NACA 64-012A AIRFOIL
       26.       26.

  0.000000  0.000000
  0.005000  0.009610
  0.007500  0.011580
  0.012500  0.014640
  0.025000  0.020180
  0.050000  0.027880
  0.075000  0.033640
  0.100000  0.038390
  0.150000  0.045800
  0.200000  0.051320
  0.250000  0.055340
  0.300000  0.058090
  0.350000  0.059650
  0.400000  0.059930
  0.450000  0.058630
  0.500000  0.056050
  0.550000  0.052440
  0.600000  0.048010
  0.650000  0.042890
  0.700000  0.037210
  0.750000  0.031180
  0.800000  0.025000
  0.850000  0.018820
  0.900000  0.012630
  0.950000  0.006440
  1.000000  0.000250

  0.000000  0.000000
  0.005000 -0.009610
  0.007500 -0.011580
  0.012500 -0.014640
  0.025000 -0.020180
  0.050000 -0.027880
  0.075000 -0.033640
  0.100000 -0.038390
  0.150000 -0.045800
  0.200000 -0.051320
  0.250000 -0.055340
  0.300000 -0.058090
  0.350000 -0.059650
  0.400000 -0.059930
  0.450000 -0.058630
  0.500000 -0.056050
  0.550000 -0.052440
  0.600000 -0.048010
  0.650000 -0.042890
  0.700000 -0.037210
  0.750000 -0.031180
  0.800000 -0.025000
  0.850000 -0.018820
  0.900000 -0.012630
  0.950000 -0.006440
  1.000000 -0.000250