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S2062 8% (s2062-il)

S2062 8% - Selig S2062 low Reynolds number airfoil


Airfoil s2062-il
Details Dat file Parser  
(s2062-il) S2062 8%
Selig S2062 low Reynolds number airfoil
Max thickness 8% at 30.1% chord.
Max camber 1.5% at 49.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
     S2062 8%
     1.00000   0.00000
     0.99677   0.00039
     0.98732   0.00167
     0.97218   0.00391
     0.95180   0.00696
     0.92650   0.01060
     0.89659   0.01474
     0.86250   0.01932
     0.82470   0.02419
     0.78368   0.02920
     0.73994   0.03412
     0.69391   0.03877
     0.64602   0.04304
     0.59676   0.04684
     0.54664   0.05008
     0.49618   0.05267
     0.44589   0.05455
     0.39627   0.05568
     0.34783   0.05600
     0.30104   0.05550
     0.25639   0.05415
     0.21429   0.05196
     0.17516   0.04893
     0.13934   0.04507
     0.10714   0.04043
     0.07882   0.03511
     0.05459   0.02921
     0.03462   0.02288
     0.01903   0.01630
     0.00791   0.00977
     0.00140   0.00366
     0.00025  -0.00148
     0.00474  -0.00622
     0.01429  -0.01106
     0.02866  -0.01543
     0.04787  -0.01906
     0.07189  -0.02189
     0.10060  -0.02393
     0.13377  -0.02522
     0.17111  -0.02581
     0.21228  -0.02580
     0.25684  -0.02525
     0.30430  -0.02428
     0.35412  -0.02295
     0.40572  -0.02133
     0.45852  -0.01951
     0.51187  -0.01753
     0.56516  -0.01544
     0.61773  -0.01324
     0.66901  -0.01091
     0.71854  -0.00842
     0.76589  -0.00595
     0.81048  -0.00375
     0.85169  -0.00194
     0.88888  -0.00059
     0.92150   0.00027
     0.94903   0.00068
     0.97099   0.00069
     0.98699   0.00045
     0.99673   0.00014
     1.00000   0.00000
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Selig format dat file

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Polars for S2062 8% (s2062-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s2062-il50,000936 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s2062-il50,000536.4 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   s2062-il100,000952.9 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s2062-il100,000549.9 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s2062-il200,000969.7 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s2062-il200,000561.8 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   s2062-il500,000989.3 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   s2062-il500,000574.6 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   s2062-il1,000,000999.7 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s2062-il1,000,000578.9 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
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