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EPPLER 49 AIRFOIL (e49-il)

EPPLER 49 AIRFOIL - Eppler E49 low Reynolds number airfoil


Airfoil e49-il
Details Dat file Parser  
(e49-il) EPPLER 49 AIRFOIL
Eppler E49 low Reynolds number airfoil
Max thickness 7.2% at 38.4% chord.
Max camber 6.5% at 62.2% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 49 AIRFOIL
      15.0      10.0
 
 0.0002000 0.0216700
 0.0032500 0.0275500
 0.0106500 0.0350900
 0.0377900 0.0525200
 0.0573200 0.0616200
 0.1385800 0.0863300
 0.2934500 0.1088000
 0.3843200 0.1143100
 0.6220800 0.1086800
 0.6676800 0.1042800
 0.8905500 0.0593500
 0.9378100 0.0375600
 0.9873600 0.0066800
 0.9966400 0.0016100
 1.0000000 0.0000000
 
 0.0002000 0.0216700
 0.0023000 0.0183600
 0.0110000 0.0167400
 0.3336100 0.0399300
 0.3901600 0.0422400
 0.4483800 0.0437000
 0.7861900 0.0330400
 0.9856000 0.0039800
 0.9963900 0.0010800
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for EPPLER 49 AIRFOIL (e49-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e49-il50,000937.5 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e49-il50,000534.3 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e49-il100,000956.6 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e49-il100,000550.9 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   e49-il200,000982.3 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   e49-il200,000565 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e49-il500,0009119.1 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e49-il1,000,0009155.5 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e49-il1,000,0005123.1 at α=0.75°Mach=0 Ncrit=5Xfoil predictionDetails
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