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EPPLER 582 AIRFOIL (e582-il)

EPPLER 582 AIRFOIL - Eppler E582 sailplane airfoil


Airfoil e582-il
Details Dat file Parser  
(e582-il) EPPLER 582 AIRFOIL
Eppler E582 sailplane airfoil
Max thickness 14.7% at 37.8% chord.
Max camber 4.2% at 43.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 582 AIRFOIL
       35.       38.

 0.0000100 0.0008600
 0.0002100 0.0023900
 0.0008400 0.0048800
 0.0023600 0.0086000
 0.0090700 0.0185300
 0.0200000 0.0293400
 0.0350400 0.0405600
 0.0541100 0.0518000
 0.0770600 0.0627600
 0.1037400 0.0731800
 0.1339300 0.0828400
 0.1673900 0.0915600
 0.2038200 0.0991700
 0.2429000 0.1055400
 0.2842600 0.1105600
 0.3275200 0.1141000
 0.3722500 0.1161000
 0.4180500 0.1164400
 0.4644800 0.1150400
 0.5112400 0.1118200
 0.5579900 0.1067800
 0.6044900 0.1000000
 0.6505001 0.0916000
 0.6955800 0.0819500
 0.7402400 0.0716300
 0.7829600 0.0611400
 0.8234000 0.0507900
 0.8609400 0.0409000
 0.8949900 0.0316800
 0.9249700 0.0233400
 0.9503400 0.0159500
 0.9708200 0.0094900
 0.9863500 0.0042900
 0.9964300 0.0010500
 1.0000000 0.0000000

 0.0000100 0.0008600
 0.0000100 -.0005600
 0.0000800 -.0012100
 0.0002100 -.0018300
 0.0004200 -.0023800
 0.0007300 -.0029000
 0.0011300 -.0034200
 0.0016300 -.0039300
 0.0028300 -.0049400
 0.0043100 -.0059500
 0.0069900 -.0074400
 0.0137400 -.0103000
 0.0297400 -.0147300
 0.0512200 -.0185100
 0.0779500 -.0216700
 0.1096500 -.0242500
 0.1459400 -.0263500
 0.1863400 -.0280300
 0.2303300 -.0293200
 0.2773700 -.0302400
 0.3268600 -.0308200
 0.3781700 -.0310500
 0.4306700 -.0309100
 0.4836900 -.0303600
 0.5365700 -.0293500
 0.5886600 -.0277800
 0.6393100 -.0255200
 0.6878501 -.0221100
 0.7345099 -.0168400
 0.7802700 -.0102900
 0.8248400 -.0041600
 0.8669100 0.0005400
 0.9051400 0.0034500
 0.9383000 0.0044500
 0.9651300 0.0037800
 0.9845600 0.0021700
 0.9961600 0.0006200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 582 AIRFOIL (e582-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e582-il50,00097.9 at α=10.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e582-il50,000520.7 at α=11.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e582-il100,000947.9 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e582-il100,000545.4 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e582-il200,000978 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e582-il200,000575 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   e582-il500,0009112 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e582-il500,0005106.9 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e582-il1,000,0009140.4 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e582-il1,000,0005128.2 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
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