EPPLER 479 AIRFOIL (e479-il)
EPPLER 479 AIRFOIL - Eppler E479 aerobatic aircraft airfoil
| Details | Dat file | Parser | |
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(e479-il) EPPLER 479 AIRFOIL Eppler E479 aerobatic aircraft airfoil Max thickness 16.6% at 25.7% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 479 AIRFOIL
31. 31.
0.0000000 0.0000000
0.0028100 0.0102500
0.0106100 0.0213800
0.0226800 0.0325300
0.0389000 0.0432200
0.0591500 0.0531100
0.0833200 0.0619000
0.1112900 0.0693700
0.1428800 0.0753400
0.1779000 0.0796500
0.2161200 0.0822000
0.2573400 0.0828400
0.3014800 0.0816200
0.3483200 0.0788100
0.3973800 0.0747100
0.4481900 0.0695200
0.5001800 0.0635000
0.5528000 0.0569000
0.6054200 0.0499500
0.6573800 0.0429200
0.7080200 0.0360300
0.7566200 0.0294900
0.8025100 0.0234600
0.8449800 0.0180800
0.8833700 0.0134200
0.9170500 0.0095100
0.9454500 0.0062600
0.9682701 0.0034900
0.9853700 0.0013900
0.9962400 0.0002800
1.0000000 0.0000000
0.0000000 0.0000000
0.0028100 -.0102500
0.0106100 -.0213800
0.0226800 -.0325300
0.0389000 -.0432200
0.0591500 -.0531100
0.0833200 -.0619000
0.1112900 -.0693700
0.1428800 -.0753400
0.1779000 -.0796500
0.2161200 -.0822000
0.2573400 -.0828400
0.3014800 -.0816200
0.3483200 -.0788100
0.3973800 -.0747100
0.4481900 -.0695200
0.5001800 -.0635000
0.5528000 -.0569000
0.6054200 -.0499500
0.6573800 -.0429200
0.7080200 -.0360300
0.7566200 -.0294900
0.8025100 -.0234600
0.8449800 -.0180800
0.8833700 -.0134200
0.9170500 -.0095100
0.9454500 -.0062600
0.9682701 -.0034900
0.9853700 -.0013900
0.9962400 -.0002800
1.0000000 0.0000000
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Polars for EPPLER 479 AIRFOIL (e479-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e479-il | 50,000 | 9 | 15.9 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e479-il | 50,000 | 5 | 23.8 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e479-il | 100,000 | 9 | 33.1 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e479-il | 100,000 | 5 | 39 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e479-il | 200,000 | 9 | 52.2 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e479-il | 200,000 | 5 | 54.1 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e479-il | 500,000 | 9 | 76.9 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e479-il | 500,000 | 5 | 74.1 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e479-il | 1,000,000 | 9 | 95.5 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e479-il | 1,000,000 | 5 | 88.5 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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