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E186 (10.27%) (e186-il)

E186 (10.27%) - Eppler E186 low Reynolds number airfoil


Airfoil e186-il
Details Dat file Parser  
(e186-il) E186 (10.27%)
Eppler E186 low Reynolds number airfoil
Max thickness 10.2% at 29% chord.
Max camber 0.8% at 29% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
E186  (10.27%)               
   1.00000  0.00000
   0.99654 -0.00021
   0.98619 -0.00066
   0.96907 -0.00091
   0.94552 -0.00050
   0.91612  0.00085
   0.88154  0.00322
   0.84239  0.00663
   0.79936  0.01104
   0.75314  0.01637
   0.70447  0.02249
   0.65412  0.02922
   0.60283  0.03631
   0.55138  0.04346
   0.50052  0.05022
   0.45073  0.05600
   0.40224  0.06042
   0.35529  0.06327
   0.31007  0.06445
   0.26677  0.06396
   0.22558  0.06192
   0.18678  0.05861
   0.15079  0.05424
   0.11800  0.04895
   0.08874  0.04289
   0.06330  0.03620
   0.04191  0.02904
   0.02475  0.02159
   0.01196  0.01411
   0.00367  0.00694
   0.00004  0.00070
   0.00225 -0.00468
   0.01046 -0.01002
   0.02370 -0.01530
   0.04187 -0.02018
   0.06484 -0.02455
   0.09244 -0.02833
   0.12444 -0.03149
   0.16054 -0.03404
   0.20040 -0.03597
   0.24360 -0.03732
   0.28968 -0.03812
   0.33815 -0.03839
   0.38847 -0.03819
   0.44007 -0.03754
   0.49239 -0.03649
   0.54483 -0.03507
   0.59681 -0.03332
   0.64773 -0.03127
   0.69702 -0.02896
   0.74414 -0.02643
   0.78854 -0.02372
   0.82972 -0.02088
   0.86723 -0.01793
   0.90062 -0.01493
   0.92952 -0.01190
   0.95357 -0.00881
   0.97275 -0.00555
   0.98725 -0.00255
   0.99667 -0.00061
   1.00000  0.00000
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Polars for E186 (10.27%) (e186-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e186-il50,000929.9 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e186-il50,000531.2 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e186-il100,000946 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   e186-il100,000545.3 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e186-il200,000961.9 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e186-il200,000558.1 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e186-il500,000979.7 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e186-il500,000571.1 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e186-il1,000,000990.7 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   e186-il1,000,000573.4 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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