GOE 147 (MVA H.6) AIRFOIL (goe147-il)
GOE 147 (MVA H.6) AIRFOIL - Gottingen 147 (MVA H.6) airfoil
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(goe147-il) GOE 147 (MVA H.6) AIRFOIL Gottingen 147 (MVA H.6) airfoil Max thickness 7.5% at 14.9% chord. Max camber 3.8% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 147 (MVA H.6) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122200 0.0181900
0.0245800 0.0271800
0.0493700 0.0412600
0.0742000 0.0520400
0.0991000 0.0584200
0.1489800 0.0666900
0.1989200 0.0703500
0.2989100 0.0707900
0.3989700 0.0668200
0.4991100 0.0581600
0.5992600 0.0480000
0.6994300 0.0370400
0.7996100 0.0253700
0.8997900 0.0138100
0.9498800 0.0079800
1.0000000 0.0016500
0.0000000 0.0000000
0.0126100 -.0078800
0.0251700 -.0111100
0.0502300 -.0151300
0.0752400 -.0158500
0.1002000 -.0132600
0.1501300 -.0087000
0.2000500 -.0029300
0.2999300 0.0044000
0.3999200 0.0072400
0.4999000 0.0067700
0.5999200 0.0053100
0.6999400 0.0036400
0.7999700 0.0018800
0.8999800 0.0007000
0.9499900 -.0003400
1.0000000 -.0016500
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Polars for GOE 147 (MVA H.6) AIRFOIL (goe147-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe147-il | 50,000 | 9 | 29.2 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe147-il | 50,000 | 5 | 36.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe147-il | 100,000 | 9 | 48.6 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe147-il | 100,000 | 5 | 49.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe147-il | 200,000 | 9 | 64.3 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe147-il | 200,000 | 5 | 66.1 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe147-il | 500,000 | 9 | 86.8 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe147-il | 500,000 | 5 | 86.3 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe147-il | 1,000,000 | 9 | 102.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe147-il | 1,000,000 | 5 | 101.4 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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