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E63 (4.25%) (e63-il)

E63 (4.25%) - Eppler E63 low Reynolds number airfoil


Airfoil e63-il
Details Dat file Parser  
(e63-il) E63 (4.25%)
Eppler E63 low Reynolds number airfoil
Max thickness 4.3% at 22.8% chord.
Max camber 5.3% at 50.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
E63  (4.25%)                 
   1.00000  0.00000
   0.99719  0.00121
   0.98938  0.00473
   0.97751  0.00986
   0.96173  0.01553
   0.94164  0.02126
   0.91717  0.02709
   0.88861  0.03301
   0.85624  0.03885
   0.82039  0.04451
   0.78141  0.04985
   0.73968  0.05480
   0.69562  0.05921
   0.64967  0.06304
   0.60229  0.06617
   0.55394  0.06857
   0.50509  0.07016
   0.45624  0.07094
   0.40786  0.07084
   0.36043  0.06990
   0.31441  0.06809
   0.27026  0.06545
   0.22840  0.06198
   0.18920  0.05775
   0.15304  0.05280
   0.12023  0.04723
   0.09103  0.04111
   0.06568  0.03457
   0.04435  0.02775
   0.02714  0.02083
   0.01416  0.01404
   0.00536  0.00766
   0.00076  0.00218
   0.00055 -0.00141
   0.00557 -0.00306
   0.01651 -0.00330
   0.03316 -0.00227
   0.05550 -0.00004
   0.08342  0.00315
   0.11671  0.00708
   0.15504  0.01151
   0.19800  0.01620
   0.24509  0.02093
   0.29574  0.02546
   0.34931  0.02962
   0.40513  0.03319
   0.46247  0.03605
   0.52056  0.03803
   0.57859  0.03907
   0.63576  0.03907
   0.69125  0.03806
   0.74430  0.03604
   0.79414  0.03310
   0.84004  0.02930
   0.88132  0.02482
   0.91735  0.01979
   0.94756  0.01439
   0.97115  0.00887
   0.98754  0.00410
   0.99695  0.00102
   1.00000  0.00000
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Polars for E63 (4.25%) (e63-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e63-il50,000952 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e63-il50,000551.1 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e63-il100,000977.5 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   e63-il100,000577.6 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e63-il200,0009112.5 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e63-il200,0005110 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   e63-il500,0009176.8 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e63-il500,0005160 at α=1°Mach=0 Ncrit=5Xfoil predictionDetails
   e63-il1,000,0009235.2 at α=1.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e63-il1,000,0005157.7 at α=0°Mach=0 Ncrit=5Xfoil predictionDetails
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