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E216 (10.4%) (e216-il)

E216 (10.4%) - Eppler E216 low Reynolds number airfoil


Airfoil e216-il
Details Dat file Parser  
(e216-il) E216 (10.4%)
Eppler E216 low Reynolds number airfoil
Max thickness 10.4% at 26.2% chord.
Max camber 4.7% at 59% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
E216  (10.4%)                
   1.00000  0.00000
   0.99692  0.00141
   0.98842  0.00552
   0.97564  0.01157
   0.95877  0.01840
   0.93743  0.02552
   0.91162  0.03300
   0.88170  0.04079
   0.84805  0.04868
   0.81104  0.05651
   0.77107  0.06407
   0.72855  0.07120
   0.68390  0.07773
   0.63757  0.08353
   0.59004  0.08847
   0.54177  0.09243
   0.49323  0.09532
   0.44490  0.09704
   0.39722  0.09754
   0.35064  0.09678
   0.30560  0.09475
   0.26249  0.09144
   0.22169  0.08690
   0.18354  0.08119
   0.14836  0.07439
   0.11644  0.06665
   0.08803  0.05809
   0.06333  0.04891
   0.04254  0.03930
   0.02576  0.02951
   0.01311  0.01981
   0.00461  0.01058
   0.00031  0.00238
   0.00108 -0.00385
   0.00769 -0.00866
   0.01979 -0.01291
   0.03703 -0.01630
   0.05924 -0.01869
   0.08628 -0.01999
   0.11795 -0.02020
   0.15401 -0.01932
   0.19420 -0.01742
   0.23817 -0.01460
   0.28554 -0.01098
   0.33588 -0.00675
   0.38868 -0.00210
   0.44341  0.00276
   0.49945  0.00757
   0.55614  0.01211
   0.61279  0.01611
   0.66862  0.01937
   0.72287  0.02167
   0.77471  0.02284
   0.82331  0.02277
   0.86782  0.02137
   0.90737  0.01863
   0.94105  0.01456
   0.96763  0.00945
   0.98608  0.00449
   0.99661  0.00113
   1.00000  0.00000
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Polars for E216 (10.4%) (e216-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e216-il50,000940.7 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   e216-il50,000543 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   e216-il100,000968.5 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   e216-il100,000568.5 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   e216-il200,000999.2 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   e216-il200,000594 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e216-il500,0009136.8 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e216-il500,0005115.8 at α=2°Mach=0 Ncrit=5Xfoil predictionDetails
   e216-il1,000,0009155.1 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e216-il1,000,0005127.4 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
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