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EPPLER 598 AIRFOIL (e598-il)

EPPLER 598 AIRFOIL - Eppler E598 airfoil


Airfoil e598-il
Details Dat file Parser  
(e598-il) EPPLER 598 AIRFOIL
Eppler E598 airfoil
Max thickness 11.1% at 24.2% chord.
Max camber 4.5% at 34.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 598 AIRFOIL
       34.       38.

 0.0000100 0.0001000
 0.0001000 0.0016400
 0.0006300 0.0043600
 0.0049000 0.0136000
 0.0131900 0.0238600
 0.0254100 0.0346000
 0.0414900 0.0454300
 0.0613000 0.0560100
 0.0847000 0.0660500
 0.1114800 0.0752900
 0.1413900 0.0834600
 0.1742200 0.0902800
 0.2097300 0.0955200
 0.2477100 0.0989900
 0.2879100 0.1005300
 0.3301200 0.1000200
 0.3741600 0.0973800
 0.4198800 0.0926000
 0.4672800 0.0858500
 0.5162000 0.0776900
 0.5661300 0.0686600
 0.6164500 0.0592000
 0.6665200 0.0497100
 0.7156200 0.0405700
 0.7630100 0.0320600
 0.8079100 0.0244500
 0.8495600 0.0178900
 0.8872400 0.0124600
 0.9202600 0.0081300
 0.9480900 0.0048000
 0.9703500 0.0023800
 0.9866700 0.0008800
 0.9966400 0.0001800
 1.0000000 0.0000000

 0.0000100 0.0001000
 0.0000800 -.0013300
 0.0001900 -.0020000
 0.0003500 -.0026300
 0.0005800 -.0032100
 0.0009000 -.0037500
 0.0013100 -.0042900
 0.0017900 -.0048300
 0.0029500 -.0058900
 0.0043500 -.0069400
 0.0068600 -.0084800
 0.0181400 -.0129700
 0.0347300 -.0164100
 0.0564800 -.0184000
 0.0835000 -.0189500
 0.1158600 -.0182500
 0.1533900 -.0167500
 0.1955900 -.0148200
 0.2419200 -.0126800
 0.2917800 -.0106200
 0.3444000 -.0089400
 0.3987900 -.0077000
 0.4541600 -.0067300
 0.5098400 -.0059400
 0.5652100 -.0052700
 0.6196200 -.0047100
 0.6724300 -.0042300
 0.7230400 -.0038200
 0.7708600 -.0034500
 0.8153300 -.0031200
 0.8559300 -.0028000
 0.8921700 -.0024500
 0.9236400 -.0020100
 0.9500500 -.0014100
 0.9712500 -.0007300
 0.9869500 -.0002200
 0.9966900 0.0000200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 598 AIRFOIL (e598-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e598-il50,00099.9 at α=0°Mach=0 Ncrit=9Xfoil predictionDetails
   e598-il50,000523.5 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e598-il100,000943.3 at α=11.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e598-il100,000550.6 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e598-il200,000972.2 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e598-il200,000575.6 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e598-il500,0009109.3 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e598-il500,0005106.3 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e598-il1,000,0009137.2 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e598-il1,000,0005128.3 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
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