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EPPLER 555 AIRFOIL (e555-il)

EPPLER 555 AIRFOIL - Eppler E555 general aviation airfoil


Airfoil e555-il
Details Dat file Parser  
(e555-il) EPPLER 555 AIRFOIL
Eppler E555 general aviation airfoil
Max thickness 16% at 31.9% chord.
Max camber 2.6% at 67.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 555 AIRFOIL
       35.       38.

 0.0000100 0.0004100
 0.0001700 0.0020400
 0.0005400 0.0037500
 0.0014600 0.0064300
 0.0044200 0.0119000
 0.0131100 0.0220300
 0.0261600 0.0325100
 0.0434600 0.0429300
 0.0648600 0.0530000
 0.0902000 0.0624700
 0.1192800 0.0711300
 0.1518400 0.0788100
 0.1875900 0.0853400
 0.2261700 0.0905600
 0.2673100 0.0942700
 0.3107700 0.0963800
 0.3562300 0.0969400
 0.4032800 0.0959700
 0.4515600 0.0935300
 0.5006400 0.0897300
 0.5501000 0.0847200
 0.5994700 0.0786800
 0.6482599 0.0718100
 0.6959600 0.0643600
 0.7420300 0.0565500
 0.7859300 0.0486200
 0.8270800 0.0408200
 0.8649400 0.0332200
 0.8989400 0.0263200
 0.9285800 0.0199200
 0.9533800 0.0142300
 0.9729000 0.0091600
 0.9872100 0.0045600
 0.9965700 0.0011900
 1.0000000 0.0000000

 0.0000100 0.0004100
 0.0000100 -.0003700
 0.0000700 -.0011200
 0.0002100 -.0018200
 0.0004400 -.0025100
 0.0007700 -.0032100
 0.0011800 -.0039200
 0.0022000 -.0053600
 0.0034600 -.0068400
 0.0057900 -.0091000
 0.0098900 -.0123700
 0.0231900 -.0201600
 0.0413400 -.0278600
 0.0640500 -.0352500
 0.0910200 -.0421600
 0.1219000 -.0484600
 0.1562700 -.0540200
 0.1936600 -.0586400
 0.2335800 -.0620700
 0.2755100 -.0639700
 0.3192200 -.0637700
 0.3647800 -.0612400
 0.4122900 -.0563500
 0.4619400 -.0494300
 0.5135900 -.0412700
 0.5666400 -.0326000
 0.6203500 -.0239700
 0.6739100 -.0158900
 0.7264200 -.0087900
 0.7769200 -.0029900
 0.8244300 0.0013000
 0.8679600 0.0040100
 0.9065700 0.0051900
 0.9394000 0.0050200
 0.9656500 0.0038400
 0.9847000 0.0021500
 0.9961799 0.0006300
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 555 AIRFOIL (e555-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e555-il50,000927.8 at α=10.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e555-il50,000532.8 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e555-il100,000951.2 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e555-il100,000551.2 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e555-il200,000969.1 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e555-il200,000567.1 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e555-il500,000993.4 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e555-il500,000586.4 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   e555-il1,000,0009110.7 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   e555-il1,000,000599.7 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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