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E62 (5.62%) (e62-il)

E62 (5.62%) - Eppler E62 low Reynolds number airfoil


Airfoil e62-il
Details Dat file Parser  
(e62-il) E62 (5.62%)
Eppler E62 low Reynolds number airfoil
Max thickness 5.6% at 26.2% chord.
Max camber 5% at 49.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
E62  (5.62%)                 
   1.00000  0.00000
   0.99699  0.00098
   0.98840  0.00397
   0.97509  0.00876
   0.95764  0.01463
   0.93610  0.02086
   0.91030  0.02718
   0.88036  0.03363
   0.84665  0.04017
   0.80955  0.04667
   0.76951  0.05301
   0.72697  0.05905
   0.68242  0.06463
   0.63636  0.06957
   0.58925  0.07364
   0.54145  0.07669
   0.49334  0.07861
   0.44527  0.07939
   0.39768  0.07909
   0.35102  0.07778
   0.30578  0.07547
   0.26238  0.07222
   0.22126  0.06806
   0.18280  0.06308
   0.14736  0.05734
   0.11523  0.05094
   0.08672  0.04401
   0.06202  0.03667
   0.04133  0.02910
   0.02476  0.02148
   0.01238  0.01408
   0.00421  0.00720
   0.00024  0.00140
   0.00115 -0.00240
   0.00762 -0.00447
   0.01974 -0.00537
   0.03744 -0.00502
   0.06068 -0.00351
   0.08936 -0.00098
   0.12328  0.00236
   0.16216  0.00630
   0.20561  0.01060
   0.25315  0.01501
   0.30425  0.01928
   0.35828  0.02314
   0.41449  0.02626
   0.47195  0.02854
   0.52982  0.02996
   0.58733  0.03056
   0.64371  0.03032
   0.69823  0.02929
   0.75016  0.02750
   0.79879  0.02504
   0.84347  0.02198
   0.88357  0.01847
   0.91854  0.01462
   0.94785  0.01059
   0.97092  0.00656
   0.98725  0.00308
   0.99685  0.00078
   1.00000  0.00000
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Polars for E62 (5.62%) (e62-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e62-il50,000948 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e62-il50,000547.7 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e62-il100,000974.7 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e62-il100,000574.4 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   e62-il200,0009107.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e62-il200,0005104.1 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e62-il500,0009156.8 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e62-il500,0005141.7 at α=2°Mach=0 Ncrit=5Xfoil predictionDetails
   e62-il1,000,0009191.5 at α=1.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e62-il1,000,0005164.6 at α=1.5°Mach=0 Ncrit=5Xfoil predictionDetails
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