GOE 376 AIRFOIL (goe376-il)
GOE 376 AIRFOIL - Gottingen 376 airfoil
| Details | Dat file | Parser | |
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(goe376-il) GOE 376 AIRFOIL Gottingen 376 airfoil Max thickness 6.6% at 30% chord. Max camber 5% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 376 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0124000 0.0180700
0.0248400 0.0284400
0.0497600 0.0425800
0.0747000 0.0532300
0.0996500 0.0608700
0.1495900 0.0713500
0.1995500 0.0774400
0.2995300 0.0825100
0.3995400 0.0798800
0.4995800 0.0736500
0.5996400 0.0637200
0.6997100 0.0507900
0.7997900 0.0363600
0.8998900 0.0199300
0.9499300 0.0114100
1.0000000 0.0000000
0.0000000 0.0000000
0.0125500 -.0081300
0.0250300 -.0058600
0.0500100 -.0019100
0.0749900 0.0014300
0.0999700 0.0046700
0.1499500 0.0094500
0.1999300 0.0129400
0.2999100 0.0165100
0.3999000 0.0178800
0.4999100 0.0166500
0.5999200 0.0140200
0.6999400 0.0112900
0.7999600 0.0068600
0.8999900 0.0024300
0.9500000 -.0002800
1.0000000 0.0000000
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Polars for GOE 376 AIRFOIL (goe376-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe376-il | 50,000 | 9 | 33.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe376-il | 50,000 | 5 | 41.5 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe376-il | 100,000 | 9 | 56.4 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe376-il | 100,000 | 5 | 58.7 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe376-il | 200,000 | 9 | 76.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe376-il | 200,000 | 5 | 76.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe376-il | 500,000 | 9 | 105.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe376-il | 500,000 | 5 | 96 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe376-il | 1,000,000 | 9 | 121.7 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe376-il | 1,000,000 | 5 | 97.2 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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