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E184 (8.33%) (e184-il)

E184 (8.33%) - Eppler E184 low Reynolds number airfoil


Airfoil e184-il
Details Dat file Parser  
(e184-il) E184 (8.33%)
Eppler E184 low Reynolds number airfoil
Max thickness 8.3% at 33.3% chord.
Max camber 0.8% at 38.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
E184  (8.33%)                
   1.00000  0.00000
   0.99676 -0.00015
   0.98705 -0.00052
   0.97084 -0.00086
   0.94823 -0.00075
   0.91969  0.00027
   0.88597  0.00242
   0.84781  0.00563
   0.80587  0.00981
   0.76081  0.01484
   0.71338  0.02055
   0.66428  0.02672
   0.61425  0.03306
   0.56400  0.03908
   0.51388  0.04433
   0.46424  0.04857
   0.41539  0.05158
   0.36763  0.05328
   0.32120  0.05362
   0.27634  0.05279
   0.23354  0.05101
   0.19328  0.04834
   0.15598  0.04490
   0.12204  0.04072
   0.09178  0.03591
   0.06552  0.03054
   0.04346  0.02472
   0.02580  0.01858
   0.01262  0.01229
   0.00397  0.00620
   0.00010  0.00091
   0.00189 -0.00382
   0.00938 -0.00854
   0.02188 -0.01302
   0.03935 -0.01707
   0.06166 -0.02058
   0.08869 -0.02350
   0.12020 -0.02584
   0.15590 -0.02760
   0.19544 -0.02882
   0.23841 -0.02952
   0.28437 -0.02976
   0.33280 -0.02958
   0.38317 -0.02902
   0.43492 -0.02814
   0.48747 -0.02698
   0.54020 -0.02557
   0.59253 -0.02396
   0.64387 -0.02217
   0.69362 -0.02025
   0.74122 -0.01823
   0.78612 -0.01613
   0.82782 -0.01400
   0.86584 -0.01185
   0.89973 -0.00972
   0.92911 -0.00763
   0.95362 -0.00555
   0.97313 -0.00343
   0.98765 -0.00154
   0.99683 -0.00036
   1.00000  0.00000
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Polars for E184 (8.33%) (e184-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e184-il50,000930.9 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   e184-il50,000531.7 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e184-il100,000944.4 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e184-il100,000543.2 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e184-il200,000958 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   e184-il200,000553.5 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e184-il500,000973.9 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e184-il500,000563.9 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e184-il1,000,000982.4 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e184-il1,000,000567 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
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