EPPLER EA 6(-1)-012 AIRFOIL (ea61012-il)
EPPLER EA 6(-1)-012 AIRFOIL - Eppler EA 6(-1)-012 airfoil
| Details | Dat file | Parser | |
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(ea61012-il) EPPLER EA 6(-1)-012 AIRFOIL Eppler EA 6(-1)-012 airfoil Max thickness 12% at 30% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER EA 6(-1)-012 AIRFOIL
14. 14.
0.0000000 0.0000000
0.0100000 0.0180000
0.0500000 0.0360000
0.1000000 0.0456000
0.2000000 0.0558000
0.3000000 0.0600000
0.4000000 0.0594000
0.5000000 0.0560000
0.6000000 0.0468000
0.7000000 0.0340000
0.8000000 0.0192000
0.9000000 0.0086000
0.9500000 0.0042000
1.0000000 0.0000000
0.0000000 0.0000000
0.0100000 -.0180000
0.0500000 -.0360000
0.1000000 -.0456000
0.2000000 -.0558000
0.3000000 -.0600000
0.4000000 -.0594000
0.5000000 -.0560000
0.6000000 -.0468000
0.7000000 -.0340000
0.8000000 -.0192000
0.9000000 -.0086000
0.9500000 -.0042000
1.0000000 0.0000000
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Similar airfoils
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Polars for EPPLER EA 6(-1)-012 AIRFOIL (ea61012-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ea61012-il | 50,000 | 9 | 25.6 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ea61012-il | 50,000 | 5 | 23.8 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ea61012-il | 100,000 | 9 | 33.5 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ea61012-il | 100,000 | 5 | 29.1 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ea61012-il | 200,000 | 9 | 34.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ea61012-il | 200,000 | 5 | 37.3 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ea61012-il | 500,000 | 9 | 47.1 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ea61012-il | 500,000 | 5 | 52.8 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ea61012-il | 1,000,000 | 9 | 64 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ea61012-il | 1,000,000 | 5 | 70.7 at α=11.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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