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S1012 (s1012-il)

S1012 - Selig S1012 HPV airfoil


Airfoil s1012-il
Details Dat file Parser  
(s1012-il) S1012
Selig S1012 HPV airfoil
Max thickness 12% at 37.3% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
S1012
     1.00000   0.00000
     0.99640   0.00018
     0.98580   0.00094
     0.96872   0.00264
     0.94571   0.00536
     0.91728   0.00912
     0.88401   0.01398
     0.84664   0.01993
     0.80601   0.02677
     0.76300   0.03416
     0.71846   0.04139
     0.67266   0.04740
     0.62512   0.05182
     0.57587   0.05510
     0.52548   0.05748
     0.47451   0.05907
     0.42356   0.05994
     0.37324   0.06011
     0.32414   0.05961
     0.27682   0.05846
     0.23184   0.05667
     0.18974   0.05425
     0.15105   0.05120
     0.11622   0.04747
     0.08566   0.04299
     0.05966   0.03766
     0.03835   0.03142
     0.02177   0.02428
     0.00984   0.01640
     0.00251   0.00810
     0.00000   0.00000
     0.00251  -0.00810
     0.00984  -0.01640
     0.02177  -0.02428
     0.03835  -0.03142
     0.05966  -0.03766
     0.08566  -0.04299
     0.11622  -0.04747
     0.15105  -0.05120
     0.18974  -0.05425
     0.23184  -0.05667
     0.27682  -0.05846
     0.32414  -0.05961
     0.37324  -0.06011
     0.42356  -0.05994
     0.47451  -0.05907
     0.52548  -0.05748
     0.57587  -0.05510
     0.62512  -0.05182
     0.67266  -0.04740
     0.71846  -0.04139
     0.76300  -0.03416
     0.80601  -0.02677
     0.84664  -0.01993
     0.88401  -0.01398
     0.91728  -0.00912
     0.94571  -0.00536
     0.96872  -0.00264
     0.98580  -0.00094
     0.99640  -0.00018
     1.00000   0.00000
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Lednicer format dat file
Selig format dat file

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Polars for S1012 (s1012-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s1012-il50,000926.2 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s1012-il50,000525.5 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s1012-il100,000937.2 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s1012-il100,000531.1 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s1012-il200,000937.7 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s1012-il200,000540 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s1012-il500,000953.5 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s1012-il500,000556.8 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s1012-il1,000,000969.9 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s1012-il1,000,000570.3 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
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