EPPLER EA 6(-1)-009 AIRFOIL (ea61009-il)
EPPLER EA 6(-1)-009 AIRFOIL - Eppler EA 6(-1)-009 airfoil
| Details | Dat file | Parser | |
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(ea61009-il) EPPLER EA 6(-1)-009 AIRFOIL Eppler EA 6(-1)-009 airfoil Max thickness 9% 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)-009 AIRFOIL
14. 14.
0.0000000 0.0000000
0.0100000 0.0136000
0.0500000 0.0264000
0.1000000 0.0348000
0.2000000 0.0420000
0.3000000 0.0450000
0.4000000 0.0438000
0.5000000 0.0408000
0.6000000 0.0344000
0.7000000 0.0255000
0.8000000 0.0145000
0.9000000 0.0050000
0.9500000 0.0021000
1.0000000 0.0000000
0.0000000 0.0000000
0.0100000 -.0136000
0.0500000 -.0264000
0.1000000 -.0348000
0.2000000 -.0420000
0.3000000 -.0450000
0.4000000 -.0438000
0.5000000 -.0408000
0.6000000 -.0344000
0.7000000 -.0255000
0.8000000 -.0145000
0.9000000 -.0050000
0.9500000 -.0021000
1.0000000 0.0000000
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Polars for EPPLER EA 6(-1)-009 AIRFOIL (ea61009-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ea61009-il | 50,000 | 9 | 23.6 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ea61009-il | 50,000 | 5 | 21.4 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ea61009-il | 100,000 | 9 | 29.5 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ea61009-il | 100,000 | 5 | 27.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ea61009-il | 200,000 | 9 | 31.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ea61009-il | 200,000 | 5 | 33.9 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ea61009-il | 500,000 | 9 | 46.5 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ea61009-il | 500,000 | 5 | 58.4 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ea61009-il | 1,000,000 | 9 | 72.9 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ea61009-il | 1,000,000 | 5 | 76 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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