NASA/LANGLEY NLF(1)-0416 AIRFOIL
  1.000000  0.000000
  0.996560  0.000980
  0.986860  0.003980
  0.971970  0.008620
  0.952240  0.014000
  0.927490  0.019740
  0.897790  0.025940
  0.863570  0.032650
  0.825300  0.039770
  0.783500  0.047240
  0.738720  0.054930
  0.691550  0.062720
  0.642620  0.070470
  0.592560  0.078010
  0.542040  0.085150
  0.491720  0.091660
  0.442270  0.097290
  0.394380  0.101620
  0.348390  0.104050
  0.304220  0.104250
  0.261870  0.102470
  0.221690  0.098920
  0.184040  0.093740
  0.149250  0.087070
  0.117610  0.079040
  0.089360  0.069840
  0.064710  0.059640
  0.043830  0.048700
  0.026870  0.037290
  0.013930  0.025730
  0.005090  0.014460
  0.000490  0.004030
  0.000000  0.000000
  0.000730 -0.004390
  0.007090 -0.011540
  0.019560 -0.018830
  0.037080 -0.025940
  0.059330 -0.032540
  0.086090 -0.038470
  0.117080 -0.043610
  0.152000 -0.047870
  0.190500 -0.051210
  0.232180 -0.053570
  0.276590 -0.054940
  0.323260 -0.055290
  0.371670 -0.054620
  0.421270 -0.052910
  0.471500 -0.050090
  0.521750 -0.046140
  0.571220 -0.040630
  0.620190 -0.032500
  0.670140 -0.022310
  0.721070 -0.012210
  0.771560 -0.003640
  0.820120  0.002780
  0.865360  0.006670
  0.905760  0.007920
  0.939780  0.006960
  0.966380  0.004780
  0.985200  0.002420
  0.996330  0.000650
  1.000000  0.000000