GOE 460 AIRFOIL (goe460-il)
GOE 460 AIRFOIL - Gottingen 460 airfoil
| Details | Dat file | Parser | |
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(goe460-il) GOE 460 AIRFOIL Gottingen 460 airfoil Max thickness 20.5% 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 460 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0275000
0.0250000 0.0395000
0.0500000 0.0555000
0.0750000 0.0675000
0.1000000 0.0760000
0.1500000 0.0890000
0.2000000 0.0960000
0.3000000 0.1025000
0.4000000 0.1005000
0.5000000 0.0925000
0.6000000 0.0800000
0.7000000 0.0645000
0.8000000 0.0450000
0.9000000 0.0235000
0.9500000 0.0115000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0275000
0.0250000 -.0395000
0.0500000 -.0555000
0.0750000 -.0675000
0.1000000 -.0760000
0.1500000 -.0890000
0.2000000 -.0960000
0.3000000 -.1025000
0.4000000 -.1005000
0.5000000 -.0925000
0.6000000 -.0800000
0.7000000 -.0645000
0.8000000 -.0450000
0.9000000 -.0235000
0.9500000 -.0115000
1.0000000 0.0000000
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Polars for GOE 460 AIRFOIL (goe460-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe460-il | 50,000 | 9 | 20.8 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe460-il | 50,000 | 5 | 25.8 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe460-il | 100,000 | 9 | 39.8 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe460-il | 100,000 | 5 | 34.1 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe460-il | 200,000 | 9 | 46.4 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe460-il | 200,000 | 5 | 39.4 at α=10.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe460-il | 500,000 | 9 | 54.4 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe460-il | 500,000 | 5 | 50.6 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe460-il | 1,000,000 | 9 | 66.6 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe460-il | 1,000,000 | 5 | 57.5 at α=10.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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