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EPPLER 548 AIRFOIL (e548-il)

EPPLER 548 AIRFOIL - Eppler E548 general aviation airfoil


Airfoil e548-il
Details Dat file Parser  
(e548-il) EPPLER 548 AIRFOIL
Eppler E548 general aviation airfoil
Max thickness 17.4% at 35.4% chord.
Max camber 2.2% at 26.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 548 AIRFOIL
       35.       38.

 0.0000100 0.0003000
 0.0001100 0.0019400
 0.0004200 0.0036800
 0.0012500 0.0064400
 0.0030400 0.0104100
 0.0105800 0.0209400
 0.0224600 0.0321000
 0.0385200 0.0434700
 0.0586100 0.0546700
 0.0825500 0.0654200
 0.1101100 0.0754600
 0.1410300 0.0845600
 0.1750100 0.0925200
 0.2117100 0.0991200
 0.2507500 0.1041700
 0.2917200 0.1073800
 0.3343200 0.1083900
 0.3785100 0.1068700
 0.4245200 0.1028100
 0.4723600 0.0967800
 0.5215600 0.0893300
 0.5715700 0.0808700
 0.6217900 0.0717800
 0.6715900 0.0624400
 0.7202700 0.0531800
 0.7671100 0.0442800
 0.8113700 0.0359900
 0.8523400 0.0284700
 0.8893200 0.0218300
 0.9216600 0.0161000
 0.9488201 0.0112700
 0.9702700 0.0071300
 0.9860600 0.0034700
 0.9963000 0.0008700
 1.0000000 0.0000000

 0.0000100 0.0003000
 0.0000300 -.0004700
 0.0001300 -.0012000
 0.0003000 -.0018900
 0.0005700 -.0025500
 0.0009500 -.0032200
 0.0014100 -.0038900
 0.0025400 -.0052600
 0.0039300 -.0066400
 0.0064900 -.0087500
 0.0130400 -.0130100
 0.0283700 -.0201800
 0.0488500 -.0271600
 0.0741700 -.0338400
 0.1040500 -.0401100
 0.1381200 -.0459500
 0.1759300 -.0513200
 0.2169600 -.0561400
 0.2606900 -.0602900
 0.3066000 -.0636900
 0.3541100 -.0662000
 0.4026700 -.0677000
 0.4517000 -.0680400
 0.5006100 -.0670400
 0.5487800 -.0642600
 0.5962200 -.0590700
 0.6435100 -.0514500
 0.6910100 -.0422400
 0.7384101 -.0326300
 0.7847900 -.0235800
 0.8291300 -.0156700
 0.8703600 -.0092800
 0.9074200 -.0045900
 0.9393000 -.0015800
 0.9651300 0.0000100
 0.9842401 0.0004600
 0.9960200 0.0002200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 548 AIRFOIL (e548-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e548-il50,000913.1 at α=-1.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e548-il50,000510.8 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e548-il100,000934.1 at α=12°Mach=0 Ncrit=9Xfoil predictionDetails
   e548-il100,000538.6 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e548-il200,000961.8 at α=10.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e548-il200,000563.4 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e548-il500,000993.7 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e548-il500,000590.7 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   e548-il1,000,0009117.2 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   e548-il1,000,0005108.8 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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