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E182 (8.47%) (e182-il)

E182 (8.47%) - Eppler E182 low Reynolds number airfoil


Airfoil e182-il
Details Dat file Parser  
(e182-il) E182 (8.47%)
Eppler E182 low Reynolds number airfoil
Max thickness 8.5% at 32.4% chord.
Max camber 1.2% at 37.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
 E182 (8.47%)
   1.00000  0.00000
   0.99676 -0.00003
   0.98709 -0.00005
   0.97104  0.00018
   0.94881  0.00098
   0.92084  0.00268
   0.88780  0.00541
   0.85036  0.00913
   0.80913  0.01374
   0.76477  0.01911
   0.71797  0.02510
   0.66943  0.03148
   0.61985  0.03799
   0.56996  0.04421
   0.52016  0.04967
   0.47080  0.05408
   0.42219  0.05723
   0.37464  0.05902
   0.32838  0.05937
   0.28363  0.05843
   0.24083  0.05643
   0.20042  0.05348
   0.16285  0.04968
   0.12850  0.04512
   0.09771  0.03989
   0.07078  0.03409
   0.04796  0.02784
   0.02943  0.02127
   0.01529  0.01456
   0.00560  0.00802
   0.00048  0.00216
   0.00095 -0.00275
   0.00718 -0.00727
   0.01852 -0.01158
   0.03492 -0.01542
   0.05625 -0.01866
   0.08241 -0.02127
   0.11318 -0.02327
   0.14828 -0.02468
   0.18735 -0.02554
   0.23001 -0.02590
   0.27579 -0.02582
   0.32419 -0.02536
   0.37467 -0.02457
   0.42666 -0.02351
   0.47956 -0.02225
   0.53275 -0.02081
   0.58563 -0.01924
   0.63758 -0.01757
   0.68800 -0.01585
   0.73631 -0.01409
   0.78195 -0.01233
   0.82438 -0.01058
   0.86311 -0.00888
   0.89769 -0.00723
   0.92769 -0.00564
   0.95276 -0.00407
   0.97272 -0.00249
   0.98752 -0.00109
   0.99681 -0.00025
   1.00000  0.00000
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Polars for E182 (8.47%) (e182-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e182-il50,000932.8 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e182-il50,000534.1 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e182-il100,000948.5 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e182-il100,000547 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e182-il200,000964.1 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e182-il200,000558.8 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e182-il500,000981.9 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e182-il500,000571.3 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e182-il1,000,000992.7 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e182-il1,000,000578.2 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
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