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E168 (12.45%) (e168-il)

E168 (12.45%) - Eppler E168 low Reynolds number airfoil


Airfoil e168-il
Details Dat file Parser  
(e168-il) E168 (12.45%)
Eppler E168 low Reynolds number airfoil
Max thickness 12.4% at 26.7% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
 E168  (12.45%)               
   1.00000  0.00000
   0.99649  0.00021
   0.98631  0.00108
   0.97018  0.00271
   0.94855  0.00476
   0.92146  0.00706
   0.88914  0.00979
   0.85210  0.01306
   0.81090  0.01691
   0.76616  0.02130
   0.71854  0.02615
   0.66871  0.03135
   0.61736  0.03673
   0.56516  0.04211
   0.51275  0.04728
   0.46075  0.05200
   0.40972  0.05606
   0.36019  0.05924
   0.31262  0.06134
   0.26739  0.06221
   0.22485  0.06177
   0.18536  0.05995
   0.14915  0.05672
   0.11641  0.05211
   0.08730  0.04627
   0.06198  0.03944
   0.04069  0.03187
   0.02363  0.02380
   0.01095  0.01550
   0.00287  0.00733
   0.00000  0.00000
   0.00287 -0.00733
   0.01095 -0.01550
   0.02363 -0.02380
   0.04069 -0.03187
   0.06198 -0.03944
   0.08730 -0.04627
   0.11641 -0.05211
   0.14915 -0.05672
   0.18536 -0.05995
   0.22485 -0.06177
   0.26739 -0.06221
   0.31262 -0.06134
   0.36019 -0.05924
   0.40972 -0.05606
   0.46075 -0.05200
   0.51275 -0.04728
   0.56516 -0.04211
   0.61736 -0.03673
   0.66871 -0.03135
   0.71854 -0.02615
   0.76616 -0.02130
   0.81090 -0.01691
   0.85210 -0.01306
   0.88914 -0.00979
   0.92146 -0.00706
   0.94855 -0.00476
   0.97018 -0.00271
   0.98631 -0.00108
   0.99649 -0.00021
   1.00000  0.00000
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Selig format dat file

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Polars for E168 (12.45%) (e168-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e168-il50,000922.6 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   e168-il50,000528 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e168-il100,000938.4 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e168-il100,000540.5 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e168-il200,000953.6 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e168-il200,000552.8 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e168-il500,000973 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e168-il500,000567.9 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e168-il1,000,000987 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e168-il1,000,000577.6 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
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