GOE 459 AIRFOIL (goe459-il)
GOE 459 AIRFOIL - Gottingen 459 airfoil
| Details | Dat file | Parser | |
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(goe459-il) GOE 459 AIRFOIL Gottingen 459 airfoil Max thickness 12.7% at 30% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 459 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0180000
0.0250000 0.0265000
0.0500000 0.0360000
0.0750000 0.0430000
0.1000000 0.0485000
0.1500000 0.0555000
0.2000000 0.0600000
0.3000000 0.0635000
0.4000000 0.0630000
0.5000000 0.0580000
0.6000000 0.0505000
0.7000000 0.0405000
0.8000000 0.0290000
0.9000000 0.0160000
0.9500000 0.0090000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0180000
0.0250000 -.0265000
0.0500000 -.0360000
0.0750000 -.0430000
0.1000000 -.0485000
0.1500000 -.0555000
0.2000000 -.0600000
0.3000000 -.0635000
0.4000000 -.0630000
0.5000000 -.0580000
0.6000000 -.0505000
0.7000000 -.0405000
0.8000000 -.0290000
0.9000000 -.0160000
0.9500000 -.0090000
1.0000000 0.0000000
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Polars for GOE 459 AIRFOIL (goe459-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe459-il | 50,000 | 9 | 28.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe459-il | 50,000 | 5 | 27.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe459-il | 100,000 | 9 | 40.5 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe459-il | 100,000 | 5 | 37.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe459-il | 200,000 | 9 | 49.3 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe459-il | 200,000 | 5 | 45.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe459-il | 500,000 | 9 | 59 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe459-il | 500,000 | 5 | 60.2 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe459-il | 1,000,000 | 9 | 75.6 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe459-il | 1,000,000 | 5 | 75.4 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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