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E212 (10.55%) (e212-il)

E212 (10.55%) - Eppler E212 low Reynolds number airfoil


Airfoil e212-il
Details Dat file Parser  
(e212-il) E212 (10.55%)
Eppler E212 low Reynolds number airfoil
Max thickness 10.6% at 27.5% chord.
Max camber 2.5% at 61.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
E212  (10.55%)               
   1.00000  0.00000
   0.99676  0.00092
   0.98759  0.00372
   0.97346  0.00803
   0.95472  0.01307
   0.93124  0.01844
   0.90316  0.02418
   0.87085  0.03023
   0.83474  0.03645
   0.79525  0.04269
   0.75283  0.04881
   0.70796  0.05465
   0.66112  0.06008
   0.61282  0.06496
   0.56355  0.06915
   0.51383  0.07256
   0.46416  0.07507
   0.41502  0.07660
   0.36689  0.07708
   0.32023  0.07647
   0.27548  0.07473
   0.23303  0.07188
   0.19326  0.06794
   0.15651  0.06295
   0.12309  0.05701
   0.09327  0.05023
   0.06729  0.04275
   0.04534  0.03473
   0.02758  0.02636
   0.01410  0.01790
   0.00499  0.00967
   0.00032  0.00224
   0.00122 -0.00398
   0.00800 -0.00970
   0.01984 -0.01532
   0.03648 -0.02045
   0.05780 -0.02486
   0.08363 -0.02840
   0.11379 -0.03097
   0.14808 -0.03252
   0.18621 -0.03301
   0.22790 -0.03248
   0.27280 -0.03099
   0.32051 -0.02861
   0.37059 -0.02548
   0.42257 -0.02175
   0.47590 -0.01759
   0.53003 -0.01320
   0.58434 -0.00878
   0.63819 -0.00452
   0.69090 -0.00063
   0.74179  0.00271
   0.79016  0.00535
   0.83528  0.00713
   0.87643  0.00794
   0.91284  0.00776
   0.94382  0.00659
   0.96851  0.00458
   0.98615  0.00231
   0.99657  0.00061
   1.00000  0.00000
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Polars for E212 (10.55%) (e212-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e212-il50,000938.3 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e212-il50,000540.6 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   e212-il100,000959.9 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e212-il100,000558.8 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   e212-il200,000981.7 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e212-il200,000575.5 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   e212-il500,0009108.4 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e212-il500,000591.7 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e212-il1,000,0009119.8 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e212-il1,000,0005101 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
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