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E205 (10.48%) (e205-il)

E205 (10.48%) - Eppler E205 low Reynolds number airfoil


Airfoil e205-il
Details Dat file Parser  
(e205-il) E205 (10.48%)
Eppler E205 low Reynolds number airfoil
Max thickness 10.5% at 29.7% chord.
Max camber 2.5% at 38.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
E205  (10.48%)               
   1.00000  0.00000
   0.99655  0.00039
   0.98649  0.00174
   0.97049  0.00427
   0.94916  0.00778
   0.92285  0.01196
   0.89175  0.01668
   0.85624  0.02199
   0.81684  0.02786
   0.77412  0.03419
   0.72866  0.04088
   0.68108  0.04777
   0.63204  0.05470
   0.58218  0.06147
   0.53217  0.06782
   0.48265  0.07342
   0.43410  0.07785
   0.38680  0.08081
   0.34101  0.08214
   0.29699  0.08177
   0.25496  0.07970
   0.21508  0.07606
   0.17764  0.07111
   0.14302  0.06507
   0.11157  0.05811
   0.08360  0.05040
   0.05937  0.04211
   0.03909  0.03344
   0.02292  0.02461
   0.01097  0.01589
   0.00331  0.00766
   0.00002  0.00055
   0.00233 -0.00506
   0.01065 -0.00988
   0.02419 -0.01420
   0.04291 -0.01776
   0.06669 -0.02053
   0.09534 -0.02252
   0.12864 -0.02378
   0.16627 -0.02436
   0.20783 -0.02435
   0.25290 -0.02384
   0.30097 -0.02292
   0.35149 -0.02168
   0.40388 -0.02021
   0.45751 -0.01859
   0.51174 -0.01689
   0.56591 -0.01516
   0.61938 -0.01345
   0.67149 -0.01180
   0.72160 -0.01023
   0.76911 -0.00876
   0.81343 -0.00740
   0.85400 -0.00614
   0.89034 -0.00497
   0.92195 -0.00380
   0.94860 -0.00252
   0.97017 -0.00125
   0.98635 -0.00036
   0.99651 -0.00003
   1.00000  0.00000
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Selig format dat file

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Polars for E205 (10.48%) (e205-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e205-il50,000932.6 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e205-il50,000534.5 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e205-il100,000953.9 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e205-il100,000554.9 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e205-il200,000975.6 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e205-il200,000574 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e205-il500,0009105.4 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e205-il500,000598.9 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e205-il1,000,0009128.3 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e205-il1,000,0005116.5 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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