GOE 276 (DAIMLER VII) AIRFOIL (goe276-il)
GOE 276 (DAIMLER VII) AIRFOIL - Gottingen 276 (DAIMLER VII) airfoil
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(goe276-il) GOE 276 (DAIMLER VII) AIRFOIL Gottingen 276 (DAIMLER VII) airfoil Max thickness 7.3% at 30% chord. Max camber 4% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 276 (DAIMLER VII) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0124100 0.0173700
0.0248600 0.0265300
0.0497900 0.0396700
0.0747300 0.0496000
0.0997000 0.0563400
0.1496400 0.0665100
0.1996100 0.0723800
0.2995900 0.0766200
0.3996000 0.0734600
0.4996300 0.0692000
0.5996600 0.0623400
0.6997200 0.0526800
0.7997900 0.0387200
0.8998700 0.0232600
0.9499199 0.0152300
1.0000000 0.0040000
0.0000000 0.0000000
0.0125500 -.0088300
0.0250500 -.0087600
0.0500300 -.0061300
0.0750200 -.0040800
0.1000100 -.0024600
0.1500000 -.0005900
0.1999900 0.0010300
0.2999800 0.0040200
0.3999700 0.0061600
0.4999600 0.0067000
0.5999700 0.0061400
0.6999700 0.0050800
0.7999800 0.0029200
0.9000000 0.0002600
0.9500100 -.0021700
1.0000000 -.0040000
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Polars for GOE 276 (DAIMLER VII) AIRFOIL (goe276-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe276-il | 50,000 | 9 | 36.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe276-il | 50,000 | 5 | 40.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe276-il | 100,000 | 9 | 53 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe276-il | 100,000 | 5 | 56.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe276-il | 200,000 | 9 | 72.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe276-il | 200,000 | 5 | 73.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe276-il | 500,000 | 9 | 97.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe276-il | 500,000 | 5 | 93.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe276-il | 1,000,000 | 9 | 114.1 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe276-il | 1,000,000 | 5 | 107.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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