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NACA 64-008A AIRFOIL (n64008a-il)

NACA 64-008A AIRFOIL - NACA 64-008A airfoil


Airfoil n64008a-il
Details Dat file Parser  
(n64008a-il) NACA 64-008A AIRFOIL
NACA 64-008A airfoil
Max thickness 8% 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 64-008A AIRFOIL
      26.       26.

  0.000000  0.000000
  0.005000  0.006460
  0.007500  0.007780
  0.012500  0.009830
  0.025000  0.013530
  0.050000  0.018630
  0.075000  0.022450
  0.100000  0.025590
  0.150000  0.030470
  0.200000  0.034140
  0.250000  0.036810
  0.300000  0.038660
  0.350000  0.039720
  0.400000  0.039980
  0.450000  0.039210
  0.500000  0.037570
  0.550000  0.035240
  0.600000  0.032340
  0.650000  0.028970
  0.700000  0.025210
  0.750000  0.021170
  0.800000  0.016980
  0.850000  0.012780
  0.900000  0.008580
  0.950000  0.004380
  1.000000  0.000180

  0.000000  0.000000
  0.005000 -0.006460
  0.007500 -0.007780
  0.012500 -0.009830
  0.025000 -0.013530
  0.050000 -0.018630
  0.075000 -0.022450
  0.100000 -0.025590
  0.150000 -0.030470
  0.200000 -0.034140
  0.250000 -0.036810
  0.300000 -0.038660
  0.350000 -0.039720
  0.400000 -0.039980
  0.450000 -0.039210
  0.500000 -0.037570
  0.550000 -0.035240
  0.600000 -0.032340
  0.650000 -0.028970
  0.700000 -0.025210
  0.750000 -0.021170
  0.800000 -0.016980
  0.850000 -0.012780
  0.900000 -0.008580
  0.950000 -0.004380
  1.000000 -0.000180
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Lednicer format dat file
Selig format dat file

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Polars for NACA 64-008A AIRFOIL (n64008a-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   n64008a-il50,000919.1 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   n64008a-il50,000523.3 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   n64008a-il100,000932.5 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   n64008a-il100,000530.1 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   n64008a-il200,000941 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   n64008a-il200,000535 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   n64008a-il500,000946.5 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   n64008a-il500,000544.5 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   n64008a-il1,000,000949.9 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   n64008a-il1,000,000559.4 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
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