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NACA 642-015A AIRFOIL (n64015a-il)

NACA 642-015A AIRFOIL - NACA 64(2)-015A airfoil


Airfoil n64015a-il
Details Dat file Parser  
(n64015a-il) NACA 642-015A AIRFOIL
NACA 64(2)-015A airfoil
Max thickness 15% 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 642-015A AIRFOIL
      26.       26.

  0.000000  0.000000
  0.005000  0.011930
  0.007500  0.014360
  0.012500  0.018150
  0.025000  0.025080
  0.050000  0.034770
  0.075000  0.042020
  0.100000  0.047990
  0.150000  0.057320
  0.200000  0.064230
  0.250000  0.069260
  0.300000  0.072700
  0.350000  0.074630
  0.400000  0.074870
  0.450000  0.073130
  0.500000  0.069780
  0.550000  0.065170
  0.600000  0.059560
  0.650000  0.053110
  0.700000  0.046000
  0.750000  0.038470
  0.800000  0.030840
  0.850000  0.023210
  0.900000  0.015580
  0.950000  0.007950
  1.000000  0.000320

  0.000000  0.000000
  0.005000 -0.011930
  0.007500 -0.014360
  0.012500 -0.018150
  0.025000 -0.025080
  0.050000 -0.034770
  0.075000 -0.042020
  0.100000 -0.047990
  0.150000 -0.057320
  0.200000 -0.064230
  0.250000 -0.069260
  0.300000 -0.072700
  0.350000 -0.074630
  0.400000 -0.074870
  0.450000 -0.073130
  0.500000 -0.069780
  0.550000 -0.065170
  0.600000 -0.059560
  0.650000 -0.053110
  0.700000 -0.046000
  0.750000 -0.038470
  0.800000 -0.030840
  0.850000 -0.023210
  0.900000 -0.015580
  0.950000 -0.007950
  1.000000 -0.000320
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Lednicer format dat file
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Polars for NACA 642-015A AIRFOIL (n64015a-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   n64015a-il50,000928.6 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   n64015a-il50,000527.9 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   n64015a-il100,000943.2 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   n64015a-il100,000536.8 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   n64015a-il200,000949.9 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   n64015a-il200,000544.5 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   n64015a-il500,000964.4 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   n64015a-il500,000552.7 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   n64015a-il1,000,000970.1 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   n64015a-il1,000,000565.2 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
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