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NACA 642-015 AIRFOIL (n64015-il)

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


Airfoil n64015-il
Details Dat file Parser  
(n64015-il) NACA 642-015 AIRFOIL
NACA 64(2)-015 airfoil
Max thickness 15% at 35% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
NACA 642-015 AIRFOIL
      26.       26.

  0.000000  0.000000
  0.005000  0.012080
  0.007500  0.014560
  0.012500  0.018420
  0.025000  0.025280
  0.050000  0.035040
  0.075000  0.042400
  0.100000  0.048420
  0.150000  0.057850
  0.200000  0.064800
  0.250000  0.069850
  0.300000  0.073190
  0.350000  0.074820
  0.400000  0.074730
  0.450000  0.072240
  0.500000  0.068100
  0.550000  0.062660
  0.600000  0.056200
  0.650000  0.048950
  0.700000  0.041130
  0.750000  0.032960
  0.800000  0.024720
  0.850000  0.016770
  0.900000  0.009500
  0.950000  0.003460
  1.000000  0.000000

  0.000000  0.000000
  0.005000  -.012080
  0.007500  -.014560
  0.012500  -.018420
  0.025000  -.025280
  0.050000  -.035040
  0.075000  -.042400
  0.100000  -.048420
  0.150000  -.057850
  0.200000  -.064800
  0.250000  -.069850
  0.300000  -.073190
  0.350000  -.074820
  0.400000  -.074730
  0.450000  -.072240
  0.500000  -.068100
  0.550000  -.062660
  0.600000  -.056200
  0.650000  -.048950
  0.700000  -.041130
  0.750000  -.032960
  0.800000  -.024720
  0.850000  -.016770
  0.900000  -.009500
  0.950000  -.003460
  1.000000  0.000000
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Lednicer format dat file
Selig format dat file

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Polars for NACA 642-015 AIRFOIL (n64015-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   n64015-il50,000927.6 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   n64015-il50,000527 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   n64015-il100,000940.3 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   n64015-il100,000535.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   n64015-il200,000948.9 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   n64015-il200,000545 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   n64015-il500,000965.2 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   n64015-il500,000552.6 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   n64015-il1,000,000972.4 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   n64015-il1,000,000565 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
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