GOE 300 (FRIEDRICHSHAFEN G20) AIRFOIL (goe300-il)
GOE 300 (FRIEDRICHSHAFEN G20) AIRFOIL - Gottingen 300 (Friedrichshafen G20) airfoil
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(goe300-il) GOE 300 (FRIEDRICHSHAFEN G20) AIRFOIL Gottingen 300 (Friedrichshafen G20) airfoil Max thickness 8.4% at 30% chord. Max camber 6.7% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 300 (FRIEDRICHSHAFEN G20) AIRFOIL
14. 14.
0.0000000 0.0000000
0.0250000 0.0389500
0.0500000 0.0566000
0.1000000 0.0784000
0.1500000 0.0915000
0.2000000 0.1015000
0.3000000 0.1090000
0.4000000 0.1078000
0.5000000 0.0989000
0.6000000 0.0854000
0.7000000 0.0685000
0.8000000 0.0485000
0.9000000 0.0256000
1.0000000 0.0018000
0.0000000 0.0000000
0.0250000 -.0097500
0.0500000 -.0080000
0.1000000 0.0030000
0.1500000 0.0125000
0.2000000 0.0186000
0.3000000 0.0247000
0.4000000 0.0245000
0.5000000 0.0215000
0.6000000 0.0173000
0.7000000 0.0130000
0.8000000 0.0086000
0.9000000 0.0040000
1.0000000 0.0000000
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Polars for GOE 300 (FRIEDRICHSHAFEN G20) AIRFOIL (goe300-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe300-il | 50,000 | 9 | 19.9 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe300-il | 50,000 | 5 | 38.1 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe300-il | 100,000 | 9 | 54.9 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe300-il | 100,000 | 5 | 61 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe300-il | 200,000 | 9 | 79.1 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe300-il | 200,000 | 5 | 81.2 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe300-il | 500,000 | 9 | 107.6 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe300-il | 500,000 | 5 | 105.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe300-il | 1,000,000 | 9 | 130.4 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe300-il | 1,000,000 | 5 | 126.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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