RAF 14 Airfoil Source: http://www.ds-cats.com/~kurisawa/aeronautics/Airfoils/01-0036.html
  1.000000  0.003800
  0.900000  0.026500
  0.800000  0.042800
  0.700000  0.054300
  0.600000  0.060800
  0.500000  0.065000
  0.400000  0.068200
  0.300000  0.070600
  0.200000  0.066300
  0.150000  0.061800
  0.100000  0.052500
  0.080000  0.046600
  0.060000  0.040000
  0.040000  0.032300
  0.030000  0.027800
  0.020000  0.022700
  0.010000  0.016700
  0.000000  0.006800
  0.010000  0.001500
  0.020000  0.000600
  0.030000  0.000100
  0.040000  0.000000
  0.060000  0.000400
  0.080000  0.002000
  0.100000  0.003900
  0.150000  0.009400
  0.200000  0.012200
  0.300000  0.013900
  0.400000  0.012700
  0.500000  0.010600
  0.600000  0.008500
  0.700000  0.006200
  0.800000  0.004200
  0.900000  0.001900
  1.000000  0.003800