GOE 372 AIRFOIL (goe372-il)
GOE 372 AIRFOIL - Gottingen 372 airfoil
| Details | Dat file | Parser | |
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(goe372-il) GOE 372 AIRFOIL Gottingen 372 airfoil Max thickness 6.2% at 29.9% chord. Max camber 4.3% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 372 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123800 0.0101400
0.0248000 0.0172900
0.0496700 0.0285700
0.0745600 0.0378600
0.0994900 0.0446400
0.1493600 0.0548900
0.1993000 0.0617900
0.2991800 0.0709400
0.3991700 0.0725900
0.4992200 0.0682400
0.5993000 0.0608900
0.6994400 0.0490400
0.7996000 0.0347000
0.8997800 0.0188500
0.9498900 0.0099200
1.0000000 0.0000000
0.0000000 0.0000000
0.0126000 -.0088600
0.0251300 -.0112100
0.0501400 -.0119200
0.0751200 -.0101400
0.1000900 -.0078500
0.1500300 -.0027700
0.1999800 0.0018000
0.2999000 0.0089500
0.3998400 0.0136000
0.4998200 0.0152500
0.5998300 0.0144000
0.6998600 0.0120500
0.7999000 0.0087000
0.8999600 0.0038500
0.9499800 0.0014200
1.0000000 0.0000000
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Polars for GOE 372 AIRFOIL (goe372-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe372-il | 50,000 | 9 | 43.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe372-il | 50,000 | 5 | 42.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe372-il | 100,000 | 9 | 62.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe372-il | 100,000 | 5 | 60.1 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe372-il | 200,000 | 9 | 82.5 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe372-il | 200,000 | 5 | 77.1 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe372-il | 500,000 | 9 | 108.6 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe372-il | 500,000 | 5 | 93 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe372-il | 1,000,000 | 9 | 126.5 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe372-il | 1,000,000 | 5 | 89.6 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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