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EPPLER 584 AIRFOIL (e584-il)

EPPLER 584 AIRFOIL - Eppler E584 sailplane airfoil


Airfoil e584-il
Details Dat file Parser  
(e584-il) EPPLER 584 AIRFOIL
Eppler E584 sailplane airfoil
Max thickness 16.6% at 38.3% chord.
Max camber 4.5% at 38.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 584 AIRFOIL
       35.       38.

 0.0000100 0.0002000
 0.0001200 0.0018800
 0.0006500 0.0045900
 0.0021600 0.0089600
 0.0086600 0.0198100
 0.0193500 0.0316300
 0.0341300 0.0439100
 0.0528700 0.0562600
 0.0754500 0.0683600
 0.1016600 0.0799300
 0.1313000 0.0907100
 0.1641000 0.1004800
 0.1997900 0.1090400
 0.2380300 0.1162200
 0.2784900 0.1218900
 0.3207500 0.1258700
 0.3644600 0.1280200
 0.4092600 0.1282200
 0.4547800 0.1264100
 0.5006200 0.1224400
 0.5466300 0.1160800
 0.5930100 0.1075000
 0.6396700 0.0962700
 0.6860501 0.0863900
 0.7315500 0.0749600
 0.7755200 0.0635300
 0.8172800 0.0524600
 0.8561500 0.0420700
 0.8914200 0.0325700
 0.9224401 0.0241200
 0.9485600 0.0166800
 0.9695600 0.0100300
 0.9856000 0.0045200
 0.9962000 0.0010800
 1.0000000 0.0000000

 0.0000100 0.0002000
 0.0000700 -.0013500
 0.0001900 -.0020700
 0.0003600 -.0027500
 0.0006000 -.0033700
 0.0009500 -.0039500
 0.0014000 -.0045200
 0.0019300 -.0050900
 0.0032300 -.0062200
 0.0048100 -.0073400
 0.0076400 -.0090100
 0.0143000 -.0120300
 0.0307200 -.0170200
 0.0526800 -.0213800
 0.0799000 -.0251000
 0.1120900 -.0282200
 0.1488700 -.0308500
 0.1897400 -.0330200
 0.2341800 -.0347800
 0.2816400 -.0361600
 0.3314900 -.0371600
 0.3831200 -.0377700
 0.4358800 -.0379700
 0.4891100 -.0377300
 0.5421600 -.0370300
 0.5943800 -.0357800
 0.6451100 -.0339000
 0.6937300 -.0312500
 0.7395800 -.0273900
 0.7829200 -.0215500
 0.8248300 -.0142900
 0.8652000 -.0073900
 0.9027400 -.0020600
 0.9360200 0.0011700
 0.9631500 0.0021900
 0.9837300 0.0016000
 0.9959400 0.0005100
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 584 AIRFOIL (e584-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e584-il50,00094.5 at α=11°Mach=0 Ncrit=9Xfoil predictionDetails
   e584-il50,000511.9 at α=-1.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e584-il100,000929.9 at α=13.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e584-il100,000532.8 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e584-il200,000967.8 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   e584-il200,000564.4 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   e584-il500,0009103.1 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   e584-il500,0005101.8 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e584-il1,000,0009134 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e584-il1,000,0005126.8 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
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