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S8036 (16%) (s8036-il)

S8036 (16%) - Selig S8036 low Reynolds number airfoil


Airfoil s8036-il
Details Dat file Parser  
(s8036-il) S8036 (16%)
Selig S8036 low Reynolds number airfoil
Max thickness 16% at 36.8% chord.
Max camber 1.3% at 40.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
S8036 (16%)
       1.00000     0.00000
       0.99759     0.00046
       0.99095     0.00217
       0.98105     0.00501
       0.96827     0.00843
       0.95247     0.01204
       0.93354     0.01594
       0.91163     0.02027
       0.88697     0.02505
       0.85984     0.03027
       0.83047     0.03590
       0.79916     0.04189
       0.76618     0.04816
       0.73183     0.05463
       0.69641     0.06119
       0.66022     0.06771
       0.62357     0.07402
       0.58668     0.07986
       0.54969     0.08509
       0.51279     0.08963
       0.47611     0.09328
       0.43972     0.09598
       0.40381     0.09776
       0.36848     0.09853
       0.33380     0.09838
       0.29999     0.09735
       0.26722     0.09547
       0.23564     0.09280
       0.20545     0.08939
       0.17681     0.08528
       0.14988     0.08053
       0.12484     0.07520
       0.10184     0.06934
       0.08104     0.06296
       0.06251     0.05610
       0.04638     0.04885
       0.03271     0.04115
       0.02141     0.03305
       0.01256     0.02483
       0.00612     0.01649
       0.00193     0.00823
       0.00001     0.00054
       0.00098    -0.00588
       0.00548    -0.01153
       0.01338    -0.01720
       0.02433    -0.02273
       0.03811    -0.02804
       0.05468    -0.03304
       0.07395    -0.03773
       0.09576    -0.04208
       0.11999    -0.04605
       0.14648    -0.04964
       0.17504    -0.05283
       0.20549    -0.05558
       0.23760    -0.05786
       0.27120    -0.05962
       0.30609    -0.06084
       0.34204    -0.06146
       0.37887    -0.06147
       0.41638    -0.06087
       0.45435    -0.05959
       0.49265    -0.05765
       0.53099    -0.05502
       0.56937    -0.05165
       0.60778    -0.04772
       0.64594    -0.04348
       0.68359    -0.03907
       0.72043    -0.03464
       0.75616    -0.03028
       0.79048    -0.02609
       0.82309    -0.02215
       0.85370    -0.01852
       0.88202    -0.01523
       0.90775    -0.01230
       0.93064    -0.00970
       0.95044    -0.00739
       0.96698    -0.00519
       0.98037    -0.00302
       0.99070    -0.00120
       0.99754    -0.00020
       1.00000     0.00000
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Polars for S8036 (16%) (s8036-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s8036-il50,000926.6 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s8036-il50,000525.7 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s8036-il100,000948.2 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s8036-il100,000548 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   s8036-il200,000970.2 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   s8036-il200,000561.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   s8036-il500,000987.3 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   s8036-il500,000573.3 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s8036-il1,000,000999.6 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s8036-il1,000,000582.1 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
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