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E211 (10.96%) (e211-il)

E211 (10.96%) - Eppler E211 low Reynolds number airfoil


Airfoil e211-il
Details Dat file Parser  
(e211-il) E211 (10.96%)
Eppler E211 low Reynolds number airfoil
Max thickness 10.9% at 31.7% chord.
Max camber 2.2% at 65.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
E211  (10.96%)               
   1.00000  0.00000
   0.99661  0.00083
   0.98698  0.00349
   0.97215  0.00790
   0.95287  0.01337
   0.92926  0.01912
   0.90115  0.02488
   0.86867  0.03076
   0.83226  0.03676
   0.79235  0.04280
   0.74945  0.04877
   0.70407  0.05457
   0.65674  0.06008
   0.60804  0.06518
   0.55854  0.06971
   0.50883  0.07350
   0.45942  0.07633
   0.41073  0.07801
   0.36317  0.07847
   0.31712  0.07762
   0.27292  0.07547
   0.23088  0.07207
   0.19136  0.06758
   0.15474  0.06214
   0.12140  0.05585
   0.09165  0.04885
   0.06576  0.04127
   0.04396  0.03325
   0.02640  0.02497
   0.01320  0.01668
   0.00444  0.00870
   0.00018  0.00159
   0.00158 -0.00429
   0.00896 -0.00967
   0.02148 -0.01482
   0.03902 -0.01942
   0.06146 -0.02337
   0.08862 -0.02662
   0.12024 -0.02916
   0.15602 -0.03099
   0.19558 -0.03213
   0.23849 -0.03260
   0.28427 -0.03242
   0.33238 -0.03159
   0.38226 -0.03009
   0.43329 -0.02779
   0.48515 -0.02441
   0.53783 -0.02006
   0.59098 -0.01530
   0.64391 -0.01057
   0.69589 -0.00618
   0.74615 -0.00238
   0.79390  0.00064
   0.83834  0.00278
   0.87873  0.00398
   0.91432  0.00429
   0.94443  0.00381
   0.96844  0.00277
   0.98589  0.00152
   0.99646  0.00044
   1.00000  0.00000
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Selig format dat file

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Polars for E211 (10.96%) (e211-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e211-il50,000937.9 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e211-il50,000539.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e211-il100,000958.3 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e211-il100,000557.6 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e211-il200,000978.9 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e211-il200,000574.7 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   e211-il500,0009106.1 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e211-il500,000591.7 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e211-il1,000,0009118.1 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e211-il1,000,0005100.7 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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