GOE 408 AIRFOIL (goe408-il)
GOE 408 AIRFOIL - Gottingen 408 airfoil
| Details | Dat file | Parser | |
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(goe408-il) GOE 408 AIRFOIL Gottingen 408 airfoil Max thickness 7.8% at 30% chord. Max camber 4.1% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 408 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0124300 0.0180500
0.0248900 0.0266000
0.0498500 0.0387000
0.0748000 0.0488000
0.0997800 0.0559000
0.1497400 0.0661000
0.1997100 0.0733000
0.2996800 0.0802000
0.3996800 0.0796000
0.4997000 0.0745000
0.5997400 0.0654000
0.6997800 0.0538000
0.7998400 0.0412000
0.8998900 0.0266000
0.9499300 0.0173000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125400 -.0089500
0.0250500 -.0114000
0.0500400 -.0093000
0.0750300 -.0072000
0.1000200 -.0046000
0.1500000 -.0009000
0.1999900 0.0013000
0.2999900 0.0027000
0.3999900 0.0031000
0.4999900 0.0025000
0.5999900 0.0014000
0.7000000 -.0002000
0.8000100 -.0023000
0.9000200 -.0049000
0.9500300 -.0067000
1.0000000 0.0000000
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Polars for GOE 408 AIRFOIL (goe408-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe408-il | 50,000 | 9 | 35.8 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe408-il | 50,000 | 5 | 40.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe408-il | 100,000 | 9 | 58.3 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe408-il | 100,000 | 5 | 59.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe408-il | 200,000 | 9 | 78.4 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe408-il | 200,000 | 5 | 75.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe408-il | 500,000 | 9 | 101.8 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe408-il | 500,000 | 5 | 94.7 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe408-il | 1,000,000 | 9 | 119.8 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe408-il | 1,000,000 | 5 | 102.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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