NACA 63-015A AIRFOIL
  1.000000  0.000320
  0.950000  0.007720
  0.900000  0.015120
  0.850000  0.022520
  0.800000  0.029910
  0.750000  0.037310
  0.700000  0.044680
  0.650000  0.051730
  0.600000  0.058200
  0.550000  0.063870
  0.500000  0.068580
  0.450000  0.072150
  0.400000  0.074350
  0.350000  0.074960
  0.300000  0.073840
  0.250000  0.070910
  0.200000  0.066190
  0.150000  0.059420
  0.100000  0.049970
  0.075000  0.043820
  0.050000  0.036180
  0.025000  0.025790
  0.012500  0.018440
  0.007500  0.014480
  0.005000  0.012030
  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