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EPPLER 862 STRUT AIRFOIL (e862-il)

EPPLER 862 STRUT AIRFOIL - Eppler E862 strut airfoil


Airfoil e862-il
Details Dat file Parser  
(e862-il) EPPLER 862 STRUT AIRFOIL
Eppler E862 strut airfoil
Max thickness 32.4% at 28.5% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 862 STRUT AIRFOIL
       31.       31.

 0.0000000 0.0000000
 0.0027100 0.0184800
 0.0103500 0.0375900
 0.0222600 0.0566800
 0.0381700 0.0752500
 0.0579000 0.0928700
 0.0812600 0.1091800
 0.1080400 0.1238100
 0.1380200 0.1364800
 0.1709500 0.1468900
 0.2065400 0.1548000
 0.2445000 0.1599000
 0.2846700 0.1618700
 0.3269800 0.1605400
 0.3714300 0.1558100
 0.4182500 0.1479100
 0.4673800 0.1375800
 0.5182900 0.1255200
 0.5703800 0.1123100
 0.6229300 0.0985100
 0.6751700 0.0846200
 0.7262300 0.0711100
 0.7787700 0.0577500
 0.8272600 0.0459100
 0.8709300 0.0355600
 0.9091001 0.0267100
 0.9411500 0.0193600
 0.9666001 0.0135700
 0.9850600 0.0093800
 0.9962500 0.0068500
 1.0000000 0.0060000

 0.0000000 0.0000000
 0.0027100 -.0184800
 0.0103500 -.0375900
 0.0222600 -.0566800
 0.0381700 -.0752500
 0.0579000 -.0928700
 0.0812600 -.1091800
 0.1080400 -.1238100
 0.1380200 -.1364800
 0.1709500 -.1468900
 0.2065400 -.1548000
 0.2445000 -.1599000
 0.2846700 -.1618700
 0.3269800 -.1605400
 0.3714300 -.1558100
 0.4182500 -.1479100
 0.4673800 -.1375800
 0.5182900 -.1255200
 0.5703800 -.1123100
 0.6229300 -.0985100
 0.6751700 -.0846200
 0.7262300 -.0711100
 0.7787700 -.0577500
 0.8272600 -.0459100
 0.8709300 -.0355600
 0.9091001 -.0267100
 0.9411500 -.0193600
 0.9666001 -.0135700
 0.9850600 -.0093800
 0.9962500 -.0068500
 1.0000000 -.0060000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 862 STRUT AIRFOIL (e862-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e862-il50,00092.8 at α=-4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e862-il50,00052.6 at α=-2°Mach=0 Ncrit=5Xfoil predictionDetails
   e862-il100,00095.1 at α=-0.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e862-il100,000510.5 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e862-il200,000920.7 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e862-il200,000532.7 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
   e862-il500,000957.1 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e862-il500,000554.9 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e862-il1,000,000978.1 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e862-il1,000,000574.9 at α=9.5°Mach=0 Ncrit=5Xfoil predictionDetails
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