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S1016 (s1016-il)

S1016 - Selig S1016 HPV airfoil


Airfoil s1016-il
Details Dat file Parser  
(s1016-il) S1016
Selig S1016 HPV airfoil
Max thickness 17.5% at 41.8% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
S1016
     1.00000   0.00000
     0.99598   0.00024
     0.98419   0.00132
     0.96527   0.00383
     0.93999   0.00803
     0.90913   0.01406
     0.87362   0.02204
     0.83461   0.03184
     0.79341   0.04301
     0.75133   0.05437
     0.70854   0.06404
     0.66386   0.07130
     0.61693   0.07689
     0.56837   0.08122
     0.51871   0.08437
     0.46855   0.08643
     0.41848   0.08742
     0.36907   0.08736
     0.32090   0.08627
     0.27453   0.08416
     0.23048   0.08103
     0.18925   0.07691
     0.15132   0.07179
     0.11710   0.06566
     0.08694   0.05853
     0.06108   0.05037
     0.03965   0.04127
     0.02273   0.03137
     0.01038   0.02091
     0.00267   0.01025
     0.00000   0.00000
     0.00267  -0.01025
     0.01038  -0.02091
     0.02273  -0.03137
     0.03965  -0.04127
     0.06108  -0.05037
     0.08694  -0.05853
     0.11710  -0.06566
     0.15132  -0.07179
     0.18925  -0.07691
     0.23048  -0.08103
     0.27453  -0.08416
     0.32090  -0.08627
     0.36907  -0.08736
     0.41848  -0.08742
     0.46855  -0.08643
     0.51871  -0.08437
     0.56837  -0.08122
     0.61693  -0.07689
     0.66386  -0.07130
     0.70854  -0.06404
     0.75133  -0.05437
     0.79341  -0.04301
     0.83461  -0.03184
     0.87362  -0.02204
     0.90913  -0.01406
     0.93999  -0.00803
     0.96527  -0.00383
     0.98419  -0.00132
     0.99598  -0.00024
     1.00000   0.00000
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Lednicer format dat file
Selig format dat file

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Polars for S1016 (s1016-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s1016-il50,000928.1 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   s1016-il50,000522.4 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s1016-il100,000939.2 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   s1016-il100,000523.5 at α=10.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s1016-il200,000935.3 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s1016-il200,000530.2 at α=10°Mach=0 Ncrit=5Xfoil predictionDetails
   s1016-il500,000940.1 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s1016-il500,000541.8 at α=10.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s1016-il1,000,000952.2 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s1016-il1,000,000552 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
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