GOE 479 AIRFOIL (goe479-il)
GOE 479 AIRFOIL - Gottingen 479 airfoil
| Details | Dat file | Parser | |
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(goe479-il) GOE 479 AIRFOIL Gottingen 479 airfoil Max thickness 11.6% at 30% chord. Max camber 4% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 479 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0263700
0.0250000 0.0352400
0.0500000 0.0485800
0.0750000 0.0597100
0.1000000 0.0684500
0.1500000 0.0809200
0.2000000 0.0889000
0.3000000 0.0968500
0.4000000 0.0958000
0.5000000 0.0892500
0.6000000 0.0772000
0.7000000 0.0621500
0.8000000 0.0446000
0.9000000 0.0235500
0.9500000 0.0120200
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0141300
0.0250000 -.0187600
0.0500000 -.0225300
0.0750000 -.0242900
0.1000000 -.0250500
0.1500000 -.0245700
0.2000000 -.0231000
0.3000000 -.0191500
0.4000000 -.0157000
0.5000000 -.0122500
0.6000000 -.0088000
0.7000000 -.0058500
0.8000000 -.0034000
0.9000000 -.0019500
0.9500000 -.0009700
1.0000000 0.0000000
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Polars for GOE 479 AIRFOIL (goe479-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe479-il | 50,000 | 9 | 31.6 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe479-il | 50,000 | 5 | 35.4 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe479-il | 100,000 | 9 | 53.9 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe479-il | 100,000 | 5 | 55.3 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe479-il | 200,000 | 9 | 75.1 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe479-il | 200,000 | 5 | 72.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe479-il | 500,000 | 9 | 101.1 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe479-il | 500,000 | 5 | 94.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe479-il | 1,000,000 | 9 | 121.5 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe479-il | 1,000,000 | 5 | 110.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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