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NACA 64-012A AIRFOIL (n64012a-il)

NACA 64-012A AIRFOIL - NACA 64(1)-012A airfoil


Airfoil n64012a-il
Details Dat file Parser  
(n64012a-il) NACA 64-012A AIRFOIL
NACA 64(1)-012A airfoil
Max thickness 12% at 40% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
NACA 64-012A AIRFOIL
      26.       26.

  0.000000  0.000000
  0.005000  0.009610
  0.007500  0.011580
  0.012500  0.014640
  0.025000  0.020180
  0.050000  0.027880
  0.075000  0.033640
  0.100000  0.038390
  0.150000  0.045800
  0.200000  0.051320
  0.250000  0.055340
  0.300000  0.058090
  0.350000  0.059650
  0.400000  0.059930
  0.450000  0.058630
  0.500000  0.056050
  0.550000  0.052440
  0.600000  0.048010
  0.650000  0.042890
  0.700000  0.037210
  0.750000  0.031180
  0.800000  0.025000
  0.850000  0.018820
  0.900000  0.012630
  0.950000  0.006440
  1.000000  0.000250

  0.000000  0.000000
  0.005000 -0.009610
  0.007500 -0.011580
  0.012500 -0.014640
  0.025000 -0.020180
  0.050000 -0.027880
  0.075000 -0.033640
  0.100000 -0.038390
  0.150000 -0.045800
  0.200000 -0.051320
  0.250000 -0.055340
  0.300000 -0.058090
  0.350000 -0.059650
  0.400000 -0.059930
  0.450000 -0.058630
  0.500000 -0.056050
  0.550000 -0.052440
  0.600000 -0.048010
  0.650000 -0.042890
  0.700000 -0.037210
  0.750000 -0.031180
  0.800000 -0.025000
  0.850000 -0.018820
  0.900000 -0.012630
  0.950000 -0.006440
  1.000000 -0.000250
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Lednicer format dat file
Selig format dat file

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Polars for NACA 64-012A AIRFOIL (n64012a-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   n64012a-il50,000927.5 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   n64012a-il50,000527.2 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   n64012a-il100,000940 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   n64012a-il100,000535.5 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   n64012a-il200,000947.8 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   n64012a-il200,000539.9 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   n64012a-il500,000956.4 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   n64012a-il500,000552.1 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   n64012a-il1,000,000961.9 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   n64012a-il1,000,000564.9 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
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