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EPPLER 479 AIRFOIL (e479-il)

EPPLER 479 AIRFOIL - Eppler E479 aerobatic aircraft airfoil


Airfoil e479-il
Details Dat file Parser  
(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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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 479 AIRFOIL (e479-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e479-il50,000915.9 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e479-il50,000523.8 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e479-il100,000933.1 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e479-il100,000539 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e479-il200,000952.2 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e479-il200,000554.1 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e479-il500,000976.9 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e479-il500,000574.1 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e479-il1,000,000995.5 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e479-il1,000,000588.5 at α=9.5°Mach=0 Ncrit=5Xfoil predictionDetails
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