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E203 (13.64%) (e203-il)

E203 (13.64%) - Eppler E203 low Reynolds number airfoil


Airfoil e203-il
Details Dat file Parser  
(e203-il) E203 (13.64%)
Eppler E203 low Reynolds number airfoil
Max thickness 13.6% at 30.7% chord.
Max camber 2.3% at 54.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
E203  (13.64%)               
   1.00000  0.00000
   0.99645  0.00066
   0.98625  0.00282
   0.97030  0.00660
   0.94932  0.01158
   0.92361  0.01723
   0.89325  0.02333
   0.85854  0.02995
   0.82000  0.03705
   0.77819  0.04450
   0.73369  0.05217
   0.68712  0.05988
   0.63910  0.06741
   0.59028  0.07452
   0.54130  0.08087
   0.49264  0.08604
   0.44460  0.08973
   0.39748  0.09175
   0.35154  0.09203
   0.30704  0.09055
   0.26419  0.08742
   0.22332  0.08289
   0.18486  0.07717
   0.14920  0.07039
   0.11671  0.06271
   0.08772  0.05430
   0.06250  0.04532
   0.04128  0.03597
   0.02427  0.02648
   0.01161  0.01710
   0.00344  0.00823
   0.00002  0.00051
   0.00258 -0.00625
   0.01115 -0.01296
   0.02471 -0.01953
   0.04311 -0.02564
   0.06616 -0.03113
   0.09366 -0.03588
   0.12534 -0.03979
   0.16091 -0.04281
   0.19999 -0.04489
   0.24219 -0.04597
   0.28702 -0.04602
   0.33398 -0.04483
   0.38286 -0.04210
   0.43379 -0.03799
   0.48643 -0.03314
   0.54007 -0.02801
   0.59395 -0.02289
   0.64730 -0.01799
   0.69937 -0.01350
   0.74940 -0.00954
   0.79665 -0.00620
   0.84043 -0.00353
   0.88005 -0.00156
   0.91489 -0.00024
   0.94441  0.00051
   0.96813  0.00076
   0.98561  0.00060
   0.99636  0.00021
   1.00000  0.00000
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Selig format dat file

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Polars for E203 (13.64%) (e203-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e203-il50,000932 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e203-il50,000531.2 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e203-il100,000954.7 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e203-il100,000555 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e203-il200,000978.2 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e203-il200,000575.9 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e203-il500,0009109.4 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e203-il500,0005101.3 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e203-il1,000,0009132.4 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e203-il1,000,0005108.6 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
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