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EPPLER 559 AIRFOIL (e559-il)

EPPLER 559 AIRFOIL - Eppler E559 general aviation airfoil


Airfoil e559-il
Details Dat file Parser  
(e559-il) EPPLER 559 AIRFOIL
Eppler E559 general aviation airfoil
Max thickness 16% at 27.2% chord.
Max camber 4.3% at 50.2% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 559 AIRFOIL
       33.       29.

 0.0001500 -.0020700
 0.0017900 0.0075900
 0.0080100 0.0189300
 0.0184200 0.0310500
 0.0328800 0.0434700
 0.0512500 0.0558100
 0.0733500 0.0677400
 0.0989700 0.0789500
 0.1278900 0.0891400
 0.1598800 0.0980300
 0.1946800 0.1053300
 0.2321200 0.1107400
 0.2721100 0.1141400
 0.3144800 0.1155000
 0.3590200 0.1149200
 0.4054100 0.1125800
 0.4532500 0.1086500
 0.5020900 0.1033300
 0.5514600 0.0968300
 0.6008500 0.0893900
 0.6497200 0.0812600
 0.6975000 0.0726700
 0.7436000 0.0638700
 0.7874300 0.0550700
 0.8284100 0.0464800
 0.8659600 0.0382600
 0.8995400 0.0305300
 0.9286600 0.0233800
 0.9528300 0.0167500
 0.9720400 0.0104200
 0.9866900 0.0048500
 0.9964600 0.0011900
 1.0000000 0.0000000

 0.0001500 -.0020700
 0.0044700 -.0104800
 0.0147600 -.0188200
 0.0297600 -.0269200
 0.0491600 -.0342700
 0.0727700 -.0405600
 0.1004200 -.0455200
 0.1319200 -.0489300
 0.1671300 -.0505700
 0.2059400 -.0503300
 0.2482400 -.0482000
 0.2939200 -.0443300
 0.3428000 -.0389600
 0.3946200 -.0325300
 0.4488900 -.0256600
 0.5047800 -.0188400
 0.5614500 -.0124000
 0.6180500 -.0066000
 0.6737000 -.0016400
 0.7275100 0.0023300
 0.7786400 0.0052200
 0.8262500 0.0070100
 0.8695300 0.0077100
 0.9077300 0.0074000
 0.9401500 0.0062200
 0.9660700 0.0043700
 0.9848700 0.0023100
 0.9962100 0.0006500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 559 AIRFOIL (e559-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e559-il50,00098.8 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e559-il50,000530.5 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   e559-il100,000943.7 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e559-il100,000552.9 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   e559-il200,000970.4 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e559-il200,000573.2 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   e559-il500,0009103.1 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e559-il500,0005101.9 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   e559-il1,000,0009130.6 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e559-il1,000,0005123.6 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
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