GOE 444 AIRFOIL (goe444-il)
GOE 444 AIRFOIL - Gottingen 444 airfoil
| Details | Dat file | Parser | |
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(goe444-il) GOE 444 AIRFOIL Gottingen 444 airfoil Max thickness 5.6% 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 444 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0060000
0.0250000 0.0090000
0.0500000 0.0130000
0.0750000 0.0160000
0.1000000 0.0190000
0.1500000 0.0230000
0.2000000 0.0255000
0.3000000 0.0280000
0.4000000 0.0280000
0.5000000 0.0270000
0.6000000 0.0240000
0.7000000 0.0195000
0.8000000 0.0140000
0.9000000 0.0080000
0.9500000 0.0045000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0060000
0.0250000 -.0090000
0.0500000 -.0130000
0.0750000 -.0160000
0.1000000 -.0190000
0.1500000 -.0230000
0.2000000 -.0255000
0.3000000 -.0280000
0.4000000 -.0280000
0.5000000 -.0270000
0.6000000 -.0240000
0.7000000 -.0195000
0.8000000 -.0140000
0.9000000 -.0080000
0.9500000 -.0045000
1.0000000 0.0000000
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Polars for GOE 444 AIRFOIL (goe444-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe444-il | 50,000 | 9 | 17.1 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe444-il | 50,000 | 5 | 16.5 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe444-il | 100,000 | 9 | 21.5 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe444-il | 100,000 | 5 | 24.8 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe444-il | 200,000 | 9 | 38.2 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe444-il | 200,000 | 5 | 35.2 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe444-il | 500,000 | 9 | 45.9 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe444-il | 500,000 | 5 | 31.8 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe444-il | 1,000,000 | 9 | 42.3 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe444-il | 1,000,000 | 5 | 34.1 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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