GOE 441 AIRFOIL (goe441-il)
GOE 441 AIRFOIL - Gottingen 441 airfoil
| Details | Dat file | Parser | |
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(goe441-il) GOE 441 AIRFOIL Gottingen 441 airfoil Max thickness 16% at 29.5% chord. Max camber 7.7% at 39.5% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 441 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0115900 0.0296500
0.0236800 0.0433200
0.0479700 0.0663700
0.0723600 0.0863100
0.0969000 0.1013600
0.1462100 0.1241700
0.1957500 0.1389800
0.2953400 0.1526200
0.3954200 0.1498800
0.4958000 0.1375500
0.5962800 0.1219200
0.6969900 0.0983900
0.7978500 0.0704700
0.8988301 0.0381600
0.9493800 0.0203000
1.0000000 0.0013500
0.0000000 0.0000000
0.0131400 -.0209000
0.0257900 -.0258100
0.0508900 -.0292500
0.0759000 -.0295800
0.1008500 -.0277200
0.1507300 -.0238000
0.2005400 -.0177700
0.3002100 -.0067300
0.3998400 0.0051200
0.4995000 0.0163600
0.5992800 0.0236100
0.6991900 0.0266600
0.7992401 0.0249200
0.8995600 0.0143800
0.9497600 0.0077200
1.0000000 -.0013500
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Polars for GOE 441 AIRFOIL (goe441-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe441-il | 50,000 | 9 | 6 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe441-il | 50,000 | 5 | 31 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe441-il | 100,000 | 9 | 45.6 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe441-il | 100,000 | 5 | 52 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe441-il | 200,000 | 9 | 67 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe441-il | 200,000 | 5 | 72.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe441-il | 500,000 | 9 | 102 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe441-il | 500,000 | 5 | 101.7 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe441-il | 1,000,000 | 9 | 132.4 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe441-il | 1,000,000 | 5 | 126.9 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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