GOE 480 AIRFOIL (goe480-il)
GOE 480 AIRFOIL - Gottingen 480 airfoil
| Details | Dat file | Parser | |
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(goe480-il) GOE 480 AIRFOIL Gottingen 480 airfoil Max thickness 11.8% at 30% chord. Max camber 5.5% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 480 AIRFOIL
13. 13.
0.0000000 0.0000000
0.0250000 0.0366400
0.0500000 0.0522700
0.1000000 0.0750500
0.2000000 0.1006000
0.3000000 0.1106500
0.4000000 0.1107000
0.5000000 0.1032500
0.6000000 0.0898000
0.7000000 0.0708500
0.8000000 0.0494000
0.9000000 0.0259500
1.0000000 0.0000000
0.0000000 0.0000000
0.0250000 -.0218600
0.0500000 -.0237200
0.1000000 -.0219500
0.2000000 -.0134000
0.3000000 -.0068500
0.4000000 -.0008000
0.5000000 0.0027500
0.6000000 0.0048000
0.7000000 0.0048500
0.8000000 0.0034000
0.9000000 0.0014500
1.0000000 0.0000000
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Similar airfoils
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Polars for GOE 480 AIRFOIL (goe480-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe480-il | 50,000 | 9 | 10.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe480-il | 50,000 | 5 | 30.3 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe480-il | 100,000 | 9 | 52.1 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe480-il | 100,000 | 5 | 57.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe480-il | 200,000 | 9 | 79 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe480-il | 200,000 | 5 | 79.2 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe480-il | 500,000 | 9 | 112.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe480-il | 500,000 | 5 | 107.2 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe480-il | 1,000,000 | 9 | 138.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe480-il | 1,000,000 | 5 | 127.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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