GOE 548 AIRFOIL (goe548-il)
GOE 548 AIRFOIL - Gottingen 548 airfoil
| Details | Dat file | Parser | |
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(goe548-il) GOE 548 AIRFOIL Gottingen 548 airfoil Max thickness 11.9% at 40% chord. Max camber 2.3% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 548 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0138000
0.0250000 0.0221000
0.0500000 0.0352000
0.0750000 0.0433000
0.1000000 0.0504000
0.1500000 0.0606000
0.2000000 0.0683000
0.3000000 0.0787000
0.4000000 0.0816000
0.5000000 0.0790000
0.6000000 0.0719000
0.7000000 0.0595500
0.8000000 0.0452000
0.9000000 0.0240000
0.9500000 0.0133000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0122000
0.0250000 -.0174000
0.0500000 -.0233000
0.0750000 -.0282000
0.1000000 -.0316000
0.1500000 -.0364000
0.2000000 -.0387000
0.3000000 -.0398000
0.4000000 -.0374000
0.5000000 -.0330000
0.6000000 -.0271000
0.7000000 -.0207000
0.8000000 -.0138000
0.9000000 -.0069000
0.9500000 -.0037000
1.0000000 0.0000000
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Polars for GOE 548 AIRFOIL (goe548-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe548-il | 50,000 | 9 | 34.1 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe548-il | 50,000 | 5 | 32.8 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe548-il | 100,000 | 9 | 53.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe548-il | 100,000 | 5 | 51.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe548-il | 200,000 | 9 | 74.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe548-il | 200,000 | 5 | 68.7 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe548-il | 500,000 | 9 | 95 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe548-il | 500,000 | 5 | 76.6 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe548-il | 1,000,000 | 9 | 100.7 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe548-il | 1,000,000 | 5 | 76.3 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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