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EPPLER 858 AIRFOIL (e858-il)

EPPLER 858 AIRFOIL - Eppler E858 propeller airfoil


Airfoil e858-il
Details Dat file Parser  
(e858-il) EPPLER 858 AIRFOIL
Eppler E858 propeller airfoil
Max thickness 22.7% at 26.6% chord.
Max camber 4.7% at 44.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 858 AIRFOIL
       34.       34.

 0.0000700 0.0020500
 0.0010800 0.0104000
 0.0034000 0.0188300
 0.0106000 0.0346800
 0.0216600 0.0511900
 0.0364600 0.0678600
 0.0548600 0.0842800
 0.0766700 0.1000800
 0.1016500 0.1148900
 0.1295200 0.1283300
 0.1599700 0.1399200
 0.1929100 0.1491500
 0.2283300 0.1556900
 0.2662200 0.1592800
 0.3067800 0.1599100
 0.3499500 0.1579400
 0.3953500 0.1537000
 0.4425900 0.1474500
 0.4912400 0.1394800
 0.5407900 0.1301200
 0.5906900 0.1197000
 0.6403500 0.1085500
 0.6891500 0.0969900
 0.7364000 0.0853200
 0.7814400 0.0738200
 0.8236000 0.0626900
 0.8622100 0.0521100
 0.8966000 0.0421700
 0.9263800 0.0329500
 0.9508100 0.0242400
 0.9700701 0.0155500
 0.9851300 0.0074100
 0.9958700 0.0018400
 1.0000000 0.0000000

 0.0000700 0.0020500
 0.0002700 -.0030600
 0.0009300 -.0065600
 0.0016700 -.0086800
 0.0027600 -.0106800
 0.0050000 -.0136700
 0.0089100 -.0176500
 0.0164800 -.0235500
 0.0231900 -.0277600
 0.0421000 -.0368500
 0.0657300 -.0450700
 0.0937900 -.0522400
 0.1259500 -.0582500
 0.1618000 -.0630000
 0.2008100 -.0663600
 0.2424700 -.0679900
 0.2865400 -.0673900
 0.3330800 -.0644100
 0.3821300 -.0591100
 0.4338100 -.0518800
 0.4878700 -.0436000
 0.5435500 -.0350000
 0.5999700 -.0266400
 0.6562100 -.0189500
 0.7112500 -.0122900
 0.7640899 -.0068700
 0.8136799 -.0028400
 0.8590400 -.0001700
 0.8992200 0.0012500
 0.9333799 0.0017700
 0.9610500 0.0018400
 0.9820000 0.0014700
 0.9953700 0.0005600
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 858 AIRFOIL (e858-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e858-il50,00093 at α=11.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e858-il50,000513 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e858-il100,000921.5 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e858-il100,000534.6 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e858-il200,000948.7 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e858-il200,000551.5 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e858-il500,000973.5 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e858-il500,000567.8 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e858-il1,000,000988.1 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e858-il1,000,000587.4 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
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