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EPPLER 395 AIRFOIL (e395-il)

EPPLER 395 AIRFOIL - Eppler E395 human e664ered aircraft airfoil


Airfoil e395-il
Details Dat file Parser  
(e395-il) EPPLER 395 AIRFOIL
Eppler E395 human e664ered aircraft airfoil
Max thickness 12.3% at 29.5% chord.
Max camber 5.2% at 52.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 395 AIRFOIL
       37.       36.

 0.0000100 0.0001300
 0.0000400 0.0008100
 0.0002900 0.0022500
 0.0007300 0.0037800
 0.0017500 0.0062300
 0.0032300 0.0089100
 0.0108800 0.0183300
 0.0228100 0.0285000
 0.0389100 0.0389900
 0.0590600 0.0494800
 0.0830900 0.0597000
 0.1108200 0.0694300
 0.1420000 0.0784500
 0.1763600 0.0866000
 0.2135800 0.0937200
 0.2533100 0.0996700
 0.2951600 0.1043000
 0.3387600 0.1074800
 0.3837500 0.1090800
 0.4297600 0.1090400
 0.4764500 0.1073200
 0.5234600 0.1039500
 0.5704500 0.0989700
 0.6171000 0.0924800
 0.6631700 0.0847000
 0.7083100 0.0760100
 0.7520000 0.0667800
 0.7937300 0.0573300
 0.8329500 0.0479700
 0.8691100 0.0389400
 0.9016800 0.0304800
 0.9301300 0.0227700
 0.9539500 0.0158400
 0.9729800 0.0096000
 0.9873400 0.0044000
 0.9966900 0.0010800
 1.0000000 0.0000000

 0.0000100 0.0001300
 0.0000200 -.0005200
 0.0001100 -.0011200
 0.0003000 -.0017100
 0.0005800 -.0023000
 0.0009300 -.0029000
 0.0018300 -.0041100
 0.0029500 -.0053400
 0.0050400 -.0072000
 0.0115400 -.0113800
 0.0250500 -.0168500
 0.0433600 -.0213400
 0.0664100 -.0246800
 0.0940800 -.0267400
 0.1262600 -.0275000
 0.1627400 -.0269600
 0.2033000 -.0252000
 0.2476600 -.0223400
 0.2954800 -.0185900
 0.3463100 -.0142100
 0.3996000 -.0094900
 0.4547200 -.0046600
 0.5109900 0.0000300
 0.5677000 0.0043600
 0.6240900 0.0081200
 0.6793600 0.0111200
 0.7327200 0.0132400
 0.7833400 0.0143700
 0.8304100 0.0144600
 0.8731400 0.0135600
 0.9107600 0.0117400
 0.9425800 0.0091400
 0.9678299 0.0060100
 0.9858400 0.0029600
 0.9964900 0.0007800
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 395 AIRFOIL (e395-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e395-il50,000931 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e395-il50,000528.2 at α=9.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e395-il100,000959.8 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e395-il100,000561.4 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e395-il200,000992.1 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e395-il200,000592 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e395-il500,0009136.4 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e395-il500,0005128.5 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e395-il1,000,0009169.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e395-il1,000,0005144.1 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
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