GOE 374 AIRFOIL (goe374-il)
GOE 374 AIRFOIL - Gottingen 374 airfoil
| Details | Dat file | Parser | |
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(goe374-il) GOE 374 AIRFOIL Gottingen 374 airfoil Max thickness 6.5% at 30% chord. Max camber 4.5% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 374 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0124100 0.0175600
0.0248600 0.0281200
0.0497900 0.0422500
0.0747400 0.0518700
0.0997100 0.0585000
0.1496600 0.0682500
0.1996300 0.0740000
0.2996100 0.0775000
0.3996300 0.0740000
0.4996600 0.0675000
0.5997100 0.0575000
0.6997700 0.0465000
0.7998400 0.0325000
0.8999200 0.0170000
0.9499600 0.0087500
1.0000000 0.0000000
0.0000000 0.0000000
0.0125200 -.0039400
0.0250100 -.0013700
0.0499900 0.0017500
0.0749800 0.0043700
0.0999700 0.0065000
0.1499600 0.0087500
0.1999500 0.0110000
0.2999400 0.0130000
0.3999300 0.0135000
0.4999400 0.0120000
0.5999500 0.0105000
0.6999600 0.0080000
0.7999800 0.0050000
0.8999900 0.0020000
0.9500000 0.0002500
1.0000000 0.0000000
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Polars for GOE 374 AIRFOIL (goe374-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe374-il | 50,000 | 9 | 32.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe374-il | 50,000 | 5 | 40.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe374-il | 100,000 | 9 | 51.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe374-il | 100,000 | 5 | 57.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe374-il | 200,000 | 9 | 72.4 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe374-il | 200,000 | 5 | 74.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe374-il | 500,000 | 9 | 98.7 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe374-il | 500,000 | 5 | 97.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe374-il | 1,000,000 | 9 | 117.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe374-il | 1,000,000 | 5 | 110.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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