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S6063 7.05% (s6063-il)

S6063 7.05% - Selig S6063 low Reynolds number airfoil


Airfoil s6063-il
Details Dat file Parser  
(s6063-il) S6063 7.05%
Selig S6063 low Reynolds number airfoil
Max thickness 7% at 29.4% chord.
Max camber 1.3% at 43.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
S6063 7.05%
     1.00000   0.00000
     0.99687   0.00017
     0.98758   0.00078
     0.97238   0.00197
     0.95160   0.00383
     0.92565   0.00638
     0.89500   0.00956
     0.86012   0.01328
     0.82151   0.01739
     0.77969   0.02175
     0.73513   0.02617
     0.68835   0.03050
     0.63984   0.03457
     0.59007   0.03827
     0.53954   0.04152
     0.48881   0.04424
     0.43838   0.04633
     0.38877   0.04774
     0.34047   0.04838
     0.29396   0.04823
     0.24968   0.04725
     0.20803   0.04544
     0.16941   0.04280
     0.13413   0.03938
     0.10252   0.03523
     0.07481   0.03044
     0.05123   0.02513
     0.03194   0.01943
     0.01708   0.01355
     0.00671   0.00772
     0.00088   0.00242
     0.00058  -0.00190
     0.00605  -0.00588
     0.01660  -0.00982
     0.03215  -0.01333
     0.05261  -0.01630
     0.07786  -0.01867
     0.10771  -0.02042
     0.14190  -0.02156
     0.18013  -0.02215
     0.22201  -0.02222
     0.26710  -0.02184
     0.31491  -0.02109
     0.36490  -0.02001
     0.41652  -0.01865
     0.46919  -0.01706
     0.52232  -0.01530
     0.57532  -0.01342
     0.62759  -0.01147
     0.67854  -0.00952
     0.72758  -0.00761
     0.77415  -0.00581
     0.81769  -0.00418
     0.85768  -0.00278
     0.89359  -0.00164
     0.92495  -0.00081
     0.95132  -0.00026
     0.97231   0.00002
     0.98758   0.00009
     0.99688   0.00004
     1.00000   0.00000
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Selig format dat file

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Polars for S6063 7.05% (s6063-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s6063-il50,000934.7 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s6063-il50,000534.7 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s6063-il100,000948.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s6063-il100,000545.3 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s6063-il200,000961.5 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s6063-il200,000553.4 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s6063-il500,000974.8 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s6063-il500,000560.2 at α=2°Mach=0 Ncrit=5Xfoil predictionDetails
   s6063-il1,000,000981.3 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s6063-il1,000,000568.1 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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