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EPPLER 558 AIRFOIL (e558-il)

EPPLER 558 AIRFOIL - Eppler E558 general aviation airfoil


Airfoil e558-il
Details Dat file Parser  
(e558-il) EPPLER 558 AIRFOIL
Eppler E558 general aviation airfoil
Max thickness 16% at 26.4% chord.
Max camber 3.8% at 49.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 558 AIRFOIL
       33.       29.

 0.0007500 -.0043500
 0.0007700 0.0046500
 0.0060100 0.0155000
 0.0155100 0.0272500
 0.0291300 0.0393700
 0.0466900 0.0514700
 0.0680400 0.0632100
 0.0929700 0.0742600
 0.1212400 0.0843300
 0.1526500 0.0931200
 0.1869300 0.1003400
 0.2239400 0.1056900
 0.2635800 0.1090300
 0.3057000 0.1103500
 0.3500900 0.1097300
 0.3964500 0.1073700
 0.4443700 0.1034400
 0.4934200 0.0981500
 0.5431100 0.0917200
 0.5929400 0.0843800
 0.6423400 0.0764000
 0.6907499 0.0680100
 0.7375600 0.0594700
 0.7821600 0.0510000
 0.8239400 0.0427900
 0.8623000 0.0350000
 0.8966900 0.0277600
 0.9265700 0.0211200
 0.9514601 0.0150300
 0.9712999 0.0092700
 0.9864100 0.0042500
 0.9964100 0.0010300
 1.0000000 0.0000000

 0.0007500 -.0043500
 0.0068100 -.0124100
 0.0183600 -.0207500
 0.0345600 -.0288200
 0.0551100 -.0362000
 0.0798300 -.0425600
 0.1085100 -.0476700
 0.1409300 -.0513000
 0.1769300 -.0532200
 0.2164000 -.0533200
 0.2591900 -.0515900
 0.3051700 -.0481600
 0.3541300 -.0432600
 0.4058200 -.0372900
 0.4597000 -.0308400
 0.5150000 -.0243400
 0.5709100 -.0181100
 0.6265800 -.0123800
 0.6811799 -.0073500
 0.7338800 -.0031600
 0.7838500 0.0001100
 0.8303100 0.0024100
 0.8724900 0.0037400
 0.9096900 0.0041800
 0.9412300 0.0038300
 0.9665100 0.0028800
 0.9749700 0.0016200
 0.9962200 0.0004800
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 558 AIRFOIL (e558-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e558-il50,00099.5 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e558-il50,000529.7 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e558-il100,000941.2 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e558-il100,000550.9 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e558-il200,000967.7 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e558-il200,000570.9 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e558-il500,0009100.1 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e558-il500,000599.1 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e558-il1,000,0009127 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e558-il1,000,0005120.5 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
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