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E226 (10.19%) (e226-il)

E226 (10.19%) - Eppler E226 low Reynolds number airfoil


Airfoil e226-il
Details Dat file Parser  
(e226-il) E226 (10.19%)
Eppler E226 low Reynolds number airfoil
Max thickness 10.2% at 31.3% chord.
Max camber 0.5% at 56.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
E226  (10.19%)               
   1.00000  0.00000
   0.99661  0.00027
   0.98667  0.00122
   0.97072  0.00302
   0.94920  0.00560
   0.92248  0.00888
   0.89101  0.01283
   0.85529  0.01736
   0.81585  0.02231
   0.77319  0.02753
   0.72785  0.03285
   0.68037  0.03809
   0.63128  0.04310
   0.58110  0.04770
   0.53037  0.05176
   0.47961  0.05514
   0.42931  0.05772
   0.37997  0.05942
   0.33207  0.06016
   0.28605  0.05989
   0.24234  0.05859
   0.20132  0.05625
   0.16335  0.05289
   0.12877  0.04858
   0.09785  0.04339
   0.07084  0.03743
   0.04797  0.03083
   0.02939  0.02376
   0.01521  0.01644
   0.00553  0.00915
   0.00044  0.00242
   0.00105 -0.00350
   0.00756 -0.00935
   0.01903 -0.01539
   0.03525 -0.02118
   0.05608 -0.02648
   0.08138 -0.03114
   0.11096 -0.03504
   0.14459 -0.03810
   0.18199 -0.04029
   0.22285 -0.04160
   0.26679 -0.04205
   0.31341 -0.04167
   0.36225 -0.04055
   0.41281 -0.03876
   0.46457 -0.03639
   0.51697 -0.03355
   0.56943 -0.03034
   0.62138 -0.02688
   0.67223 -0.02327
   0.72137 -0.01963
   0.76824 -0.01607
   0.81224 -0.01270
   0.85283 -0.00963
   0.88945 -0.00692
   0.92159 -0.00467
   0.94873 -0.00286
   0.97049 -0.00146
   0.98659 -0.00051
   0.99659 -0.00009
   1.00000  0.00000
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Polars for E226 (10.19%) (e226-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e226-il50,000930.4 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e226-il50,000532.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e226-il100,000945.3 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e226-il100,000544.2 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e226-il200,000959.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   e226-il200,000555.3 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e226-il500,000977.1 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e226-il500,000567.3 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e226-il1,000,000986.8 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e226-il1,000,000573.4 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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