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EPPLER EA 8(-1)-006 AIRFOIL (ea81006-il)

EPPLER EA 8(-1)-006 AIRFOIL - Eppler EA 8(-1)-006 airfoil


Airfoil ea81006-il
Details Dat file Parser  
(ea81006-il) EPPLER EA 8(-1)-006 AIRFOIL
Eppler EA 8(-1)-006 airfoil
Max thickness 6% 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 8(-1)-006 AIRFOIL
       14.       14.

 0.0000000 0.0000000
 0.0100000 0.0100000
 0.0500000 0.0178000
 0.1000000 0.0238000
 0.2000000 0.0288000
 0.3000000 0.0300000
 0.4000000 0.0298000
 0.5000000 0.0280000
 0.6000000 0.0255000
 0.7000000 0.0212000
 0.8000000 0.0148000
 0.9000000 0.0074000
 0.9500000 0.0036000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0100000 -.0100000
 0.0500000 -.0178000
 0.1000000 -.0238000
 0.2000000 -.0288000
 0.3000000 -.0300000
 0.4000000 -.0298000
 0.5000000 -.0280000
 0.6000000 -.0255000
 0.7000000 -.0212000
 0.8000000 -.0148000
 0.9000000 -.0074000
 0.9500000 -.0036000
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for EPPLER EA 8(-1)-006 AIRFOIL (ea81006-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ea81006-il50,000917.9 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   ea81006-il50,000519.4 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ea81006-il100,000922.7 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ea81006-il100,000523.4 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ea81006-il200,000935 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ea81006-il200,000535.7 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ea81006-il500,000943.3 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ea81006-il500,000553.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   ea81006-il1,000,000967.4 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ea81006-il1,000,000566 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
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