GOE 346 (FRIEDRICHSHAFEN-STAAKEN) AIRFOIL (goe346-il)
GOE 346 (FRIEDRICHSHAFEN-STAAKEN) AIRFOIL - Gottingen 346 (Friedrichshafen-Staaken) airfoil
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(goe346-il) GOE 346 (FRIEDRICHSHAFEN-STAAKEN) AIRFOIL Gottingen 346 (Friedrichshafen-Staaken) airfoil Max thickness 5.7% at 39.9% chord. Max camber 3.8% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 346 (FRIEDRICHSHAFEN-STAAKEN) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123600 0.0166000
0.0248100 0.0231100
0.0497200 0.0339200
0.0746500 0.0416200
0.0996000 0.0477300
0.1495400 0.0556500
0.1994900 0.0606700
0.2994500 0.0658000
0.3994400 0.0666400
0.4994700 0.0631700
0.5995300 0.0566100
0.6996100 0.0463400
0.7997200 0.0335800
0.8998500 0.0181100
0.9499100 0.0103300
1.0000000 0.0017500
0.0000000 0.0000000
0.0125800 -.0099900
0.0250800 -.0093900
0.0500400 -.0046800
0.0750100 -.0014700
0.0999900 0.0013300
0.1499500 0.0055500
0.1999400 0.0075700
0.2999200 0.0096000
0.3999200 0.0092400
0.4999400 0.0073700
0.5999500 0.0055100
0.6999700 0.0037400
0.7999800 0.0018800
0.9000000 0.0001100
0.9500100 -.0010700
1.0000000 -.0017500
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Polars for GOE 346 (FRIEDRICHSHAFEN-STAAKEN) AIRFOIL (goe346-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe346-il | 50,000 | 9 | 40.3 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe346-il | 50,000 | 5 | 42.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe346-il | 100,000 | 9 | 61.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe346-il | 100,000 | 5 | 59.5 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe346-il | 200,000 | 9 | 81.2 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe346-il | 200,000 | 5 | 72.8 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe346-il | 500,000 | 9 | 95.5 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe346-il | 500,000 | 5 | 83 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe346-il | 1,000,000 | 9 | 100.8 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe346-il | 1,000,000 | 5 | 91.1 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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