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WACO COOTIE AIRFOIL (cootie-il)

WACO COOTIE AIRFOIL - Waco Cootie airfoil


Airfoil cootie-il
Details Dat file Parser  
(cootie-il) WACO COOTIE AIRFOIL
Waco Cootie airfoil
Max thickness 8.5% at 30% chord.
Max camber 5.5% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
WACO COOTIE AIRFOIL
       17.       17.

  0.000000  0.011000
  0.012500  0.029000
  0.025000  0.039400
  0.050000  0.053800
  0.075000  0.064000
  0.100000  0.073000
  0.150000  0.086400
  0.200000  0.095600
  0.300000  0.103600
  0.400000  0.103600
  0.500000  0.097000
  0.600000  0.085000
  0.700000  0.070000
  0.800000  0.050000
  0.900000  0.028000
  0.950000  0.017000
  1.000000  0.005000

  0.000000  0.011000
  0.012500  0.001000
  0.025000  0.000000
  0.050000  0.000000
  0.075000  0.002600
  0.100000  0.006400
  0.150000  0.012000
  0.200000  0.015000
  0.300000  0.019000
  0.400000  0.022000
  0.500000  0.021200
  0.600000  0.016400
  0.700000  0.012400
  0.800000  0.008400
  0.900000  0.004000
  0.950000  0.002000
  1.000000  0.000000
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Lednicer format dat file
Selig format dat file

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Polars for WACO COOTIE AIRFOIL (cootie-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   cootie-il50,000936.3 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   cootie-il50,000539.7 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   cootie-il100,000960.1 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   cootie-il100,000562.8 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   cootie-il200,000984 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   cootie-il200,000583.4 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   cootie-il500,0009116 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   cootie-il500,0005107.6 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   cootie-il1,000,0009136.9 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   cootie-il1,000,0005121.1 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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