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EPPLER EA 6(-1)-009 AIRFOIL (ea61009-il)

EPPLER EA 6(-1)-009 AIRFOIL - Eppler EA 6(-1)-009 airfoil


Airfoil ea61009-il
Details Dat file Parser  
(ea61009-il) EPPLER EA 6(-1)-009 AIRFOIL
Eppler EA 6(-1)-009 airfoil
Max thickness 9% 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)-009 AIRFOIL
       14.       14.

 0.0000000 0.0000000
 0.0100000 0.0136000
 0.0500000 0.0264000
 0.1000000 0.0348000
 0.2000000 0.0420000
 0.3000000 0.0450000
 0.4000000 0.0438000
 0.5000000 0.0408000
 0.6000000 0.0344000
 0.7000000 0.0255000
 0.8000000 0.0145000
 0.9000000 0.0050000
 0.9500000 0.0021000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0100000 -.0136000
 0.0500000 -.0264000
 0.1000000 -.0348000
 0.2000000 -.0420000
 0.3000000 -.0450000
 0.4000000 -.0438000
 0.5000000 -.0408000
 0.6000000 -.0344000
 0.7000000 -.0255000
 0.8000000 -.0145000
 0.9000000 -.0050000
 0.9500000 -.0021000
 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)-009 AIRFOIL (ea61009-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ea61009-il50,000923.6 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ea61009-il50,000521.4 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ea61009-il100,000929.5 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ea61009-il100,000527.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ea61009-il200,000931.8 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   ea61009-il200,000533.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   ea61009-il500,000946.5 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ea61009-il500,000558.4 at α=9.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ea61009-il1,000,000972.9 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ea61009-il1,000,000576 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
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