GOE 593 AIRFOIL (goe593-il)
GOE 593 AIRFOIL - Gottingen 593 airfoil
| Details | Dat file | Parser | |
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(goe593-il) GOE 593 AIRFOIL Gottingen 593 airfoil Max thickness 11.9% at 30% chord. Max camber 4.1% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 593 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0253700
0.0250000 0.0357500
0.0500000 0.0500000
0.0750000 0.0612500
0.1000000 0.0705000
0.1500000 0.0840000
0.2000000 0.0920000
0.3000000 0.0990000
0.4000000 0.0990000
0.5000000 0.0935000
0.6000000 0.0825000
0.7000000 0.0675000
0.8000000 0.0490000
0.9000000 0.0270000
0.9500000 0.0150000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0116300
0.0250000 -.0157500
0.0500000 -.0200000
0.0750000 -.0222500
0.1000000 -.0230000
0.1500000 -.0230000
0.2000000 -.0225000
0.3000000 -.0200000
0.4000000 -.0180000
0.5000000 -.0150000
0.6000000 -.0120000
0.7000000 -.0090000
0.8000000 -.0060000
0.9000000 -.0030000
0.9500000 -.0015000
1.0000000 0.0000000
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Polars for GOE 593 AIRFOIL (goe593-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe593-il | 50,000 | 9 | 24.3 at α=12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe593-il | 50,000 | 5 | 35.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe593-il | 100,000 | 9 | 52.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe593-il | 100,000 | 5 | 53.2 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe593-il | 200,000 | 9 | 74.6 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe593-il | 200,000 | 5 | 69.9 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe593-il | 500,000 | 9 | 101.4 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe593-il | 500,000 | 5 | 88.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe593-il | 1,000,000 | 9 | 117.1 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe593-il | 1,000,000 | 5 | 107.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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