
1.0000000 0.0000000
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Polars for GOE 776 AIRFOIL (goe776-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe776-il | 50,000 | 9 | 6.6 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe776-il | 50,000 | 5 | 19.2 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe776-il | 100,000 | 9 | 33.3 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe776-il | 100,000 | 5 | 28.8 at α=10.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe776-il | 200,000 | 9 | 41.2 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe776-il | 200,000 | 5 | 35.1 at α=10° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe776-il | 500,000 | 9 | 50 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe776-il | 500,000 | 5 | 48.5 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe776-il | 1,000,000 | 9 | 66.3 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe776-il | 1,000,000 | 5 | 61.4 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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