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EPPLER 585 AIRFOIL (e585-il)

EPPLER 585 AIRFOIL - Eppler E585 sailplane airfoil


Airfoil e585-il
Details Dat file Parser  
(e585-il) EPPLER 585 AIRFOIL
Eppler E585 sailplane airfoil
Max thickness 14.6% at 37.6% chord.
Max camber 4.2% at 42.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 585 AIRFOIL
       35.       38.

 0.0000100 0.0009500
 0.0002100 0.0024800
 0.0008500 0.0049600
 0.0024100 0.0087000
 0.0091600 0.0186000
 0.0201200 0.0293700
 0.0351900 0.0405400
 0.0542800 0.0517300
 0.0772500 0.0626300
 0.1039400 0.0729800
 0.1341500 0.0825800
 0.1676100 0.0912400
 0.2040400 0.0987900
 0.2431200 0.1051000
 0.2844700 0.1100600
 0.3277200 0.1135500
 0.3724400 0.1155000
 0.4158000 0.1158000
 0.4646400 0.1143600
 0.5113800 0.1111100
 0.5581300 0.1060500
 0.6046000 0.0992500
 0.6506000 0.0908400
 0.6959700 0.0812000
 0.7403200 0.0709000
 0.7830500 0.0604200
 0.8234600 0.0501200
 0.8610100 0.0402700
 0.8950599 0.0311100
 0.9250500 0.0228400
 0.9504500 0.0155500
 0.9709300 0.0092100
 0.9864399 0.0041600
 0.9964600 0.0010200
 1.0000000 0.0000000

 0.0000100 0.0009500
 0.0000100 -.0004700
 0.0000800 -.0011200
 0.0002100 -.0017300
 0.0004100 -.0022900
 0.0007100 -.0028100
 0.0011200 -.0033200
 0.0016100 -.0038300
 0.0028000 -.0048500
 0.0042700 -.0058600
 0.0069400 -.0073600
 0.0136000 -.0102100
 0.0294800 -.0146600
 0.0508200 -.0184700
 0.0773800 -.0216600
 0.1088800 -.0242600
 0.1449500 -.0263600
 0.1851000 -.0280300
 0.2288300 -.0292700
 0.2755800 -.0301200
 0.3247700 -.0305800
 0.3757700 -.0306400
 0.4279400 -.0302600
 0.4806300 -.0293900
 0.5331800 -.0279300
 0.5849300 -.0256400
 0.6355800 -.0221300
 0.6851600 -.0173800
 0.7336500 -.0117600
 0.7809300 -.0059700
 0.8263000 -.0010100
 0.8685800 0.0025400
 0.9066200 0.0044900
 0.9393600 0.0048500
 0.9657200 0.0038500
 0.9848000 0.0021500
 0.9962200 0.0006100
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 585 AIRFOIL (e585-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e585-il50,00098 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e585-il50,000521.2 at α=12°Mach=0 Ncrit=5Xfoil predictionDetails
   e585-il100,000950.3 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e585-il100,000547.7 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e585-il200,000981.4 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   e585-il200,000578.6 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e585-il500,0009118 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e585-il500,0005110.5 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e585-il1,000,0009146.1 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e585-il1,000,0005131.3 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
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