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E210 (13.64%) (e210-il)

E210 (13.64%) - Eppler E210 low Reynolds number airfoil


Airfoil e210-il
Details Dat file Parser  
(e210-il) E210 (13.64%)
Eppler E210 low Reynolds number airfoil
Max thickness 13.6% at 32.1% chord.
Max camber 3.7% at 50.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
E210  (13.64%)               
   1.00000  0.00000
   0.99649  0.00099
   0.98657  0.00414
   0.97139  0.00936
   0.95177  0.01587
   0.92780  0.02285
   0.89930  0.03003
   0.86643  0.03752
   0.82966  0.04531
   0.78948  0.05329
   0.74640  0.06133
   0.70096  0.06928
   0.65374  0.07698
   0.60532  0.08427
   0.55630  0.09093
   0.50729  0.09677
   0.45890  0.10148
   0.41157  0.10470
   0.36556  0.10619
   0.32115  0.10583
   0.27857  0.10360
   0.23805  0.09952
   0.19976  0.09375
   0.16395  0.08656
   0.13099  0.07822
   0.10119  0.06893
   0.07485  0.05890
   0.05220  0.04836
   0.03344  0.03755
   0.01874  0.02675
   0.00820  0.01630
   0.00192  0.00664
   0.00011 -0.00142
   0.00415 -0.00786
   0.01439 -0.01363
   0.02986 -0.01884
   0.05040 -0.02327
   0.07585 -0.02686
   0.10596 -0.02961
   0.14043 -0.03150
   0.17889 -0.03256
   0.22092 -0.03282
   0.26604 -0.03226
   0.31370 -0.03090
   0.36333 -0.02858
   0.41467 -0.02499
   0.46778 -0.02034
   0.52228 -0.01529
   0.57738 -0.01033
   0.63227 -0.00574
   0.68610 -0.00175
   0.73807  0.00150
   0.78735  0.00390
   0.83317  0.00541
   0.87478  0.00603
   0.91146  0.00582
   0.94253  0.00486
   0.96733  0.00340
   0.98536  0.00181
   0.99632  0.00051
   1.00000  0.00000
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Polars for E210 (13.64%) (e210-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e210-il50,00099.8 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e210-il50,000530.8 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   e210-il100,000952.7 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e210-il100,000557.1 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   e210-il200,000978.7 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e210-il200,000579.6 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e210-il500,0009113 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e210-il500,0005109 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e210-il1,000,0009140.3 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e210-il1,000,0005129.5 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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