GOE 595 AIRFOIL (goe595-il)
GOE 595 AIRFOIL - Gottingen 595 airfoil
| Details | Dat file | Parser | |
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(goe595-il) GOE 595 AIRFOIL Gottingen 595 airfoil Max thickness 9.6% at 30% chord. Max camber 3% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 595 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0168500
0.0250000 0.0242000
0.0500000 0.0354000
0.0750000 0.0451000
0.1000000 0.0528000
0.1500000 0.0637000
0.2000000 0.0701000
0.3000000 0.0774000
0.4000000 0.0772000
0.5000000 0.0735000
0.6000000 0.0663000
0.7000000 0.0551000
0.8000000 0.0404000
0.9000000 0.0217000
0.9500000 0.0116000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0081500
0.0250000 -.0108000
0.0500000 -.0151000
0.0750000 -.0169000
0.1000000 -.0182000
0.1500000 -.0193000
0.2000000 -.0194000
0.3000000 -.0181000
0.4000000 -.0168000
0.5000000 -.0140000
0.6000000 -.0112000
0.7000000 -.0084000
0.8000000 -.0056000
0.9000000 -.0028000
0.9500000 -.0014000
1.0000000 0.0000000
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Polars for GOE 595 AIRFOIL (goe595-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe595-il | 50,000 | 9 | 36.9 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe595-il | 50,000 | 5 | 38.1 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe595-il | 100,000 | 9 | 55.1 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe595-il | 100,000 | 5 | 54.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe595-il | 200,000 | 9 | 74.6 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe595-il | 200,000 | 5 | 68.8 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe595-il | 500,000 | 9 | 97.7 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe595-il | 500,000 | 5 | 86.8 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe595-il | 1,000,000 | 9 | 110.6 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe595-il | 1,000,000 | 5 | 100.1 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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