GOE 457 AIRFOIL (goe457-il)
GOE 457 AIRFOIL - Gottingen 457 airfoil
| Details | Dat file | Parser | |
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(goe457-il) GOE 457 AIRFOIL Gottingen 457 airfoil Max thickness 7.8% at 19.9% chord. Max camber 4.2% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 457 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122800 0.0193400
0.0246500 0.0302800
0.0495100 0.0432600
0.0744100 0.0519500
0.0993300 0.0587300
0.1492100 0.0693000
0.1991400 0.0755700
0.2990900 0.0799100
0.3991200 0.0772500
0.4991900 0.0706900
0.5992800 0.0629300
0.6994000 0.0526700
0.7995500 0.0397100
0.8997500 0.0217600
0.9498600 0.0119300
1.0000000 0.0000000
0.0000000 0.0000000
0.0126000 -.0087600
0.0251200 -.0102100
0.0501200 -.0108300
0.0751100 -.0096400
0.1000900 -.0082600
0.1500700 -.0058900
0.2000300 -.0027200
0.2999600 0.0035200
0.3999200 0.0071600
0.4998900 0.0096000
0.5998900 0.0094400
0.6999100 0.0082800
0.7999300 0.0061200
0.8999600 0.0033600
0.9499800 0.0014300
1.0000000 0.0000000
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Polars for GOE 457 AIRFOIL (goe457-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe457-il | 50,000 | 9 | 34.5 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe457-il | 50,000 | 5 | 40.1 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe457-il | 100,000 | 9 | 54.5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe457-il | 100,000 | 5 | 56.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe457-il | 200,000 | 9 | 73.6 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe457-il | 200,000 | 5 | 72.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe457-il | 500,000 | 9 | 98.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe457-il | 500,000 | 5 | 93.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe457-il | 1,000,000 | 9 | 117 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe457-il | 1,000,000 | 5 | 108.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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