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MARSKE PIONEER IID TIP AIRFOIL (NACA 431012A*.833 HYBRID) (marske4-il)

MARSKE PIONEER IID TIP AIRFOIL (NACA 431012A*.833 HYBRID) - Marske Pioneer IID tip airfoil (NACA 43012A*.833 hybrid)


Airfoil marske4-il
Details Dat file Parser  
(marske4-il) MARSKE PIONEER IID TIP AIRFOIL (NACA 431012A*.833 HYBRID)
Marske Pioneer IID tip airfoil (NACA 43012A*.833 hybrid)
Max thickness 10.2% at 20% 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 TIP AIRFOIL (NACA 431012A*.833 HYBRID)
       17.       17.

  0.000000  0.000000
  0.012500  0.032400
  0.025000  0.042800
  0.050000  0.057700
  0.075000  0.066900
  0.100000  0.073100
  0.150000  0.077700
  0.200000  0.077300
  0.250000  0.074600
  0.300000  0.071400
  0.400000  0.064200
  0.500000  0.054700
  0.600000  0.043300
  0.700000  0.030800
  0.800000  0.020300
  0.900000  0.010400
  1.000000  0.000000

  0.000000  0.000000
  0.012500 -0.006900
  0.025000 -0.009500
  0.050000 -0.012800
  0.075000 -0.015400
  0.100000 -0.017600
  0.150000 -0.021400
  0.200000 -0.024600
  0.250000 -0.027200
  0.300000 -0.029200
  0.400000 -0.032700
  0.500000 -0.033600
  0.600000 -0.032700
  0.700000 -0.030000
  0.800000 -0.022800
  0.900000 -0.012500
  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 TIP AIRFOIL (NACA 431012A*.833 HYBRID) (marske4-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   marske4-il50,000917 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   marske4-il50,000522.3 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   marske4-il100,000924.8 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   marske4-il100,000534.1 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   marske4-il200,000939.5 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   marske4-il200,000550.4 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   marske4-il500,000973.9 at α=11.25°Mach=0 Ncrit=9Xfoil predictionDetails
   marske4-il500,000578.9 at α=9.5°Mach=0 Ncrit=5Xfoil predictionDetails
   marske4-il1,000,0009100.6 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   marske4-il1,000,000598.6 at α=9.75°Mach=0 Ncrit=5Xfoil predictionDetails
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