GOE 483 AIRFOIL (goe483-il)
GOE 483 AIRFOIL - Gottingen 483 airfoil
| Details | Dat file | Parser | |
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(goe483-il) GOE 483 AIRFOIL Gottingen 483 airfoil Max thickness 5.5% at 15% chord. Max camber 5.8% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 483 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0145600
0.0250000 0.0231300
0.0500000 0.0367500
0.0750000 0.0468800
0.1000000 0.0550000
0.1500000 0.0667500
0.2000000 0.0745000
0.3000000 0.0815000
0.4000000 0.0810000
0.5000000 0.0750000
0.6000000 0.0660000
0.7000000 0.0525000
0.8000000 0.0360000
0.9000000 0.0185000
0.9500000 0.0092500
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0044400
0.0250000 -.0048800
0.0500000 -.0032500
0.0750000 -.0001300
0.1000000 0.0040000
0.1500000 0.0122500
0.2000000 0.0210000
0.3000000 0.0330000
0.4000000 0.0355000
0.5000000 0.0330000
0.6000000 0.0270000
0.7000000 0.0205000
0.8000000 0.0140000
0.9000000 0.0075000
0.9500000 0.0037500
1.0000000 0.0000000
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Polars for GOE 483 AIRFOIL (goe483-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe483-il | 50,000 | 9 | 42.8 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe483-il | 50,000 | 5 | 44.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe483-il | 100,000 | 9 | 62.7 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe483-il | 100,000 | 5 | 65.1 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe483-il | 200,000 | 9 | 83.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe483-il | 200,000 | 5 | 85.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe483-il | 500,000 | 9 | 114.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe483-il | 500,000 | 5 | 112.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe483-il | 1,000,000 | 9 | 137.4 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe483-il | 1,000,000 | 5 | 121.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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