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EPPLER 58 AIRFOIL (e58-il)

EPPLER 58 AIRFOIL - Eppler E58 low Reynolds number airfoil


Airfoil e58-il
Details Dat file Parser  
(e58-il) EPPLER 58 AIRFOIL
Eppler E58 low Reynolds number airfoil
Max thickness 5.6% at 30% chord.
Max camber 6.5% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 58 AIRFOIL
       18.       18.

 0.0000000 0.0000000
 0.0125000 0.0150000
 0.0250000 0.0235000
 0.0500000 0.0350000
 0.0750000 0.0440000
 0.1000000 0.0520000
 0.1500000 0.0630000
 0.2000000 0.0720000
 0.2500000 0.0780000
 0.3000000 0.0830000
 0.4000000 0.0880000
 0.5000000 0.0890000
 0.6000000 0.0850000
 0.7000000 0.0770000
 0.8000000 0.0620000
 0.9000000 0.0370000
 0.9500000 0.0200000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0050000
 0.0250000 -.0050000
 0.0500000 -.0040000
 0.0750000 -.0020000
 0.1000000 0.0010000
 0.1500000 0.0090000
 0.2000000 0.0160000
 0.2500000 0.0220000
 0.3000000 0.0270000
 0.4000000 0.0350000
 0.5000000 0.0400000
 0.6000000 0.0420000
 0.7000000 0.0410000
 0.8000000 0.0360000
 0.9000000 0.0250000
 0.9500000 0.0150000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 58 AIRFOIL (e58-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e58-il50,000946.1 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e58-il50,000544.1 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e58-il100,000970.8 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e58-il100,000568.4 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e58-il200,0009108.2 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e58-il200,0005106.6 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e58-il500,0009175.1 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   e58-il500,0005166.6 at α=1.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e58-il1,000,0009235.7 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e58-il1,000,0005160.8 at α=0°Mach=0 Ncrit=5Xfoil predictionDetails
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