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SPICA 11.73% smoothed (spicasm-il)

SPICA 11.73% smoothed - Anderson SPICA R/C sailplane airfoil (smoothed)


Airfoil spicasm-il
Details Dat file Parser  
(spicasm-il) SPICA 11.73% smoothed
Anderson SPICA R/C sailplane airfoil (smoothed)
Max thickness 11.7% at 30% chord.
Max camber 4.7% at 35% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
  SPICA  11.73% smoothed
  1.00000  0.0
  0.95000  0.01195
  0.90000  0.02270
  0.85000  0.03275
  0.80000  0.04260
  0.75000  0.05238
  0.70000  0.06190
  0.65000  0.07107
  0.60000  0.07970
  0.55000  0.08773
  0.50000  0.09490
  0.45000  0.10053
  0.40000  0.10415
  0.35000  0.10583
  0.30000  0.10530
  0.25000  0.10242
  0.20000  0.09690
  0.15000  0.08805
  0.10000  0.07400
  0.08000  0.06634
  0.06000  0.05704
  0.04000  0.04560
  0.02000  0.03042
  0.01000  0.02053
  0.0      0.0
  0.01000 -0.01280
  0.02000 -0.01510
  0.04000 -0.01632
  0.06000 -0.01590
  0.08000 -0.01564
  0.10000 -0.01530
  0.15000 -0.01445
  0.20000 -0.01360
  0.25000 -0.01275
  0.30000 -0.01190
  0.35000 -0.01105
  0.40000 -0.01020
  0.45000 -0.00935
  0.50000 -0.00850
  0.55000 -0.00765
  0.60000 -0.00680
  0.65000 -0.00595
  0.70000 -0.00510
  0.75000 -0.00425
  0.80000 -0.00340
  0.85000 -0.00255
  0.90000 -0.00170
  0.95000 -0.00085
  1.00000  0.0
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Lednicer format dat file
Selig format dat file

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Polars for SPICA 11.73% smoothed (spicasm-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   spicasm-il50,000910.6 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   spicasm-il50,000530.9 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   spicasm-il100,000950.9 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   spicasm-il100,000555.9 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   spicasm-il200,000977.9 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   spicasm-il200,000577.6 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   spicasm-il500,0009112.1 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   spicasm-il500,0005104.2 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   spicasm-il1,000,0009136.7 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   spicasm-il1,000,0005123.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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