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