GOE 393 AIRFOIL (goe393-il)
GOE 393 AIRFOIL - Gottingen 393 airfoil
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(goe393-il) GOE 393 AIRFOIL Gottingen 393 airfoil Max thickness 6.1% at 19.9% chord. Max camber 4.2% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 393 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122700 0.0171600
0.0246600 0.0251300
0.0495100 0.0366600
0.0744100 0.0444900
0.0993200 0.0508300
0.1491900 0.0604900
0.1991000 0.0673600
0.2990500 0.0709900
0.3991100 0.0670300
0.4992300 0.0576600
0.5994100 0.0458100
0.6995500 0.0338400
0.7996900 0.0229800
0.8998400 0.0120100
0.9499199 0.0059800
1.0000000 0.0006500
0.0000000 0.0000000
0.0126500 -.0110300
0.0251700 -.0128600
0.0501700 -.0129300
0.0751300 -.0100000
0.1000800 -.0056600
0.1499800 0.0015000
0.1999100 0.0066700
0.2998200 0.0132000
0.3998000 0.0148400
0.4998300 0.0126700
0.5999000 0.0090600
0.6999300 0.0053400
0.7999700 0.0021800
0.9000000 0.0000100
0.9500100 -.0008200
1.0000000 -.0006500
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Polars for GOE 393 AIRFOIL (goe393-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe393-il | 50,000 | 9 | 34.7 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe393-il | 50,000 | 5 | 39.4 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe393-il | 100,000 | 9 | 55.9 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe393-il | 100,000 | 5 | 57.3 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe393-il | 200,000 | 9 | 75.4 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe393-il | 200,000 | 5 | 74.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe393-il | 500,000 | 9 | 101.3 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe393-il | 500,000 | 5 | 97.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe393-il | 1,000,000 | 9 | 120.4 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe393-il | 1,000,000 | 5 | 113.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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