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MARSKE PIONEER IA AIRFOIL (NACA 23112/43012A HYBRID) (marske2-il)

MARSKE PIONEER IA AIRFOIL (NACA 23112/43012A HYBRID) - Marske Pioneer IA airfoil (NACA 23112/43012A hybrid)


Airfoil marske2-il
Details Dat file Parser  
(marske2-il) MARSKE PIONEER IA AIRFOIL (NACA 23112/43012A HYBRID)
Marske Pioneer IA airfoil (NACA 23112/43012A hybrid)
Max thickness 12.1% at 25% chord.
Max camber 2.7% at 15% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
MARSKE PIONEER IA AIRFOIL (NACA 23112/43012A HYBRID)
       17.       17.

  0.000000  0.000000
  0.012500  0.033200
  0.025000  0.044300
  0.050000  0.059800
  0.075000  0.070000
  0.100000  0.076900
  0.150000  0.083400
  0.200000  0.084400
  0.250000  0.082800
  0.300000  0.080300
  0.400000  0.072900
  0.500000  0.062800
  0.600000  0.050600
  0.700000  0.036600
  0.800000  0.024400
  0.900000  0.012300
  1.000000  0.000000

  0.000000  0.000000
  0.012500 -0.010200
  0.025000 -0.014100
  0.050000 -0.018400
  0.075000 -0.021700
  0.100000 -0.024500
  0.150000 -0.029600
  0.200000 -0.034200
  0.250000 -0.037700
  0.300000 -0.040200
  0.400000 -0.043300
  0.500000 -0.043200
  0.600000 -0.040800
  0.700000 -0.035500
  0.800000 -0.026300
  0.900000 -0.014000
  1.000000  0.000000
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Lednicer format dat file
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Polars for MARSKE PIONEER IA AIRFOIL (NACA 23112/43012A HYBRID) (marske2-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   marske2-il50,000918.9 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   marske2-il50,000524 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   marske2-il100,000928.8 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   marske2-il100,000535.7 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   marske2-il200,000943 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   marske2-il200,000551.5 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   marske2-il500,000972.4 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   marske2-il500,000577.5 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
   marske2-il1,000,000999 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   marske2-il1,000,000597 at α=10.75°Mach=0 Ncrit=5Xfoil predictionDetails
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