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S2060 8% (s2060-il)

S2060 8% - Selig S2060 low Reynolds number airfoil


Airfoil s2060-il
Details Dat file Parser  
(s2060-il) S2060 8%
Selig S2060 low Reynolds number airfoil
Max thickness 8% at 30.2% chord.
Max camber 1.6% at 49.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
     S2060 8%
     1.00000   0.00000
     0.99677   0.00040
     0.98734   0.00172
     0.97223   0.00403
     0.95191   0.00714
     0.92667   0.01085
     0.89683   0.01507
     0.86281   0.01971
     0.82508   0.02465
     0.78414   0.02972
     0.74048   0.03470
     0.69451   0.03941
     0.64668   0.04372
     0.59747   0.04756
     0.54740   0.05083
     0.49698   0.05345
     0.44671   0.05536
     0.39710   0.05649
     0.34866   0.05682
     0.30186   0.05631
     0.25718   0.05495
     0.21505   0.05274
     0.17587   0.04968
     0.13999   0.04579
     0.10772   0.04112
     0.07931   0.03575
     0.05499   0.02980
     0.03493   0.02340
     0.01923   0.01676
     0.00802   0.01015
     0.00142   0.00395
     0.00021  -0.00149
     0.00446  -0.00665
     0.01350  -0.01170
     0.02734  -0.01600
     0.04616  -0.01942
     0.06994  -0.02199
     0.09852  -0.02379
     0.13165  -0.02489
     0.16900  -0.02535
     0.21020  -0.02524
     0.25478  -0.02467
     0.30224  -0.02367
     0.35205  -0.02233
     0.40363  -0.02070
     0.45638  -0.01883
     0.50968  -0.01676
     0.56291  -0.01447
     0.61557  -0.01192
     0.66723  -0.00924
     0.71731  -0.00667
     0.76516  -0.00438
     0.81011  -0.00245
     0.85154  -0.00094
     0.88886   0.00012
     0.92154   0.00074
     0.94908   0.00095
     0.97103   0.00083
     0.98701   0.00051
     0.99673   0.00016
     1.00000   0.00000
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Selig format dat file

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Polars for S2060 8% (s2060-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s2060-il50,000936.4 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s2060-il50,000536.9 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   s2060-il100,000953.6 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s2060-il100,000550.6 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s2060-il200,000970.9 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   s2060-il200,000562.9 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   s2060-il500,000991 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   s2060-il500,000575.1 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s2060-il1,000,0009101.5 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s2060-il1,000,000579 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
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