GOE 375 AIRFOIL (goe375-il)
GOE 375 AIRFOIL - Gottingen 375 airfoil
| Details | Dat file | Parser | |
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(goe375-il) GOE 375 AIRFOIL Gottingen 375 airfoil Max thickness 6.5% at 20% chord. Max camber 4.5% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 375 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0124100 0.0210600
0.0248600 0.0321100
0.0497900 0.0472200
0.0747400 0.0573400
0.0997100 0.0639500
0.1496800 0.0721700
0.1996600 0.0759000
0.2996500 0.0773500
0.3996700 0.0733000
0.4997000 0.0662500
0.5997400 0.0572000
0.6998000 0.0451500
0.7998600 0.0306000
0.8999299 0.0165500
0.9499600 0.0087700
1.0000000 0.0000000
0.0000000 0.0000000
0.0125200 -.0039400
0.0250000 -.0003900
0.0499800 0.0042200
0.0749700 0.0058400
0.0999700 0.0074500
0.1499600 0.0091700
0.1999500 0.0109000
0.2999400 0.0123500
0.3999400 0.0123000
0.4999500 0.0117500
0.5999500 0.0102000
0.6999700 0.0076500
0.7999800 0.0041000
0.8999900 0.0020500
0.9500000 0.0002700
1.0000000 0.0000000
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Polars for GOE 375 AIRFOIL (goe375-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe375-il | 50,000 | 9 | 32.6 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe375-il | 50,000 | 5 | 37.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe375-il | 100,000 | 9 | 46.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe375-il | 100,000 | 5 | 52.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe375-il | 200,000 | 9 | 62.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe375-il | 200,000 | 5 | 67.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe375-il | 500,000 | 9 | 88.9 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe375-il | 500,000 | 5 | 91.5 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe375-il | 1,000,000 | 9 | 109.9 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe375-il | 1,000,000 | 5 | 108.4 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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