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E64 (8.45%) (e64-il)

E64 (8.45%) - Eppler E64 low Reynolds number airfoil


Airfoil e64-il
Details Dat file Parser  
(e64-il) E64 (8.45%)
Eppler E64 low Reynolds number airfoil
Max thickness 8.4% at 27.8% chord.
Max camber 2.9% at 56.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
E64  (8.45%)                 
   1.00000  0.00000
   0.99679  0.00076
   0.98761  0.00311
   0.97324  0.00686
   0.95409  0.01145
   0.93022  0.01659
   0.90185  0.02223
   0.86942  0.02829
   0.83336  0.03455
   0.79408  0.04081
   0.75200  0.04691
   0.70756  0.05267
   0.66122  0.05793
   0.61344  0.06257
   0.56469  0.06646
   0.51543  0.06950
   0.46615  0.07162
   0.41731  0.07275
   0.36938  0.07288
   0.32280  0.07197
   0.27803  0.07004
   0.23547  0.06710
   0.19553  0.06322
   0.15858  0.05844
   0.12494  0.05285
   0.09490  0.04653
   0.06872  0.03960
   0.04658  0.03221
   0.02863  0.02453
   0.01496  0.01680
   0.00560  0.00931
   0.00056  0.00258
   0.00075 -0.00255
   0.00675 -0.00664
   0.01818 -0.01038
   0.03477 -0.01348
   0.05640 -0.01582
   0.08293 -0.01735
   0.11415 -0.01810
   0.14979 -0.01809
   0.18954 -0.01740
   0.23300 -0.01610
   0.27973 -0.01431
   0.32924 -0.01212
   0.38098 -0.00965
   0.43439 -0.00701
   0.48884 -0.00434
   0.54370 -0.00173
   0.59831  0.00069
   0.65199  0.00284
   0.70409  0.00461
   0.75392  0.00595
   0.80082  0.00678
   0.84416  0.00709
   0.88331  0.00686
   0.91770  0.00612
   0.94675  0.00491
   0.96990  0.00333
   0.98661  0.00169
   0.99665  0.00046
   1.00000  0.00000
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Polars for E64 (8.45%) (e64-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e64-il50,000941.5 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e64-il50,000542.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   e64-il100,000964 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e64-il100,000562.3 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e64-il200,000988.4 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e64-il200,000581.8 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e64-il500,0009120.6 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   e64-il500,0005103.3 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e64-il1,000,0009140.7 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e64-il1,000,0005113.2 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
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