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NASA/LANGLEY 64-012 AIRFOIL (n64012-il)

NASA/LANGLEY 64-012 AIRFOIL - NACA 64(1)-012 airfoil


Airfoil n64012-il
Details Dat file Parser  
(n64012-il) NASA/LANGLEY 64-012 AIRFOIL
NACA 64(1)-012 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
NASA/LANGLEY 64-012 AIRFOIL
       26.       26.

  0.000000  0.000000
  0.005000  0.009780
  0.007500  0.011790
  0.012500  0.014900
  0.025000  0.020350
  0.050000  0.028100
  0.075000  0.033940
  0.100000  0.038710
  0.150000  0.046200
  0.200000  0.051730
  0.250000  0.055760
  0.300000  0.058440
  0.350000  0.059780
  0.400000  0.059810
  0.450000  0.057980
  0.500000  0.054800
  0.550000  0.050560
  0.600000  0.045480
  0.650000  0.039740
  0.700000  0.033500
  0.750000  0.026950
  0.800000  0.020290
  0.850000  0.013820
  0.900000  0.007860
  0.950000  0.002880
  1.000000  0.000000

  0.000000  0.000000
  0.005000 -0.009780
  0.007500 -0.011790
  0.012500 -0.014900
  0.025000 -0.020350
  0.050000 -0.028100
  0.075000 -0.033940
  0.100000 -0.038710
  0.150000 -0.046200
  0.200000 -0.051730
  0.250000 -0.055760
  0.300000 -0.058440
  0.350000 -0.059780
  0.400000 -0.059810
  0.450000 -0.057980
  0.500000 -0.054800
  0.550000 -0.050560
  0.600000 -0.045480
  0.650000 -0.039740
  0.700000 -0.033500
  0.750000 -0.026950
  0.800000 -0.020290
  0.850000 -0.013820
  0.900000 -0.007860
  0.950000 -0.002880
  1.000000  0.000000
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Lednicer format dat file
Selig format dat file

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Polars for NASA/LANGLEY 64-012 AIRFOIL (n64012-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   n64012-il50,000926.7 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   n64012-il50,000527.1 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   n64012-il100,000939.9 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   n64012-il100,000532.8 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   n64012-il200,000943.5 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   n64012-il200,000539.4 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   n64012-il500,000956.5 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   n64012-il500,000551.5 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   n64012-il1,000,000960.9 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   n64012-il1,000,000565.4 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
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