GOE 301 (FRIEDRICHSHAFEN G 13) AIRFOIL (goe301-il)
GOE 301 (FRIEDRICHSHAFEN G 13) AIRFOIL - Gottingen 301 (Friedrichshafen G 13) airfoil
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(goe301-il) GOE 301 (FRIEDRICHSHAFEN G 13) AIRFOIL Gottingen 301 (Friedrichshafen G 13) airfoil Max thickness 10% at 28.9% chord. Max camber 6.5% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 301 (FRIEDRICHSHAFEN G 13) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122200 0.0274200
0.0246000 0.0395500
0.0494200 0.0573000
0.0742800 0.0710600
0.0991800 0.0808100
0.1490200 0.0958200
0.1989300 0.1053300
0.2886400 0.1137400
0.3988500 0.1123700
0.4989400 0.1043900
0.5990800 0.0904100
0.6992500 0.0734300
0.7994400 0.0544500
0.8996800 0.0309800
0.9498200 0.0179900
1.0000000 0.0015000
0.0000000 0.0000000
0.0126000 -.0100700
0.0251200 -.0114400
0.0500900 -.0086900
0.0750500 -.0044300
0.1000100 -.0011800
0.1499600 0.0043300
0.1999100 0.0090400
0.2998500 0.0148600
0.3998200 0.0173800
0.4998200 0.0179000
0.5998200 0.0174200
0.6998500 0.0144400
0.7998900 0.0104600
0.8999400 0.0054800
0.9499800 0.0016900
1.0000000 -.0015000
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Polars for GOE 301 (FRIEDRICHSHAFEN G 13) AIRFOIL (goe301-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe301-il | 50,000 | 9 | 19 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe301-il | 50,000 | 5 | 38.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe301-il | 100,000 | 9 | 55.7 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe301-il | 100,000 | 5 | 61.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe301-il | 200,000 | 9 | 81.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe301-il | 200,000 | 5 | 81.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe301-il | 500,000 | 9 | 112.7 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe301-il | 500,000 | 5 | 108.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe301-il | 1,000,000 | 9 | 138.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe301-il | 1,000,000 | 5 | 128.3 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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