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EPPLER EA 6(-1)-012 AIRFOIL (ea61012-il)

EPPLER EA 6(-1)-012 AIRFOIL - Eppler EA 6(-1)-012 airfoil


Airfoil ea61012-il
Details Dat file Parser  
(ea61012-il) EPPLER EA 6(-1)-012 AIRFOIL
Eppler EA 6(-1)-012 airfoil
Max thickness 12% at 30% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER EA 6(-1)-012 AIRFOIL
       14.       14.

 0.0000000 0.0000000
 0.0100000 0.0180000
 0.0500000 0.0360000
 0.1000000 0.0456000
 0.2000000 0.0558000
 0.3000000 0.0600000
 0.4000000 0.0594000
 0.5000000 0.0560000
 0.6000000 0.0468000
 0.7000000 0.0340000
 0.8000000 0.0192000
 0.9000000 0.0086000
 0.9500000 0.0042000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0100000 -.0180000
 0.0500000 -.0360000
 0.1000000 -.0456000
 0.2000000 -.0558000
 0.3000000 -.0600000
 0.4000000 -.0594000
 0.5000000 -.0560000
 0.6000000 -.0468000
 0.7000000 -.0340000
 0.8000000 -.0192000
 0.9000000 -.0086000
 0.9500000 -.0042000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER EA 6(-1)-012 AIRFOIL (ea61012-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ea61012-il50,000925.6 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   ea61012-il50,000523.8 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   ea61012-il100,000933.5 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ea61012-il100,000529.1 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ea61012-il200,000934.7 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ea61012-il200,000537.3 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ea61012-il500,000947.1 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   ea61012-il500,000552.8 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ea61012-il1,000,000964 at α=10.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ea61012-il1,000,000570.7 at α=11.75°Mach=0 Ncrit=5Xfoil predictionDetails
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