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NACA 63-015A AIRFOIL (n63015a-il)

NACA 63-015A AIRFOIL - NACA 63-015A airfoil


Airfoil n63015a-il
Details Dat file Parser  
(n63015a-il) NACA 63-015A AIRFOIL
NACA 63-015A 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 63-015A AIRFOIL
       26.       26.

  0.000000  0.000000
  0.005000  0.012030
  0.007500  0.014480
  0.012500  0.018440
  0.025000  0.025790
  0.050000  0.036180
  0.075000  0.043820
  0.100000  0.049970
  0.150000  0.059420
  0.200000  0.066190
  0.250000  0.070910
  0.300000  0.073840
  0.350000  0.074960
  0.400000  0.074350
  0.450000  0.072150
  0.500000  0.068580
  0.550000  0.063870
  0.600000  0.058200
  0.650000  0.051730
  0.700000  0.044680
  0.750000  0.037310
  0.800000  0.029910
  0.850000  0.022520
  0.900000  0.015120
  0.950000  0.007720
  1.000000  0.000320

  0.000000  0.000000
  0.005000 -0.012030
  0.007500 -0.014480
  0.012500 -0.018440
  0.025000 -0.025790
  0.050000 -0.036180
  0.075000 -0.043820
  0.100000 -0.049970
  0.150000 -0.059420
  0.200000 -0.066190
  0.250000 -0.070910
  0.300000 -0.073840
  0.350000 -0.074960
  0.400000 -0.074350
  0.450000 -0.072150
  0.500000 -0.068580
  0.550000 -0.063870
  0.600000 -0.058200
  0.650000 -0.051730
  0.700000 -0.044680
  0.750000 -0.037310
  0.800000 -0.029910
  0.850000 -0.022520
  0.900000 -0.015120
  0.950000 -0.007720
  1.000000 -0.000320
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Lednicer format dat file
Selig format dat file

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Polars for NACA 63-015A AIRFOIL (n63015a-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   n63015a-il50,000928.9 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   n63015a-il50,000528.5 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   n63015a-il100,000944.4 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   n63015a-il100,000539.3 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   n63015a-il200,000953.2 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   n63015a-il200,000546.6 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   n63015a-il500,000966.3 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   n63015a-il500,000555.2 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   n63015a-il1,000,000972.8 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   n63015a-il1,000,000566.9 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
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