GOE 440 AIRFOIL (goe440-il)
GOE 440 AIRFOIL - Gottingen 440 airfoil
| Details | Dat file | Parser | |
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(goe440-il) GOE 440 AIRFOIL Gottingen 440 airfoil Max thickness 15.3% at 30% chord. Max camber 9.7% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 440 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0124900 0.0052200
0.0249700 0.0147500
0.0499000 0.0548900
0.0748300 0.0914400
0.0997800 0.1140900
0.1497300 0.1421800
0.1997000 0.1580800
0.2996800 0.1699700
0.3996800 0.1658600
0.4997100 0.1534500
0.5997500 0.1335400
0.6997899 0.1079300
0.7998500 0.0775200
0.8999200 0.0407100
0.9499600 0.0218000
1.0000000 0.0013000
0.0000000 0.0000000
0.0125100 -.0031800
0.0250100 -.0031500
0.0500100 -.0026000
0.0750000 -.0009600
0.1000000 0.0011900
0.1499900 0.0033800
0.1999900 0.0076800
0.2999700 0.0174700
0.3999500 0.0281600
0.4999300 0.0346500
0.5999200 0.0396400
0.6999199 0.0398300
0.7999300 0.0347200
0.8999600 0.0222100
0.9499800 0.0123000
1.0000000 -.0013000
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Polars for GOE 440 AIRFOIL (goe440-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe440-il | 50,000 | 9 | 9.5 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe440-il | 50,000 | 5 | 31.9 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe440-il | 100,000 | 9 | 53.2 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe440-il | 100,000 | 5 | 52.9 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe440-il | 200,000 | 9 | 71.1 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe440-il | 200,000 | 5 | 67.7 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe440-il | 500,000 | 9 | 92.2 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe440-il | 500,000 | 5 | 86.7 at α=0.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe440-il | 1,000,000 | 9 | 109.5 at α=0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe440-il | 1,000,000 | 5 | 100.3 at α=0.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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