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SOMERS S102 AIRFOIL (BLUNT) (s102b-il)

SOMERS S102 AIRFOIL (BLUNT) - Dan Somers airfoil for the Toyota general aviation airplane


Airfoil s102b-il
Details Dat file Parser  
(s102b-il) SOMERS S102 AIRFOIL (BLUNT)
Dan Somers airfoil for the Toyota general aviation airplane
Max thickness 15% at 40% chord.
Max camber 2% at 68.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
SOMERS S102 AIRFOIL (BLUNT)
       33.       33.

  0.000010  0.000390
  0.000170  0.002170
  0.003570  0.011220
  0.011170  0.021280
  0.022810  0.031600
  0.038450  0.041660
  0.058030  0.050910
  0.081810  0.058870
  0.110190  0.065620
  0.142970  0.071630
  0.179540  0.077040
  0.219370  0.081780
  0.261910  0.085780
  0.306620  0.088920
  0.352960  0.091090
  0.400370  0.092150
  0.448280  0.091940
  0.496140  0.090130
  0.543790  0.086200
  0.591590  0.080250
  0.639460  0.072990
  0.686780  0.065020
  0.732900  0.056720
  0.777150  0.048420
  0.818850  0.040360
  0.857320  0.032720
  0.891910  0.025530
  0.924090  0.018640
  0.950970  0.012790
  0.972220  0.008120
  0.987590  0.004740
  0.996890  0.002690
  1.000000  0.002000

  0.000010  0.000390
  0.000090 -0.001470
  0.000540 -0.003080
  0.001510 -0.004540
  0.003000 -0.006000
  0.010180 -0.010650
  0.024520 -0.016600
  0.044240 -0.022430
  0.068960 -0.028110
  0.098300 -0.033570
  0.131800 -0.038760
  0.169020 -0.043570
  0.209430 -0.047910
  0.252500 -0.051660
  0.297690 -0.054670
  0.344410 -0.056780
  0.392080 -0.057760
  0.440110 -0.057360
  0.487870 -0.054950
  0.535700 -0.049550
  0.584860 -0.041520
  0.635440 -0.032520
  0.686450 -0.023710
  0.736820 -0.015720
  0.785480 -0.009000
  0.831350 -0.003770
  0.873430 -0.000180
  0.910730  0.001800
  0.942280  0.002380
  0.967340  0.001990
  0.985440  0.001150
  0.996360  0.000340
  1.000000  0.000000

Dat file parser warnings
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Polars for SOMERS S102 AIRFOIL (BLUNT) (s102b-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s102b-il50,000931.1 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   s102b-il50,000528.1 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   s102b-il100,000942.6 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   s102b-il100,000543.8 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   s102b-il200,000960.5 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   s102b-il200,000557.6 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   s102b-il500,000981.9 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   s102b-il500,000570.7 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   s102b-il1,000,000996.4 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   s102b-il1,000,000585.3 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
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