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EPPLER 560 AIRFOIL (e560-il)

EPPLER 560 AIRFOIL - Eppler E560 general aviation airfoil


Airfoil e560-il
Details Dat file Parser  
(e560-il) EPPLER 560 AIRFOIL
Eppler E560 general aviation airfoil
Max thickness 16.1% at 24% chord.
Max camber 4.9% at 51.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 560 AIRFOIL
       33.       29.

 0.0000100 -.0000300
 0.0028700 0.0103700
 0.0100900 0.0222100
 0.0214100 0.0347300
 0.0367400 0.0474700
 0.0559100 0.0600900
 0.0787600 0.0722400
 0.1050900 0.0836400
 0.1346400 0.0939900
 0.1671900 0.1030100
 0.2024800 0.1104000
 0.2403400 0.1159000
 0.2806400 0.1193700
 0.3232200 0.1207800
 0.3678600 0.1202200
 0.4142500 0.1178800
 0.4619700 0.1139200
 0.5105900 0.1085500
 0.5596300 0.1019600
 0.6085800 0.0943900
 0.6569100 0.0860700
 0.7040700 0.0772500
 0.7494800 0.0681700
 0.7925701 0.0590400
 0.8327700 0.0500600
 0.8695300 0.0414000
 0.9023400 0.0332000
 0.9307100 0.0255500
 0.9541900 0.0184100
 0.9727800 0.0115400
 0.9869800 0.0054300
 0.9965200 0.0013500
 1.0000000 0.0000000

 0.0000100 -.0000300
 0.0029000 -.0089000
 0.0118200 -.0172500
 0.0255400 -.0253700
 0.0437000 -.0327000
 0.0661300 -.0389100
 0.0926800 -.0437200
 0.1231800 -.0469000
 0.1575100 -.0482400
 0.1955800 -.0476300
 0.2373200 -.0450600
 0.2826300 -.0406900
 0.3313600 -.0347900
 0.3832900 -.0278300
 0.4379000 -.0204800
 0.4943700 -.0132700
 0.5518300 -.0065600
 0.6093800 -.0006400
 0.6661000 0.0042800
 0.7210701 0.0080500
 0.7733999 0.0105800
 0.8222000 0.0118500
 0.8666200 0.0118800
 0.9058500 0.0107900
 0.9391600 0.0087300
 0.9657300 0.0059300
 0.9848300 0.0030300
 0.9962200 0.0008200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 560 AIRFOIL (e560-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e560-il50,00097.8 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e560-il50,000531.1 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e560-il100,000945.7 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e560-il100,000554.6 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e560-il200,000972.8 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e560-il200,000575.3 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e560-il500,0009105.6 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   e560-il500,0005103.3 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e560-il1,000,0009133.1 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e560-il1,000,0005123.5 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
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