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E214 (11.1%) (e214-il)

E214 (11.1%) - Eppler E214 low Reynolds number airfoil


Airfoil e214-il
Details Dat file Parser  
(e214-il) E214 (11.1%)
Eppler E214 low Reynolds number airfoil
Max thickness 11.1% at 33.1% chord.
Max camber 3.7% at 56.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
E214  (11.1%)                
   1.00000  0.00000
   0.99669  0.00104
   0.98737  0.00422
   0.97312  0.00916
   0.95431  0.01501
   0.93081  0.02139
   0.90279  0.02833
   0.87072  0.03576
   0.83508  0.04344
   0.79626  0.05105
   0.75457  0.05841
   0.71040  0.06544
   0.66430  0.07207
   0.61682  0.07813
   0.56852  0.08344
   0.51991  0.08776
   0.47142  0.09093
   0.42346  0.09281
   0.37645  0.09332
   0.33076  0.09241
   0.28674  0.09008
   0.24474  0.08639
   0.20510  0.08142
   0.16816  0.07532
   0.13424  0.06822
   0.10365  0.06028
   0.07665  0.05168
   0.05349  0.04258
   0.03434  0.03321
   0.01934  0.02379
   0.00856  0.01465
   0.00210  0.00619
   0.00005 -0.00086
   0.00360 -0.00632
   0.01326 -0.01087
   0.02830 -0.01475
   0.04858 -0.01784
   0.07390 -0.02011
   0.10406 -0.02161
   0.13874 -0.02236
   0.17759 -0.02245
   0.22017 -0.02193
   0.26599 -0.02086
   0.31449 -0.01928
   0.36508 -0.01721
   0.41714 -0.01453
   0.47030 -0.01100
   0.52450 -0.00678
   0.57932 -0.00245
   0.63400  0.00155
   0.68770  0.00495
   0.73959  0.00756
   0.78883  0.00923
   0.83461  0.00994
   0.87612  0.00970
   0.91265  0.00862
   0.94352  0.00684
   0.96809  0.00461
   0.98582  0.00235
   0.99646  0.00065
   1.00000  0.00000
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Selig format dat file

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Polars for E214 (11.1%) (e214-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e214-il50,000937.9 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   e214-il50,000539.8 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e214-il100,000961.9 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e214-il100,000563.2 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   e214-il200,000987.6 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e214-il200,000584.9 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   e214-il500,0009121.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e214-il500,0005111.3 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e214-il1,000,0009145.9 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   e214-il1,000,0005122.2 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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