EPPLER 58 AIRFOIL (e58-il)
EPPLER 58 AIRFOIL - Eppler E58 low Reynolds number airfoil
| Details | Dat file | Parser | |
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(e58-il) EPPLER 58 AIRFOIL Eppler E58 low Reynolds number airfoil Max thickness 5.6% at 30% chord. Max camber 6.5% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 58 AIRFOIL
18. 18.
0.0000000 0.0000000
0.0125000 0.0150000
0.0250000 0.0235000
0.0500000 0.0350000
0.0750000 0.0440000
0.1000000 0.0520000
0.1500000 0.0630000
0.2000000 0.0720000
0.2500000 0.0780000
0.3000000 0.0830000
0.4000000 0.0880000
0.5000000 0.0890000
0.6000000 0.0850000
0.7000000 0.0770000
0.8000000 0.0620000
0.9000000 0.0370000
0.9500000 0.0200000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0050000
0.0250000 -.0050000
0.0500000 -.0040000
0.0750000 -.0020000
0.1000000 0.0010000
0.1500000 0.0090000
0.2000000 0.0160000
0.2500000 0.0220000
0.3000000 0.0270000
0.4000000 0.0350000
0.5000000 0.0400000
0.6000000 0.0420000
0.7000000 0.0410000
0.8000000 0.0360000
0.9000000 0.0250000
0.9500000 0.0150000
1.0000000 0.0000000
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Polars for EPPLER 58 AIRFOIL (e58-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e58-il | 50,000 | 9 | 46.1 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e58-il | 50,000 | 5 | 44.1 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e58-il | 100,000 | 9 | 70.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e58-il | 100,000 | 5 | 68.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e58-il | 200,000 | 9 | 108.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e58-il | 200,000 | 5 | 106.6 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e58-il | 500,000 | 9 | 175.1 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e58-il | 500,000 | 5 | 166.6 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e58-il | 1,000,000 | 9 | 235.7 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e58-il | 1,000,000 | 5 | 160.8 at α=0° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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