EPPLER 426 AIRFOIL (e426-il)
EPPLER 426 AIRFOIL - Eppler E426 airfoil
| Details | Dat file | Parser | |
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(e426-il) EPPLER 426 AIRFOIL Eppler E426 airfoil Max thickness 10.8% at 25.5% chord. Max camber 0.6% at 50.6% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 426 AIRFOIL
20. 21.
0.0003000 0.0028000
0.0050000 0.0114000
0.0134000 0.0206000
0.0260000 0.0295000
0.0430000 0.0379000
0.0640000 0.0452000
0.0890000 0.0511000
0.1170000 0.0556000
0.1510000 0.0585000
0.2290000 0.0606000
0.3190000 0.0597000
0.4180000 0.0549000
0.5210000 0.0470000
0.6250000 0.0373000
0.7250000 0.0272000
0.8160000 0.0181000
0.8920000 0.0107000
0.9520000 0.0053000
0.9870000 0.0013000
1.0000000 0.0000000
0.0003000 0.0028000
0.0010000 -.0054000
0.0070000 -.0137000
0.0180000 -.0220000
0.0330000 -.0297000
0.0510000 -.0364000
0.0750000 -.0416000
0.1020000 -.0453000
0.1340000 -.0473000
0.1730000 -.0480000
0.2550000 -.0475000
0.3020000 -.0463000
0.4010000 -.0415000
0.5060000 -.0340000
0.6130000 -.0253000
0.7150000 -.0167000
0.8090000 -.0096000
0.8880000 -.0047000
0.9470000 -.0018000
0.9870000 -.0002000
1.0000000 0.0000000
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Polars for EPPLER 426 AIRFOIL (e426-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e426-il | 50,000 | 9 | 22.8 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e426-il | 50,000 | 5 | 26.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e426-il | 100,000 | 9 | 33.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e426-il | 100,000 | 5 | 38.5 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e426-il | 200,000 | 9 | 48.2 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e426-il | 200,000 | 5 | 54.1 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e426-il | 500,000 | 9 | 74.9 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e426-il | 500,000 | 5 | 74.4 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e426-il | 1,000,000 | 9 | 92.4 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e426-il | 1,000,000 | 5 | 89 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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