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S1010 HPV airfoil (s1010-il)

S1010 HPV airfoil - Selig S1010 HPV airfoil


Airfoil s1010-il
Details Dat file Parser  
(s1010-il) S1010 HPV airfoil
Selig S1010 HPV airfoil
Max thickness 6% at 23.3% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
S1010 HPV airfoil
     1.00000   0.00000
     0.99681   0.00011
     0.98742   0.00058
     0.97219   0.00153
     0.95153   0.00292
     0.92572   0.00466
     0.89507   0.00673
     0.86004   0.00916
     0.82114   0.01188
     0.77893   0.01477
     0.73398   0.01763
     0.68672   0.02014
     0.63738   0.02220
     0.58637   0.02394
     0.53426   0.02546
     0.48168   0.02678
     0.42926   0.02790
     0.37759   0.02883
     0.32731   0.02952
     0.27899   0.02996
     0.23322   0.03011
     0.19053   0.02992
     0.15147   0.02931
     0.11647   0.02816
     0.08589   0.02633
     0.05996   0.02363
     0.03869   0.02003
     0.02209   0.01557
     0.01007   0.01044
     0.00259   0.00500
     0.00000   0.00000
     0.00259  -0.00500
     0.01007  -0.01044
     0.02209  -0.01557
     0.03869  -0.02003
     0.05996  -0.02363
     0.08589  -0.02633
     0.11647  -0.02816
     0.15147  -0.02931
     0.19053  -0.02992
     0.23322  -0.03011
     0.27899  -0.02996
     0.32731  -0.02952
     0.37759  -0.02883
     0.42926  -0.02790
     0.48168  -0.02678
     0.53426  -0.02546
     0.58637  -0.02394
     0.63738  -0.02220
     0.68672  -0.02014
     0.73398  -0.01763
     0.77893  -0.01477
     0.82114  -0.01188
     0.86004  -0.00916
     0.89507  -0.00673
     0.92572  -0.00466
     0.95153  -0.00292
     0.97219  -0.00153
     0.98742  -0.00058
     0.99681  -0.00011
     1.00000   0.00000
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Selig format dat file

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Polars for S1010 HPV airfoil (s1010-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s1010-il50,000920.4 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s1010-il50,000521.3 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   s1010-il100,000929.5 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s1010-il100,000529.9 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   s1010-il200,000937.3 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   s1010-il200,000540.1 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   s1010-il500,000953.1 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   s1010-il500,000555.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s1010-il1,000,000966.3 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   s1010-il1,000,000569.2 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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