EPPLER EA 8(-1)-006 AIRFOIL (ea81006-il)
EPPLER EA 8(-1)-006 AIRFOIL - Eppler EA 8(-1)-006 airfoil
| Details | Dat file | Parser | |
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(ea81006-il) EPPLER EA 8(-1)-006 AIRFOIL Eppler EA 8(-1)-006 airfoil Max thickness 6% 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 8(-1)-006 AIRFOIL
14. 14.
0.0000000 0.0000000
0.0100000 0.0100000
0.0500000 0.0178000
0.1000000 0.0238000
0.2000000 0.0288000
0.3000000 0.0300000
0.4000000 0.0298000
0.5000000 0.0280000
0.6000000 0.0255000
0.7000000 0.0212000
0.8000000 0.0148000
0.9000000 0.0074000
0.9500000 0.0036000
1.0000000 0.0000000
0.0000000 0.0000000
0.0100000 -.0100000
0.0500000 -.0178000
0.1000000 -.0238000
0.2000000 -.0288000
0.3000000 -.0300000
0.4000000 -.0298000
0.5000000 -.0280000
0.6000000 -.0255000
0.7000000 -.0212000
0.8000000 -.0148000
0.9000000 -.0074000
0.9500000 -.0036000
1.0000000 0.0000000
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Polars for EPPLER EA 8(-1)-006 AIRFOIL (ea81006-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ea81006-il | 50,000 | 9 | 17.9 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ea81006-il | 50,000 | 5 | 19.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ea81006-il | 100,000 | 9 | 22.7 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ea81006-il | 100,000 | 5 | 23.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ea81006-il | 200,000 | 9 | 35 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ea81006-il | 200,000 | 5 | 35.7 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ea81006-il | 500,000 | 9 | 43.3 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ea81006-il | 500,000 | 5 | 53.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ea81006-il | 1,000,000 | 9 | 67.4 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ea81006-il | 1,000,000 | 5 | 66 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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