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SD5060 (9.5%) (sd5060-il)

SD5060 (9.5%) - Selig/Donovan SD5060 low Reynolds number airfoil


Airfoil sd5060-il
Details Dat file Parser  
(sd5060-il) SD5060 (9.5%)
Selig/Donovan SD5060 low Reynolds number airfoil
Max thickness 9.5% at 24.9% chord.
Max camber 2% at 48.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
  SD5060 (9.5%)
  1.00000  0.0
  0.99678  0.00023
  0.98720  0.00102
  0.97149  0.00256
  0.95002  0.00500
  0.92326  0.00838
  0.89173  0.01268
  0.85600  0.01778
  0.81664  0.02351
  0.77422  0.02967
  0.72929  0.03600
  0.68236  0.04227
  0.63396  0.04824
  0.58457  0.05370
  0.53465  0.05847
  0.48468  0.06239
  0.43508  0.06536
  0.38632  0.06730
  0.33882  0.06816
  0.29301  0.06793
  0.24931  0.06664
  0.20814  0.06433
  0.16992  0.06105
  0.13504  0.05683
  0.10383  0.05168
  0.07656  0.04565
  0.05343  0.03875
  0.03444  0.03104
  0.01954  0.02280
  0.00878  0.01443
  0.00223  0.00637
  0.00003 -0.00066
  0.00334 -0.00656
  0.01244 -0.01208
  0.02641 -0.01729
  0.04507 -0.02178
  0.06835 -0.02538
  0.09613 -0.02795
  0.12829 -0.02938
  0.16475 -0.02973
  0.20524 -0.02920
  0.24935 -0.02795
  0.29661 -0.02611
  0.34651 -0.02384
  0.39845 -0.02126
  0.45183 -0.01851
  0.50602 -0.01568
  0.56034 -0.01288
  0.61416 -0.01020
  0.66680 -0.00772
  0.71760 -0.00551
  0.76592 -0.00361
  0.81113 -0.00206
  0.85265 -0.00089
  0.88992 -0.00008
  0.92244  0.00039
  0.94974  0.00057
  0.97144  0.00051
  0.98721  0.00032
  0.99679  0.00010
  1.00001 -0.00000
Dat file parser warnings
  • Line 62 - X value too large but included: 1.00001 -0.00000
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Selig format dat file

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Polars for SD5060 (9.5%) (sd5060-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   sd5060-il50,000933.6 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   sd5060-il50,000536.3 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   sd5060-il100,000951.5 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   sd5060-il100,000550.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   sd5060-il200,000968.6 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   sd5060-il200,000562.8 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   sd5060-il500,000988.8 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   sd5060-il500,000579.8 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   sd5060-il1,000,0009100.9 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   sd5060-il1,000,000594.9 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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