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EPPLER 393 AIRFOIL (e393-il)

EPPLER 393 AIRFOIL - Eppler E393 airfoil


Airfoil e393-il
Details Dat file Parser  
(e393-il) EPPLER 393 AIRFOIL
Eppler E393 airfoil
Max thickness 11.5% at 32.3% chord.
Max camber 4% at 46% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 393 AIRFOIL
       33.       30.

 0.0000000 0.0000000
 0.0014500 0.0046300
 0.0074000 0.0128800
 0.0176700 0.0220100
 0.0321400 0.0315000
 0.0507700 0.0410200
 0.0734100 0.0503400
 0.0998800 0.0592300
 0.1299300 0.0675300
 0.1633100 0.0750500
 0.1996700 0.0816500
 0.2386600 0.0871600
 0.2798900 0.0914600
 0.3229200 0.0943400
 0.3674600 0.0955800
 0.4132800 0.0950600
 0.4601200 0.0928400
 0.5077100 0.0889800
 0.5557300 0.0836800
 0.6038900 0.0771900
 0.6517299 0.0699300
 0.6986200 0.0622200
 0.7439700 0.0543000
 0.7871800 0.0463700
 0.8276700 0.0386300
 0.8649099 0.0312200
 0.8983700 0.0242900
 0.9275700 0.0179100
 0.9522100 0.0120700
 0.9721900 0.0069700
 0.9872200 0.0030700
 0.9967200 0.0007400
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0002600 -.0017500
 0.0049000 -.0067600
 0.0155300 -.0114300
 0.0314500 -.0154400
 0.0525000 -.0186900
 0.0785200 -.0211600
 0.1092600 -.0228600
 0.1444000 -.0238400
 0.1835700 -.0241200
 0.2263100 -.0237500
 0.2721400 -.0227400
 0.3205100 -.0210700
 0.3709700 -.0186100
 0.4232000 -.0154000
 0.4768100 -.0116000
 0.5313700 -.0075000
 0.5862800 -.0034900
 0.6407500 0.0001400
 0.6939700 0.0032000
 0.7451700 0.0055800
 0.7935900 0.0071900
 0.8384700 0.0079900
 0.8791100 0.0080100
 0.9148600 0.0072900
 0.9450901 0.0059000
 0.9691200 0.0039800
 0.9863500 0.0019800
 0.9966100 0.0005200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 393 AIRFOIL (e393-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e393-il50,000935.4 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e393-il50,000535.3 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e393-il100,000960.6 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e393-il100,000562 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e393-il200,000987.5 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e393-il200,000586.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e393-il500,0009124.7 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   e393-il500,0005117.5 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   e393-il1,000,0009152.7 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e393-il1,000,0005135.4 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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