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S1014 (s1014-il)

S1014 - Selig S1014 HPV airfoil


Airfoil s1014-il
Details Dat file Parser  
(s1014-il) S1014
Selig S1014 HPV airfoil
Max thickness 16.5% at 42.2% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
S1014
     1.00000   0.00000
     0.99610   0.00022
     0.98465   0.00119
     0.96622   0.00341
     0.94151   0.00710
     0.91119   0.01238
     0.87604   0.01936
     0.83705   0.02802
     0.79532   0.03806
     0.75202   0.04895
     0.70829   0.05951
     0.66413   0.06797
     0.61835   0.07380
     0.57065   0.07784
     0.52167   0.08056
     0.47199   0.08210
     0.42222   0.08254
     0.37293   0.08195
     0.32472   0.08040
     0.27812   0.07791
     0.23370   0.07455
     0.19197   0.07037
     0.15346   0.06540
     0.11862   0.05966
     0.08788   0.05315
     0.06153   0.04581
     0.03978   0.03765
     0.02271   0.02873
     0.01032   0.01922
     0.00265   0.00944
     0.00000   0.00000
     0.00265  -0.00944
     0.01032  -0.01922
     0.02271  -0.02873
     0.03978  -0.03765
     0.06153  -0.04581
     0.08788  -0.05315
     0.11862  -0.05966
     0.15346  -0.06540
     0.19197  -0.07037
     0.23370  -0.07455
     0.27812  -0.07791
     0.32472  -0.08040
     0.37293  -0.08195
     0.42222  -0.08254
     0.47199  -0.08210
     0.52167  -0.08056
     0.57065  -0.07784
     0.61835  -0.07380
     0.66413  -0.06797
     0.70829  -0.05951
     0.75202  -0.04895
     0.79532  -0.03806
     0.83705  -0.02802
     0.87604  -0.01936
     0.91119  -0.01238
     0.94151  -0.00710
     0.96622  -0.00341
     0.98465  -0.00119
     0.99610  -0.00022
     1.00000   0.00000
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Lednicer format dat file
Selig format dat file

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Polars for S1014 (s1014-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s1014-il50,000927 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s1014-il50,000520.3 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s1014-il100,000938.2 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   s1014-il100,000523.2 at α=10.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s1014-il200,000933.7 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s1014-il200,000530.3 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s1014-il500,000945.8 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s1014-il500,000542 at α=9.5°Mach=0 Ncrit=5Xfoil predictionDetails
   s1014-il1,000,000954.9 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s1014-il1,000,000552.6 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
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