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MARSKE PIONEER IID ROOT AIRFOIL (NACA 431012A/24112 HYBRID) (marske3-il)

MARSKE PIONEER IID ROOT AIRFOIL (NACA 431012A/24112 HYBRID) - Marske Pioneer IID root airfoil (NACA 43012A/24112 hybrid)


Airfoil marske3-il
Details Dat file Parser  
(marske3-il) MARSKE PIONEER IID ROOT AIRFOIL (NACA 431012A/24112 HYBRID)
Marske Pioneer IID root airfoil (NACA 43012A/24112 hybrid)
Max thickness 12.1% at 30% chord.
Max camber 2.8% at 15% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 
MARSKE PIONEER IID ROOT AIRFOIL (NACA 431012A/24112 HYBRID)
       17.       17.

  0.000000  0.000000
  0.012500  0.032200
  0.025000  0.043700
  0.050000  0.059400
  0.075000  0.069700
  0.100000  0.077000
  0.150000  0.084500
  0.200000  0.086300
  0.250000  0.085100
  0.300000  0.082500
  0.400000  0.074400
  0.500000  0.063700
  0.600000  0.050800
  0.700000  0.036600
  0.800000  0.024800
  0.900000  0.012800
  1.000000  0.000000

  0.000000  0.000000
  0.012500 -0.009000
  0.025000 -0.012300
  0.050000 -0.017300
  0.075000 -0.021300
  0.100000 -0.024500
  0.150000 -0.029300
  0.200000 -0.033100
  0.250000 -0.035500
  0.300000 -0.038100
  0.400000 -0.041800
  0.500000 -0.042300
  0.600000 -0.041500
  0.700000 -0.036400
  0.800000 -0.026500
  0.900000 -0.014100
  1.000000  0.000000
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Lednicer format dat file
Selig format dat file

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Polars for MARSKE PIONEER IID ROOT AIRFOIL (NACA 431012A/24112 HYBRID) (marske3-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   marske3-il50,000919 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   marske3-il50,000525 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   marske3-il100,000930.4 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   marske3-il100,000537.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   marske3-il200,000946.3 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   marske3-il200,000554 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   marske3-il500,000975.4 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   marske3-il500,000579 at α=10°Mach=0 Ncrit=5Xfoil predictionDetails
   marske3-il1,000,000999.8 at α=11°Mach=0 Ncrit=9Xfoil predictionDetails
   marske3-il1,000,000597.8 at α=10.5°Mach=0 Ncrit=5Xfoil predictionDetails
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