EPPLER 59 AIRFOIL (e59-il)
EPPLER 59 AIRFOIL - Eppler E59 low Reynolds number airfoil
| Details | Dat file | Parser | |
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(e59-il) EPPLER 59 AIRFOIL Eppler E59 low Reynolds number airfoil Max thickness 5.6% at 25% chord. Max camber 5.2% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 59 AIRFOIL
18. 18.
0.0000000 0.0000000
0.0125000 0.0160000
0.0250000 0.0220000
0.0500000 0.0320000
0.0750000 0.0395000
0.1000000 0.0460000
0.1500000 0.0560000
0.2000000 0.0630000
0.2500000 0.0680000
0.3000000 0.0720000
0.4000000 0.0770000
0.5000000 0.0760000
0.6000000 0.0730000
0.7000000 0.0650000
0.8000000 0.0520000
0.9000000 0.0320000
0.9500000 0.0180000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0060000
0.0250000 -.0070000
0.0500000 -.0060000
0.0750000 -.0040000
0.1000000 -.0020000
0.1500000 0.0030000
0.2000000 0.0080000
0.2500000 0.0120000
0.3000000 0.0160000
0.4000000 0.0230000
0.5000000 0.0280000
0.6000000 0.0310000
0.7000000 0.0300000
0.8000000 0.0270000
0.9000000 0.0190000
0.9500000 0.0120000
1.0000000 0.0000000
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Polars for EPPLER 59 AIRFOIL (e59-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e59-il | 50,000 | 9 | 43.1 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e59-il | 50,000 | 5 | 46.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e59-il | 100,000 | 9 | 69.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e59-il | 100,000 | 5 | 70.6 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e59-il | 200,000 | 9 | 103.6 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e59-il | 200,000 | 5 | 99.6 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e59-il | 500,000 | 9 | 155.6 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e59-il | 500,000 | 5 | 119.3 at α=0.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e59-il | 1,000,000 | 9 | 188.8 at α=0.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e59-il | 1,000,000 | 5 | 108.8 at α=-1° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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