GOE 767 AIRFOIL (goe767-il)
GOE 767 AIRFOIL - Gottingen 767 airfoil
| Details | Dat file | Parser | |
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(goe767-il) GOE 767 AIRFOIL Gottingen 767 airfoil Max thickness 12% at 20% chord. Max camber 1.5% at 20% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 767 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0299000
0.0250000 0.0400000
0.0500000 0.0533000
0.1000000 0.0672000
0.1500000 0.0738000
0.2000000 0.0750000
0.2500000 0.0737000
0.3000000 0.0705000
0.4000000 0.0609000
0.5000000 0.0498000
0.6000000 0.0390000
0.7000000 0.0294000
0.8000000 0.0197000
0.9000000 0.0097000
0.9500000 0.0050000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0190000
0.0250000 -.0260000
0.0500000 -.0348000
0.1000000 -.0420000
0.1500000 -.0444000
0.2000000 -.0450000
0.2500000 -.0452000
0.3000000 -.0443000
0.4000000 -.0410000
0.5000000 -.0364000
0.6000000 -.0306000
0.7000000 -.0236000
0.8000000 -.0162000
0.9000000 -.0084000
0.9500000 -.0042000
1.0000000 0.0000000
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Polars for GOE 767 AIRFOIL (goe767-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe767-il | 50,000 | 9 | 15.5 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe767-il | 50,000 | 5 | 23.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe767-il | 100,000 | 9 | 30.3 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe767-il | 100,000 | 5 | 38.6 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe767-il | 200,000 | 9 | 49.7 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe767-il | 200,000 | 5 | 54.9 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe767-il | 500,000 | 9 | 76 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe767-il | 500,000 | 5 | 74.7 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe767-il | 1,000,000 | 9 | 93.1 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe767-il | 1,000,000 | 5 | 91.5 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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