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S4083 (8%) (s4083-il)

S4083 (8%) - Selig S4083 low Reynolds number airfoil


Airfoil s4083-il
Details Dat file Parser  
(s4083-il) S4083 (8%)
Selig S4083 low Reynolds number airfoil
Max thickness 8% at 22.5% chord.
Max camber 3.4% at 35.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
S4083 (8%)
       1.00000     0.00000
       0.99815     0.00055
       0.99308     0.00220
       0.98528     0.00445
       0.97469     0.00689
       0.96115     0.00948
       0.94473     0.01230
       0.92555     0.01533
       0.90374     0.01855
       0.87944     0.02193
       0.85282     0.02544
       0.82404     0.02907
       0.79330     0.03277
       0.76080     0.03653
       0.72675     0.04031
       0.69137     0.04410
       0.65491     0.04787
       0.61762     0.05157
       0.57975     0.05519
       0.54158     0.05867
       0.50338     0.06196
       0.46541     0.06498
       0.42794     0.06768
       0.39121     0.06995
       0.35544     0.07169
       0.32082     0.07282
       0.28758     0.07322
       0.25575     0.07277
       0.22538     0.07150
       0.19665     0.06938
       0.16955     0.06640
       0.14416     0.06271
       0.12060     0.05835
       0.09893     0.05339
       0.07927     0.04795
       0.06168     0.04208
       0.04618     0.03591
       0.03289     0.02953
       0.02180     0.02306
       0.01293     0.01669
       0.00632     0.01057
       0.00201     0.00493
       0.00000     0.00016
       0.00099    -0.00346
       0.00541    -0.00618
       0.01305    -0.00842
       0.02383    -0.01019
       0.03765    -0.01146
       0.05447    -0.01227
       0.07419    -0.01265
       0.09672    -0.01261
       0.12192    -0.01219
       0.14968    -0.01143
       0.17983    -0.01037
       0.21221    -0.00907
       0.24659    -0.00757
       0.28279    -0.00593
       0.32055    -0.00420
       0.35964    -0.00243
       0.39979    -0.00067
       0.44075     0.00104
       0.48221     0.00264
       0.52390     0.00412
       0.56552     0.00546
       0.60684     0.00667
       0.64768     0.00768
       0.68776     0.00824
       0.72657     0.00826
       0.76358     0.00787
       0.79860     0.00723
       0.83138     0.00643
       0.86173     0.00551
       0.88946     0.00454
       0.91437     0.00355
       0.93632     0.00262
       0.95515     0.00179
       0.97082     0.00115
       0.98328     0.00067
       0.99239     0.00031
       0.99805     0.00010
       1.00000     0.00000
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Polars for S4083 (8%) (s4083-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s4083-il50,000931.1 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s4083-il50,000538.5 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   s4083-il100,000951.8 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s4083-il100,000556.2 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   s4083-il200,000973.3 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s4083-il200,000574.4 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   s4083-il500,0009102.8 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s4083-il500,000598.5 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   s4083-il1,000,0009124.3 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s4083-il1,000,0005115.8 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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